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AIAA JOURNAL OF PROPULSION AND POWER
http://www.aiaa.org/Research/index.hfm?res=13
Volume 19 Number 5 September 2003
Combustion Dynamics in Lean-Premixed Prevaporized (LPP) GasTurbines
Introduction: Combustion Dynamics in Lean-Premixed Prevaporized(LPP) Gas Turbines
721
Tim Lieuwen; Keith McManus
Combustion Dynamics and Instabilities: Elementary Coupling andDriving Mechanisms
722
Sébastien Ducruix; Thierry Schuller; Daniel Durox; Sébastien Candel
Experimental Diagnostics for the Study of Combustion Instabilities inLean Premixed Combustors
735
J. G. Lee; D. A. Santavicca
Acoustic Analysis of Gas Turbine Combustors 751
Ann P. Dowling; Simon R. Stow
Modeling Premixed Combustion-Acoustic Wave Interactions: A Review 765
T. Lieuwen
Large-Eddy Simulation of Combustion Dynamics of Lean-PremixedSwirl-Stabilized Combustor
782
Ying Huang; Hong-Gye Sung; Shih-Yang Hsieh; Vigor Yang
Passive Control of Combustion Dynamics in Stationary Gas Turbines 795
Geo A. Richards; Douglas L. Straub; Edward H. Robey
Factors Affecting the Control of Unstable Combustors 811
Jeffrey M. Cohen; Andrzej Banaszuk
Challenges and Progress in Controlling Dynamics in Gas TurbineCombustors
822
H. C. Mongia; T. J. Held; G. C. Hsiao; R. P. Pandalai
Full-length Papers
Time-Averaged Gradient Control of Thermoacoustic Instabilities 830
Michael A. Vaudrey; William T. Baumann; William R. Saunders
Premixed Flame Kinematics in a Longitudinal Acoustic Field 837
Doh-Hyoung Lee; Tim C. Lieuwen
Atomic Emission Spectrometry for Profiling High Temperatures inCombustion System
847
Shigeo Yatsu; Hiroyuki Oyama; Takunari Mizuno; Hideharu Kimura;Kuniyuki Kitagawa; Naoyuki Kayukawa
Ignition Characteristics of Methane and Hydrogen Using a PlasmaTorch in Supersonic Flow
853
Tomoaki Kitagawa; Atsushi Moriwaki; Koichi Murakami; Kenichi Takita;Goro Masuya
Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane 859
Takeshi Kanda; Kenji Kudo
Aerodynamic Performance Analysis of a Hypersonic Inlet Isolator UsingComputation and Experiment
868
Birgit U. Reinartz; Carsten D. Herrmann; Josef Ballmann; Wolfgang W.Koschel
Effects of Injection Configuration on Performance of a StagedSupersonic Combustor
876
Sadatake Tomioka; Kan Kobayashi; Kenji Kudo; Atsuo Murakami;Tohru Mitani
Fuel Injection and Flame Stabilization in a Liquid-Kerosene-FueledSupersonic Combustor
885
G. Yu; J. G. Li; X. Y. Chang; L. H. Chen; C. J. Sung
Magnetohydrodynamic Power Generation Experiments with Fuji-1Blowdown Facility
894
Y. Okuno; T. Okamura; T. Suekane; H. Yamasaki; S. Kabashima; S.Shioda
Some Aspects of Chemical Kinetics in Chapman-Jouguet Detonation:Induction Length Analysis
901
Tianfeng Lu; Chung K. Law; Yiguang Ju
Partial Fuel Filling in Pulse Detonation Engines 908
Chiping Li; K. Kailasanath
Tailored Fuel Injection for Pulsed Detonation Engines via FeedbackControl
917
Alberto Aliseda; Kartik B. Ariyur; Olivier Sarrazin; Juan C. Lasheras;Miroslav Krstic
Two-Dimensional Compressible Non-Acoustic Modeling of StirlingMachine-Type Components
922
Roy C. Tew Jr; Mounir B. Ibrahim
Jet Engine Gas-Path Measurement Filtering Using Center WeightedIdempotent Median Filters
930
Ranjan Ganguli
Dynamic and Nonlinear Simulation of Liquid-Propellant Engines 938
H. Karimi; A. Nassirharand
Multi-Element Unstructured Methodology for Analysis ofTurbomachinery Systems
945
Vineet Ahuja; Jeremy D. Shipman; S. Arunajatesan; Ashvin Hosangadi
Numerical Parameter Studies of Ion-Thruster-Beam Neutralization 953
Carsten Othmer; Karl-Heinz Glassmeier; Uwe Motschmann; IngoRichter
Development of a Finite Element-Based Hall-Thruster Model 964
Subrata Roy; B. P. Pandey
Volume 19 Number 4 July 2003
Full-length Papers
Analysis of Inducer Recirculating Inlet Flow 521
François Bario; Thierry M. Faure; Emmanuel Jondeau; Jean-LucNormand; Jean-Michel Nguyen Duc
Theoretical Performance of a Magnetohydrodynamic-Bypass ScramjetEngine with Nonequilibrium Ionization
529
Chul Park; David W. Bogdanoff; Unmeel B. Mehta
Deceleration of Supersonic Plasma Flow by an Applied Magnetic Field 538
Sergei V. Bobashev; Yurii P. Golovachov; David M. Van Wie
Computational Fluid Dynamics Analysis of the Central Institute ofAviation Motors/NASA Scramjet
547
Carlos G. Rodriguez
System Performance and Thermodynamic Cycle Analysis ofAirbreathing Pulse Detonation Engines
556
Yuhui Wu; Fuhua Ma; Vigor Yang
Pulse Detonation Engine Characterization and Control Using TunableDiode-Laser Sensors
568
Daniel W. Mattison; Christopher M. Brophy; Scott T. Sanders; Lin Ma;Kevin M. Hinckley; Jay B. Jeffries; Ronald K. Hanson
Detonation Initiation by Controlled Triggering of Electric Discharges 573
S. M. Frolov; V. Y. Basevich; V. S. Aksenov; S. A. Polikhov
Constant-Frequency Hypervelocity Slings 581
D. A. Tidman
Measurements and Simulation of Orifice Flow for MicropropulsionTesting
588
A. A. Alexeenko; S. F. Gimelshein; D. A. Levin; A. D. Ketsdever; M. S.Ivanov
One-Dimensional Hollow Cathode Model 595
Ira Katz; John R. Anderson; James E. Polk; John R. Brophy
Ignition Delay for Jet Propellant 10/Air and Jet Propellant 10/High-Energy Density Fuel/Air Mixtures
601
David W. Mikolaitis; Corin Segal; Abhilash Chandy
Numerical Simulation of Ion Beam Optics for Multiple-Grid Systems 607
Yoshinori Nakayama; Paul J. Wilbur
Combustion and Thermal Studies on Al/Ti/Ni/Zr Composite ModifiedDouble-Base Systems
614
C. N. Divekar; S. N. Asthana; Haridwar Singh
Erosive Burning of Ammonium Perchlorate/Hydroxyl-Terminated-Polybutadiene Propellants Under Supersonic Crossflows
623
S. Krishnan; K. K. Rajesh
Characteristics of Liquid Film and Spray Injected from Swirl CoaxialInjector
632
Takao Inamura; Hiroshi Tamura; Hiroshi Sakamoto
Analytical and Experimental Studies of Tile-Shaped Aerospike Nozzles 640
Wu-Ye Dai; Yu Liu; Xian-Chen Cheng; Bin Ma
Closed-Loop Vectoring Control of a Turbulent Jet Using PeriodicExcitation
646
D. Rapoport; I. Fono; K. Cohen; A. Seifert
Flow Separation Inside a Supersonic Nozzle Exhausting into aSubsonic Compressible Crossflow
655
S. J. Beresh; J. F. Henfling; R. J. Erven
Improved Aerodynamic-Ramp Injector in Supersonic Flow 663
L. S. Jacobsen; S. D. Gallimore; J. A. Schetz; W. F. O'Brien
Rotordynamic Bearing Dampers for Cryogenic Rocket EngineTurbopumps
674
Bugra H. Ertas; Eyad Al-Khateeb; John M. Vance
Evaluating Experimental Data Requirements for Spatially VaryingTurbine Flowfields Through Uncertainty Analysis
683
Susan T. Hudson; Boon Liang Heng
Adjoint Calculation of Sensitivities of Turbomachinery ObjectiveFunctions
693
M. Sergio Campobasso; Mihai C. Duta; Michael B. Giles
Low-Engine-Order Excitation Mechanisms in Axial-FlowTurbomachinery
704
C. Bréard; J. S. Green; M. Imregun
Technical Notes
Combustion Effects of C60 Soot in Ammonium Nitrate Propellants 713
Brian E. Greiner; Robert A. Frederick Jr.; Marlow D. Moser
Performance Analysis of Short Takeoff and Vertical Landing AircraftNozzle in Hover
715
Frank K. Lu; Douglas A. Terrier
Erratum
Errata on Theoretical Performance of FrictionlessMagnetohydrodynamics-Bypass Scramjet
718
Chul Park; David Bogdanoff; Unmeel B. Mehta
Volume 19 Number 3 May 2003
Full-length Papers
Scalability for Rocket Nozzle Flows Based on Subscale and Full-ScaleTesting
321
Gerald Hagemann; Jan Alting; Dieter Preclik
Edge Diffusion Flame Stabilization Behind a Step over a LiquidReactant
332
Matthew Juniper; Sébastien Candel
Characterization of Cryogenic Injection at Supercritical Pressure 342
Richard Branam; Wolfgang Mayer
Improvement of Inlet Flow Characteristics of LE-7A Liquid HydrogenPump
356
Masaharu Uchiumi; Kenjiro Kamijo; Kunio Hirata; Akira Konno;Tomoyuki Hashimoto; Satoshi Kobayasi
Rocket Engine Turbine Blade Surface Pressure Distributions:Experiment and Computations
364
Susan T. Hudson; Thomas F. Zoladz; Daniel J. Dorney
Effect of Nozzle Cavity on Resonance in Large SRM: NumericalSimulations
374
J. Anthoine; J.-M. Buchlin; J.-F. Guéry
Two-Phase Vorticoacoustic Flow Interactions in Solid-Propellant RocketMotors
385
Weidong Cai; Fuhua Ma; Vigor Yang
Thermoviscoelastic Characterization of a Composite Solid PropellantUsing Tubular Test
397
V. R. Sanal Kumar
Constant Volume Explosions of Aerosols of Metallic Mechanical Alloysand Powder Blends
405
Mirko Schoenitz; Edward L. Dreizin; Emil Shtessel
Optimization of Electric Thrusters for Primary Propulsion Based on theRocket Equation
413
Monika Auweter-Kurtz; Helmut Kurtz
Model of an Electrothermal Pulsed Plasma Thruster 424
Michael Keidar; Iain D. Boyd; Isak I. Beilis
Scale Effects on Solid-Propellant Coaxial MagnetoplasmadynamicThruster Performance
431
Giorgio Paccani; Luigi Petrucci; William D. Deininger
Low-Current, Xenon Orificed Hollow Cathode Performance for In-SpaceApplications
438
Matthew T. Domonkos; Michael J. Patterson; Alec D. Gallimore
Conservation Coupling Technique for Dynamic Inlet-Engine Analyses 444
Keith Numbers; Awatef Hamed
Multicriteria Design Optimization of Integrated Three-DimensionalSupersonic Inlets
456
Arnaud Gaiddon; Doyle D. Knight
Normal Shock/Boundary-Layer Interaction Control Using AeroelasticMesoflaps
464
Everett S. Hafenrichter; Yeol Lee; J. Craig Dutton; Eric Loth
Computation of Transonic Diffuser Flows by a Lagged k-_ TurbulenceModel
473
Q. Xiao; H. M. Tsai; F. Liu
Characteristics and Control of Combustion Instabilities in a Swirl-Stabilized Spray Combustor
484
S. Acharya; S. Murugappan; M. O'Donnell; E. J. Gutmark
Study of Interspacecraft Coulomb Forces and Implications forFormation Flying
497
Lyon B. King; Gordon G. Parker; Satwik Deshmukh; Jer-Hong Chong
Hysteresis Effects on Thrust Measurement and its Uncertainty 506
Joseph D. Sims; Hugh W. Coleman
Technical Notes
Analysis of Entrainment in a Sudden-Expansion Channel with WallMass Transfer
514
Jing-Tang Yang; Shih-Chao Lee; Yei-Chin Chao
Leading-Edge Shape and Aeroengine Fan Blade Performance 517
A. I. Sayma; M. Kim; N. H. S. Smith
Volume 19 Number 2 March 2003
Full-length Papers
Conceptual Development of Quiet Turbofan Engines for SupersonicAircraft
161
Dimitri Papamoschou; Marco Debiasi
Integration of an Aeroramp Injector/Plasma Igniter for HydrocarbonScramjets
170
L. S. Jacobsen; S. D. Gallimore; J. A. Schetz; W. F. O'Brien
Operational Sensitivities of an Integrated Scramjet Ignition/Fuel-Injection System
183
S. D. Gallimore; L. S. Jacobsen; W. F. O'Brien; J. A. Schetz
High Ram Acceleration Using Open-Base Projectile 190
Yuichiro Hamate; Akihiro Sasoh; Kazuyoshi Takayama
Kinetic Model for Aluminum-Sensitized Ram Accelerator Combustion 196
Laurent Catoire; Jean-François Legendre; Marc Giraud
Study of Combustion Characteristics of AmmoniumDinitramide/Polycaprolactone Propellants
203
Oleg P. Korobeinichev; Alexander A. Paletsky; Alexander G.Tereschenko; Evgeny N. Volkov
Design and Use of a Batch Reactor for Catalytic Decomposition ofPropellants
213
Rachel Eloirdi; Sylvie Rossignol; Charles Kappenstein; Daniel Duprez;Nicolas Pillet
Stability of Hydrogen/Hydrocarbon Blended Fuel Flames 220
Ahsan R. Choudhuri; S. R. Gollahalli
Numerical Simulation of High-Pressure and Fuel-Rich TurbulentCombustion Field
226
Takurou Makita; Takahisa Yamamoto; Tomohiko Furuhata; Norio Arai
Two-Phase Computational Fluid Dynamics Analysis Applied toPrefilming Pure-Airblast Atomizer
235
Philip E. O. Buelow; Chien-Pei Mao; Steven Smith; David Bretz
Axial Compressor Blade-to-Blade Unsteady Aerodynamic Variability 242
Douglas M. Boyd; Sanford Fleeter
Effects of Flow Instabilities on the Linear Analysis of TurbomachineryAeroelasticity
250
M. Sergio Campobasso; Michael B. Giles
Numerical Simulation of Aerodynamic Damping for Flutter Analysis ofTurbomachinery Blade Rows
260
R. Srivastava; M. A. Bakhle; T. G. Keith Jr.
Proper Orthogonal Decomposition of Turbine Rotor-Stator Interaction 268
Paul G. A. Cizmas; Antonio Palacios
Inlet/Engine Interactions in an Axisymmetric Pulse Detonation EngineSystem
282
Jonas Gustavsson; Venkata Nori; Corin Segal
Vortex Shedding Induced Sound Inside a Cold-Flow Simulation ofSegmented Chamber
287
Alison Flatau; W. K. Van Moorhem
Numerical Simulations of Wall and Shear Layer Instabilities in ColdFlow Setup
297
Jérôme Vétel; Frédéric Plourde; Son Doan Kim; Jean-François Guery
Technical Notes
Analyzing Mistuning of Bladed Disks by Symmetry and Reduced-OrderAerodynamic Modeling
307
B. Shapiro; K. E. Willcox
Active Control of Compressor Instability and Surge by Stator BladesAdjustment
312
M. T. Schobeiri; M. Attia
Aerodynamic Design of a VerticalThrust Adapter for Jet Engines 317
T. Strand
Volume 19 Number 1 January 2003
Editorial
Announcements and Acknowledgments 1
Reviewers for October 2001-September 2002 11
Ethical Standards for Publication of Aeronautics and AstronauticsResearch
12
AIAA Manuscript Review Process 13
Full-length Papers
Assessing Jet-Induced Spatial Mixing in a Rich, Reacting Crossflow 14
T. N. Demayo; M. Y. Leong; G. S. Samuelsen; J. D. Holdeman
Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube 22
E. Wintenberger; J. M. Austin; M. Cooper; S. Jackson; J. E. Shepherd
Thrust-Vectoring Nozzle Performance Modeling 39
Erich A. Wilson; Dan Adler; Pinhas Bar-Yoseph
Numerical Simulation of Distributed Combustion in Solid Rocket Motorswith Metalized Propellant
48
Jayant S. Sabnis
Plateau Burning Behavior of Ammonium Perchlorate Sandwiches andPropellants at Elevated Pressures
56
Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman;Jerry M. Seitzman
Optical Fouling of the RB199 Pyrometer 66
Clive Kerr; Paul Ivey
Bypass-Regulated Solid Fuel Ramjet Combustor in Variable FlightConditions
73
Deborah Pelosi-Pinhas; Alon Gany
Investigation of Instabilities in a Lean, Premixed Step Combustor 81
Jeffrey M. Cohen; Brian E. Wake; Dochul Choi
Sensitivity of Hydrocarbon Combustion Modeling for Hypersonic MissileDesign
89
Ryan P. Starkey; Mark J. Lewis
Rocketdyne Hypersonic Flow Laboratory as High-PerformanceExpansion Tube for Scramjet Testing
98
Benjamin S. Stewart; Richard G. Morgan; Peter A. Jacobs
Sonic Injection from Diamond-Shaped Orifices into a SupersonicCrossflow
104
Sadatake Tomioka; Lance S. Jacobsen; Joseph A. Schetz
Mixing Augmentation of Transverse Injection in Scramjet Combustor 115
Sang-Hyeon Lee; Tohru Mitani
Combined/Simultaneous Gust and Oscillating Compressor BladeUnsteady Aerodynamics
125
Kuk Kim Frey; Sanford Fleeter
Traveling Wave Excitation System for Bladed Disks 135
Keith W. Jones; Charles J. Cross
Numerical Study of Cryogenic Jets Under Supercritical Conditions 142
J. M. M. Barata; A. R. R. Silva
Technical Notes
Optimal Actuator/Sensor Placement for Control of CombustionInstabilities
148
Nidal Al-Masoud; Tarunraj Singh
Modified Mixing Analogy for Studies of Mixing in Supersonic Flows 151
Sadatake Tomioka; Lance S. Jacobsen; Joseph A. Schetz
Technical Comments
Technical Comment on "Vorticity Dynamics in Isobarically ClosedPorous Channels, Part 1: Standard Perturbations,"
155
R. L. Glick
Reply to Robert L. Glick's Comment: Physicality of Core Flow Models inRocket Motors
156
Joseph Majdalani
Volume 18 Number 6 November 2002
Advanced Performance Modeling of Experimental Laser Lightcraft 1129
Ten-See Wang; Yen-Sen Chen; Jiwen Liu; Leik N. Myrabo; Franklin B.Mead Jr.
Analysis and Application of Chorochronic Periodicity inTurbomachinery Rotor/Stator Interaction Computations
1139
G. A. Gerolymos; G. J. Michon; J. Neubauer
Experimental Study of the Transient Underexpanded Jet Generatedby Electrothermal Capillary Plasma
1153
Jong-Uk Kim; N. T. Clemens; P. L. Varghese
Mass-Based Optimization of Thermal Management and PowerSystems for Space Applications
1161
K. D. Freudenberg; W. E. Lear; S. A. Sherif; E. L. Golliher
Thermodynamics of Airbreathing Pulse-Detonation Engines 1170
J. A. C. Kentfield
Thermodynamic Limits of Work and Pressure Gain in Combustion andEvaporation Processes
1176
M. Razi Nalim
Work Potential Perspective of Engine Component Performance 1183
Bryce Roth
Numerical Reconstruction of Ejector Rocket Experimental Tests 1191
A. Matesanz; A. Velazquez; J. Tizon; J. Montanes
Motor and Plume Particle Size Prediction in Solid-Propellant RocketMotors
1199
Oleg B. Kovalev
Casting Process Impact on Small-Scale Solid Rocket Motor BallisticPerformance
1211
P. Le Breton; D. Ribéreau
Comparison of Laser- and Pressure-Driven Thrust Response of HMX 1218
Gautam N. Kudva; Thomas A. Litzinger
Modeling Cavitating Venturi Flows 1227
Changhai Xu; Stephen D. Heister; Robert Field
Hydrogen Peroxide Decomposition on Various Supported CatalystsEffect of Stabilizers
1235
Laurence Pirault-Roy; Charles Kappenstein; Maurice Guérin; RachelEloirdi; Nicolas Pillet
Thermochemistry of Species Produced from Monomethylhydrazine inPropulsion and Space-Related Applications
1242
Laurent Catoire; Mark T. Swihart
Advanced Seals for Industrial Turbine Applications: Design Approachand Static Seal Development
1254
Mahmut F. Aksit; Raymond E. Chupp; O. Saim Dinc; MehmetDemiroglu
Advanced Seals for Industrial Turbine Applications: Dynamic SealDevelopment
1260
Raymond E. Chupp; Farshad Ghasripoor; Norman A. Turnquist;Mehmet Demiroglu; Mahmut F. Aksit
Measured Flow Oscillations and Instabilities in Labyrinth Seal Cavities 1267
David L. Rhode; J. Wayne Johnson
Effects of Blade Count on Linearized and Nonlinear Hot StreakClocking Simulations
1273
Douglas L. Sondak; Vipul Gupta; Paul D. Orkwis; Daniel J. Dorney
Airfoil Row/Wake Interactions in a High-Speed Axial Compressor 1280
Robert T. Johnston; Sanford Fleeter
Interaction of Decaying Freestream Turbulence with a Moving ShockWave: Pressure Field
1289
S. Xanthos; G. Briassulis; Y. Andreopoulos
Proportional Control of Combustion Instabilities in a Simulated Gas-Turbine Combustor
1298
Christian Oliver Paschereit; Ephraim Gutmark
Technical Notes
Effects of End Wall Geometry and Stacking on Supersonic TurbinePerformance
1305
Daniel J. Dorney; Lisa W. Griffin; Frank W. Huber; Douglas L. Sondak
Controlling Electron Backstreaming Phenomena Through the Use of aTransverse Magnetic Field
1308
John E. Foster; Michael J. Patterson
2002 Journal of Propulsion and Power Index
Subject Index 1312
Author Index 1318
Chronological Index 1320
Volume 18 Number 5 September 2002
Full-Length Papers
A PIV Investigation of Rotor-IGV Interactions in a TransonicCompressor
969
Albert J. Sanders; John Papalia; Sanford Fleeter
Turbomachine Blade Row Interaction Predictions with a Three-Dimensional Finite Element Method
978
Dana A. Gottfried; Sanford Fleeter
Analysis of Dual-Mode Hydrocarbon Scramjet Operation at Mach 4-6.5
990
R. A. Baurle; D. R. Eklund
Acoustic Flutter Control of Three-Dimensional Transonic Rotor Flow 1003
Pong-Jeu Lu; Dartzi Pan; Yi-Di Yu
High-Speed Centrifugal Compressor Surge Initiation Characterization 1012
William C. Oakes; Patrick B. Lawless; John R. Fagan; Sanford Fleeter
Gas Turbine Engine and Sensor Fault Diagnosis Using OptimizationTechniques
1019
Marco Zedda; Riti Singh
Effect of Integration of Scramjet into Airframe on Engine Performanceand Payload
1026
Daisuke Akihisa; Takeshi Kanda; Kouichiro Tani; Kenji Kudo; GoroMasuya
Direct Experimental Impulse Measurements for Detonations andDeflagrations
1033
M. Cooper; S. Jackson; J. Austin; E. Wintenberger; J. E. Shepherd
Numerical Simulation of a Pulse Detonation Engine with HydrogenFuels
1042
Houshang B. Ebrahimi; Charles L. Merkle
Influence of Radical Concentration and Fuel Decomposition onIgnition of Propane/Air Mixture
1049
Yuriy Ya. Buriko; Viacheslav A. Vinogradov; Valentin F. Goltsev; PaulJ. Waltrup
Effects of Halons and Halon Replacements on Hydrogen-FueledLaminar Premixed Flames
1059
C. H. Kim; O. C. Kwon; G. M. Faeth
Pilot Flame Effects on Gas Jet Flames in Crossflow 1068
Sien-Fong Goh; S. R. Gollahalli
Assessment of Combustion Characteristics and Mechanism ofHydroxylammonium Nitrate-Based Liquid Monopropellant
1076
Yi-Ping Chang; Kenneth K. Kuo
Nonlinear Heterogeneous Model of Composite Solid-PropellantCombustion
1086
B. Rasmussen; R. A. Frederick Jr.
Combustion Response of Ammonium Perchlorate CompositePropellants
1093
Michael Shusser; Fred E. C. Culick; Norman S. Cohen
Property Transformation of Thermotropic Liquid Crystals Polymers 1101
J. J. Rusek; K. P. Chaffee
High Strain-Rate Constitutive Models for Solid Rocket Propellants 1106
Sook-Ying Ho
Study of Flow Separation in Truncated Ideal Contour Nozzle 1112
S. B. Verma
Technical Notes
Experimental Investigation of End-Wall Flow in Turbine Rotor 1122
X. Xiao; B. Lakshminarayana
Effect of Transient Gasdynamic Processes on the Impulse of PulseDetonation Engines
1124
C. B. Kiyanda; V. Tanguay; A. J. Higgins; J. H. S. Lee
Supersonic Wave/Blade-Row Interactions Establish BoundaryConditions for Unsteady Inlet Flows
1126
Miklos Sajben
Volume 18 Number 4 July 2002
Special Section: Electric Propulsion Space Experiment (ESEX)Program
Electric Propulsion Space Experiment (ESEX) p721
Roger M. Myers
Review of the Electric Propulsion Space Experiment (ESEX) Program p723
D. R. Bromaghim; J. R. Leduc; R. M. Salasovich; G. G. Spanjers; J.M. Fife; M. J. Dulligan; J. H. Schilling; D. C. White; L. K. Johnson
System Engineering, Design, Integration, and Qualification of ElectricPropulsion Space Experiment
p731
Mary M. Kriebel
Development and Flight Qualification of a 26-Kilowatt ArcjetPropulsion Subsystem
p740
R. J. Cassady; W. A. Hoskins; C. E. Vaughan
Orbital Performance Measurements of Air Force Electric PropulsionSpace Experiment Ammonia Arcjet
p749
J. M. Fife; D. R. Bromaghim; D. A. Chart; W. A. Hoskins; C. E.Vaughan; L. K. Johnson
Effect of ESEX 26-kW Arcjet Operation on SpacecraftCommunications
p754
M. J. Dulligan; R. Bromaghim; J. A. Zimmerman; R. M. Salasovich; D.Hardesty; L. K. Johnson
On-Orbit Optical Observations of Electric Propulsion SpaceExperiment 26-Kilowatt Arcjet
p763
L. K. Johnson; G. G. Spanjers; D. R. Bromaghim; M. W. Dulligan; W.A. Hoskins
Solar Cell Degradation During the 26-Kilowatt Electric PropulsionSpace Experiment Flight
p768
J. H. Schilling; G. G. Spanjers; D. R. Bromaghim; L. K. Johnson
Mass Deposition Measurements from 26-Kilowatt Electric PropulsionSpace Experiment Flight
p772
G. G. Spanjers; J. H. Schilling; S. F. Engelman; D. R. Bromaghim; L.K. Johnson
Radiometric Analysis from the 26-Kilowatt Electric Propulsion SpaceExperiment Flight
p777
G. G. Spanjers; J. H. Schilling; D. R. Bromaghim; L. K. Johnson
Full-Length Papers
Observations of Soot in the Combustion of Methanol/Toluene SprayFlames
p781
C. T. Avedisian; C. Presser; A. K. Gupta
Computational-Fluid-Dynamics Investigation of Aeromechanics p788
Peter D. Silkowski; Chae M. Rhie; George S. Copeland; James A.Eley; James M. Bleeg
Facility Effects on Performance Measurements of MicropropulsionSystems that Utilize Gas Expansion
p797
Andrew D. Ketsdever
Sensitivity of Solid Rocket Motors to Electrostatic Discharge: Historyand Future
p805
Alain Davenas; Roger Rat
Announcements and Acknowledgments
Asphaltic Thermoplastic Propellants p810
John J. Rusek
Full-Length Papers
Model of Aluminum Agglomerate Evolution in Combustion Products ofSolid Rocket Propellant
p814
V. A. Babuk; V. A. Vasilyev
Chemical Speciation and Dynamics in the Surface Combustion Zoneof Energetic Materials
p824
Thomas B. Brill; Merrill C. Beckstead; Joseph E. Flanagan; M. C. Lin;Thomas A. Litzinger; R. H. Woodward Waesche; Charles A. Wight
Thermomechanical Analysis and Optimization of Cryogenic LiquidRocket Engines
p835
Detlef Kuhl; Jörg Riccius; Oskar J. Haidn
Effect of Momentum Ratio on the Mixing Performance of Unlike SplitTriplet Injectors
p847
Y. D. Won; Y. H. Cho; S. W. Lee; W. S. Yoon
Flourescence and Temperature Measurements in an Actively ForcedSwirl-Stabilized Spray Combustor
p855
V. Santhanam; F. C. Knopf; S. Acharya; E. Gutmark
Heat Release Rates of Burning Items in Fires p866
Hyeong-Jin Kim; David G. Lilley
New Fossil Power Systems and the Role of Open-CycleMagnetohydrodynamics Generators
p871
Naoyuki Kayukawa
Application of Autoassociative Neural Network on Gas-Path SensorData Validation
p879
Pong-Jeu Lu; Tzu-Cheng Hsu
Control of Low-Pressure Turbine Separation Using Vortex-GeneratorJets
p889
Rolf Sondergaard; Richard B. Rivir; Jeffrey P. Bons
Analysis and Multidisciplinary Optimization of Internal CoolantNetworks in Turbine Blades
p896
Thomas J. Martin; George S. Dulikravich
Optimum Mixing of Core and Bypass Streams in High-Bypass CivilTurbofan
p907
Vivek Sanghi; B. K. Lakshmanan; S. K. Sane
Automated Design Optimization of a Three-Dimensional S-ShapedSubsonic Diffuser
p913
Sophia Lefantzi; Doyle D. Knight
Inlet/Compressor System Response to Short-Duration AcousticDisturbances
p922
Anthony B. Opalski; Miklos Sajben
Analysis of a Fusion-Electric Airbreathing Earth to Orbit LaunchVehicle
p933
Robert B. Adams; D. Brian Landrum
Characterization of Expansion Tube Flows for HypervelocityCombustion Studies
p943
Adela Ben-Yakar; Ronald K. Hanson
Drag and Total Pressure Distributions in Scramjet Engines at Mach 8Flight
p953
Tohru Mitani; Tetsuo Hiraiwa; Yuichi Tarukawa; Goro Masuya
Technical Notes
Laser-Air Interactions in an Internal Supersonic Flowpath p961
Robert B. Adams; D. Brian Landrum
Timescaling Control Volumes During Real Time Digital Simulation of aMilitary Turbofan
p964
Vivek Sanghi; B. K. Lakshmanan
Technical Comments
Comment on "Equation for Additive Drag Coefficient at StaticConditions"
p967
William H. Heiser; Jack D. Mattingly
Reply to Technical Comment from William H. Heiser and Jack D.Mattingly
p968
K. L. Christensen
Volume 18 Number 3 May 2002
Full-Length Papers
Project Orion and Future Prospects for Nuclear Pulse Propulsion 497
G. R. Schmidt; J. A. Bonometti; C. A. Irvine
Study of the Phase-Lock Phenomenon for a Circular Slingatron 505
G. R. Cooper; D. A. Tidman
Shape Optimization of Supersonic Turbines Using GlobalApproximation Methods
509
Approximation Methods
Nilay Papila; Wei Shyy; Lisa Griffin; Daniel J. Dorney
Unsteady Cascade Aerodynamics in the Time Domain 519
Dana A. Gottfried; Sanford Fleeter
Multiobjective Optimization of Rocket Engine Pumps UsingEvolutionary Algorithm
528
Akira Oyama; Meng-Sing Liou
Three-Dimensional Hybrid Mesh Generation for TurbomachineryAirfoils
536
Kyu-Sup Kim; Paul G. A. Cizmas
Development of High-Performance Airfoils for Axial Flow CompressorsUsing Evolutionary Computation
544
Ernesto Benini; Andrea Toffolo
High-Pressure Steam Flow in Turbine Bypass Valve System Part 1:Valve Flow
555
R. S. Amano; G. R. Draxler
High-Pressure Steam Flow in Turbine Bypass Valve System Part 2:Pipe Flow
561
R. S. Amano; G. R. Draxler; J. M. Golembiewski
Acceptance Screening of Turbopump Gears Using the CepstrumMethod
572
S. J. DiMaggio
Appearance of Restricted Shock Separation in Rocket Nozzles 577
G. Hagemann; M. Frey; W. Koschel
Performance Analysis of Secondary Gas Injection into a Conical RocketNozzle
585
Hyun Ko; Woong-Sup Yoon
Ejector Primary Flow Molecular Weight Effects in an Ejector-RamRocket Engine
592
Sam Han; John Peddieson Jr.; David Gregory
Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines 600
William H. Knuth; Martin J. Chiaverini; J. Arthur Sauer; Daniel J.Gramer
Combustion of Liquefying Hybrid Propellants: Part 1, General Theory 610
M. A. Karabeyoglu; D. Altman; B. J. Cantwell
Combustion of Liquefying Hybrid Propellants: Part 2, Stability of LiquidFilms
621
M. A. Karabeyoglu; B. J. Cantwell
Burning Aluminum Particles Inside a Laboratory-Scale Solid RocketMotor
631
John C. Melcher; Herman Krier; Rodney L. Burton
Evaluation of Ultrasound Technique for Solid-Propellant Burning-RateResponse Measurements
641
Jeffrey J. Murphy; Herman Krier
Aerodynamic Optimization of Turbomachinery Cascades UsingEuler/Boundary-Layer Coupled Genetic Algorithms
652
Ozhan Oksuz; I. Sinan Akmandor; Mehmet S. Kavsaoglu
When Do Open-Loop Strategies for Combustion Control Work? 658
R. K. Prasanth; A. M. Annaswamy; J. P. Hathout; A. F. Ghoniem
Flashover: A Study of Parameter Effects on Time to Reach FlashoverConditions
669
Hyeong-Jin Kim; David G. Lilley
Comparison of Criteria for Room Flashover 674
Hyeong-Jin Kim; David G. Lilley
Effects of Airstream Mach Number on H2/N2 Plasma Igniter 679
Goro Masuya; Kenichi Takita; Katsuyoshi Takahashi; Fumio Takatori;Hiroyuki Ohzeki
Elliptic Coflow Effects on a Circular Gas Jet Flame 686
Ahsan R. Choudhuri; Sayela P. Luna; S. R. Gollahalli
Experimental Study of a 3-kW Stirling Engine 696
Noboru Kagawa
Improved Mean-Flow Solution for Slab Rocket Motors with RegressingWalls
703
Chong Zhou; Joseph Majdalani
Technical Notes
Geometric Evaluation of Axisymmetric Thrust-Vectoring Nozzles forAerodynamic Performance Predictions
712
Erich A. Wilson; Dan Adler; Pinhas Z. Bar-Yoseph
Combustion Characteristics of Ethylene in Scramjet Engines 716
A. A. Taha; S. N. Tiwari; T. O. Mohieldin
High-Intensity Sound Absorption at an Orifice with Bias Flow 718
Xiaodong Jing; Xiaofeng Sun
Volume 18 Number 2 March 2002
Full-Length Papers
Multilevel Analysis of Pulsed Detonation Engines 225
Houshang B. Ebrahimi; Rajendran Mohanraj; Charles L. Merkle
Development of Advanced Industrial Furnace Using Highly PreheatedCombustion Air
233
T. Hasegawa; S. Mochida; A. K. Gupta
Effects of Liquid-Oxygen Post Biasing on SSME Injector WallCompatibility
240
P. A. Strakey; D. G. Talley; L. K. Tseng; K. I. Miner
Time- and Length Scales of Combustion in Liquid Rocket ThrustChambers
247
B. Ivancic; W. Mayer
Computations of Axisymmetric Plug-Nozzle Flowfields: Flow Structuresand Thrust Performance
254
Takashi Ito; Kozo Fujii; A. Koich Hayashi
Numerical Simulation of Side Loads in an Ideal Truncated Nozzle 261
Sébastien Deck; Philippe Guillen
Design Analysis of a Satellite Hydrazine Propulsion System 270
An-Shik Yang; Tien-Chuan Kuo
Leak Fault Detection of Liquid Rocket Engine Based on StrongTracking Filter
280
Yu Daren; Wang Jianbo
Temperature-Dependent Modal Test/Analysis Correlation of X-34FASTRAC Composite Rocket Nozzle
284
Andrew M. Brown
Characteristic Analysis of Flow-Induced Vibrations on Inducer ofOxygen Pump
289
Liang Hengli; Chen Zuoyi
Numerical Predictions of Channel Flows with Fluid Injection UsingReynolds-Stress Model
295
Bruno Chaouat
Effect of Nozzle Cavity on Resonance in Large SRM: TheoreticalModeling
304
J. Anthoine; J-M. Buchlin; A. Hirschberg
Dynamic Combustion of Solid Propellants: Effects of UnsteadyCondensed Phase Degradation Layer
312
K. R. Anil Kumar; K. N. Lakshmisha
Slingatron: A High Velocity Rapid Fire Sling 322
Derek A. Tidman
Sizing a Slingatron-Based Space Launcher 330
Mark L. Bundy; Derek A. Tidman; Gene R. Cooper
Numerical Simulations of the Slingatron 338
G. R. Cooper; D. A. Tidman; M. L. Bundy
Ethylene Ignition and Detonation Chemistry, Part 1: Detailed Modelingand Experimental Comparison
344
B. Varatharajan; F. A. Williams
Ethylene Ignition and Detonation Chemistry, Part 2: Ignition Historiesand Reduced Mechanisms
352
B. Varatharajan; F. A. Williams
Study of the High-Temperature Autoignition of n-Alkane/O2/Ar Mixtures 363
D. C. Horning; D. F. Davidson; R. K. Hanson
Profiling of Redox Index During Combustion to Monitor C/C CompositeDegradation in Flames
372
Kuniyuki Kitagawa; Masao Kubota; Norio Arai; Ashwani K. Gupta
Chemiluminescence-Based Feedback Control of Equivalence Ratio fora Continuous Combustor
376
a Continuous Combustor
Douglas A. Scott; Galen B. King; Normand M. Laurendeau
Linear Deterministic Source Terms for Hot Streak Simulations 383
Paul D. Orkwis; Mark G. Turner; John W. Barter
Combustion Instability Active Control Using Periodic Fuel Injection 390
J. P. Hathout; M. Fleifil; A. M. Annaswamy; A. F. Ghoniem
Constant Volume Limit of Pulsed Propulsion for a Constant _ Ideal Gas 400
Douglas G. Talley; Edward B. Coy
Combustion Air Jet Influence on Primary Zone Characteristics for Gas-Turbine Combustors
407
S. Gogineni; D. Shouse; C. Frayne; J. Stutrud; G. Sturgess
Mach 8 Testing of a Scramjet Engine with Ramp Compression 417
Takeshi Kanda; Kouichiro Tani; Kan Kobayashi; Toshihito Saito; TetsujiSunami
Magnetohydrodynamic Power Extraction from Cold Hypersonic Airflowswith External Ionizers
424
Sergey O. MacHeret; Mikhail N. Shneider; Richard B. Miles
Analysis of a High-Efficiency Low-Emissions "Chemical Gas Turbine"System
432
Takahisa Yamamoto; Tomohiko Furuhata; Norio Arai; Noam Lior
Fuzzy Logic Intelligent System for Gas Turbine Module and SystemFault Isolation
440
Ranjan Ganguli
Particle Image Velocimetry Characterization of a Chordwise BendingCascade Flowfield
448
Daniel A. Ehrlich; Sanford Fleeter
Rotor Blade-to-Blade Wake Variability and Effect on Downstream VaneResponse
456
Albert J. Sanders; Sanford Fleeter
Massively Parallel Simulation of the Unsteady Flow in an Axial TurbineStage
465
Jixian Yao; Roger L. Davis; Juan J. Alonso; Antony Jameson
Impeller Blade Unsteady Aerodynamic Response to Vaned DiffuserPotential Fields
472
Dana Gottfried; Sanford Fleeter
Recent GRC Aerospace Technologies Applicable to Terrestrial EnergySystems
481
M. David Kankam; Valerie J. Lyons; Mark A. Hoberecht; Robert R.Tacina; Aloysius F. Hepp
Technical Notes
Correlating Laser Induced Fluorescence and Molecular Beam MassSpectrometry Ion Energy Distributions
489
George J. Williams; Timothy B. Smith; Frank S. Gulczinski; Alec D.Gallimore
Transonic Rotor Blade Pressure Measurement Using FluorescentPaints
491
T. Liu; S. Torgerson; J. Sullivan; R. Johnston; S. Fleeter
Unsteady Flow in a Supersonic Turbine with Variable Specific Heats 493
Daniel J. Dorney; Lisa W. Griffin; Frank Huber; Douglas L. Sondak
Volume 18 Number 1 January 2002
Editorial
Announcements and Acknowledgments 1
V. Yang
Reviewers for October 2000-September 2001 10
Editorial Policy Statement on Numerical Accuracy and ExperimentalUncertainty
11
Ethical Standards for Publication of Aeronautics and AstronauticsResearch
12
AIAA Manuscript Review Process 13
Full-Length Papers
History of U.S. Navy Ramjet, Scramjet, and Mixed-Cycle PropulsionDevelopment
14
P. J. Waltrup; M. E. White; F. Zarlingo; E. S. Gravlin
Integrated Design and Analysis of Intakes and Nozzles in Air-BreathingEngines
28
M. Ferlauto; F. Larocca; L. Zannetti
Analytical Model of the Base Flow Between a Subsonic and SupersonicFlow
35
Doo S. Baik; Glen W. Zumwalt
Numerical Simulation of the Ram Accelerator Using a New ChemicalKinetics Mechanism
44
Michael J. Nusca
Scale-Up Experiments on Liquid-Fueled Active Combustion Control 53
Ken H. Yu; Ken J. Wilson
Experimental Investigation of Limit-Cycle Oscillations in an UnstableGas Turbine Combustor
61
Tim C. Lieuwen
Thermodynamic Cycle Analysis of Pulse Detonation Engines 68
William H. Heiser; David T. Pratt
Fundamentals of Idealized Airbreathing Pulse-Detonation Engines 77
J. A. C. Kentfield
Selection of Actuators and Sensors for Surge Control 84
Marc Van De Wal; Frank Willems; Bram De Jager
Flow Control via Rotor Trailing Edge Blowing in Rotor/Stator AxialCompressor
93
A. M. Wo; A. C. Lo; W. C. Chang
Active Control of Discrete-Frequency Noise Generated by Rotor-StatorInteractions
100
Scott Sawyer; Sanford Fleeter; John Simonich
Shock Fitting a Transonic Cascade Solution into an Inverse DesignTechnique
107
Jeffrey W. Yokota; Adam J. Medd
Experimental and Analytical Design Verification of the Dual-BellConcept
116
Gerald Hagemann; Michael Terhardt; Dietrich Haeseler; Manuel Frey
Effects of Grain Geometry on Pulse-Triggered Combustion Instability inRocket Motors
123
Mehdi Golafshani; Mohammad Farshchi; Hojat Ghassemi
Overview of the Development of Hydrazinium Nitroformate 131
H. F. R. Schöyer; W. H. M. Welland-Veltman; J. Louwers; P. A. O. G.Korting; A. E. D. M. van der Heijden; H. L. J. Keizers; R. P. van denBerg
Overview of the Development of Hydrazinium Nitroformate-BasedPropellants
138
H. F. R. Schöyer; W. H. M. Welland-Veltmans; J. Louwers; P. A. O. G.Korting; A. E. D. M. van der Heijden; H. L. J. Keizers; R. P. van denBerg
Design of a Fusion Propulsion System - Part 1: Gigawatt-LevelMagnetoplasmadynamic Source
146
Pavlos G. Mikellides; Peter J. Turchi; Ioannis G. Mikellides
Design of a Fusion Propulsion System - Part 2: Numerical Simulation ofMagnetic-Nozzle Flows
152
Ioannis G. Mikellides; Pavlos G. Mikellides; Peter J. Turchi; Thomas M.York
Interior and Exterior Laser-Induced Fluorescence and PlasmaMeasurements within a Hall Thruster
159
W. A. Hargus Jr; M. A. Cappelli
Verification Tests of Carbon-Carbon Composite Grids for MicrowaveDischarge Ion Thruster
169
I. Funaki; H. Kuninaka; K. Toki; Y. Shimizu; K. Nishiyama; Y. Horiuchi
Cascade Arc Studies of Hydrogen/Nitrogen Plasmas in Nonequilibrium 176
Trevor Moeller; Dennis Keefer; Robert Rhodes
Flow Past Stationary Spherical Particles with Streamwise VelocityFluctuation
184
A. Dasgupta; T. I-P. Shih
Reduced Chemical Kinetic Mechanisms for Hydrocarbon Fuels 192
Christopher J. Montgomery; Marc A. Cremer; Jyh-Yuan Chen; BerkeleyBerkeley; Charles K. Westbrook; Lourdes Q. Maurice
Two-Dimensional Spectroscopic Analysis of a Flame Using HighlyPreheated Combustion Air
199
Noriyuki Konishi; Kuniyuki Kitagawa; Norio Arai; Ashwani K. Gupta
Technical Notes
Anomalous Deflagration Behavior of Ammonium Perchlorate atElevated Pressures
205
Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman;Jeffrey M. Freeman
Effects of GH2/LOX Velocity and Momentum Ratios on Shear CoaxialInjector Atomization
209
M. Ferraro; R. J. Kujala; J.-L. Thomas; M. J. Glogowski; M. M. Micci
Equation for Additive Drag Coefficient at Static Conditions 211
K. L. Christensen
Intercusp Electron Transport in an NSTAR-Derivative Ion Thruster 213
John E. Foster
Optimal Three-Dimensional Nozzle Shape Design Using CFD andParallel Simulated Annealing
217
X. Wang; M. Damodaran
Propagation of Acoustic Waves in a Two-Phase Vaporizing Mixture 222
Joël Dupays; François Vuillot
Erratum 224
Progress in Hypersonic Science and Technology Development
Volume 17 Number 6 November 2001
Editorial 1137
History
Scramjet Engines: The First Forty Years 1138
Edward T. Curran
Program Overview and Case Studies
Two-Stage-to-Orbit Spaceplane Concept with Growth Potential 1149
Unmeel B. Mehta; Jeffrey V. Bowles
Testing Technologies and Flight Experiments
Numerical Research of Gaseous Fuel Preinjection in HypersonicThree-Dimensional Inlet
1162
O. V. Guoskov; V. I. Kopchenov; K. E. Lomkov; V. A. Vinogradov; P.J. Waltrup
Program Overview and Case Studies
Development of Hydrocarbon-Fueled Scramjet Engines: TheHypersonic Technology (HyTech) Program
1170
O. A. Powell; J. T. Edwards; R. B. Norris; K. E. Numbers; J. A. Pearce
French-Russian Partnership on Hypersonic Wide-Range Ramjets 1177
Marc Bouchez; François Falempin; Vadim Levine; Valery Avrashkov;Dmitri Davidenko
Multidisciplinary Optimization of Airbreathing Hypersonic Vehicles 1184
Kevin G. Bowcutt
Synthesis of a FESTIP Airbreathing TSTO Space TransportationSystem
1191
H. Grallert
System Performance Analysis and Concept Studies
Upper Bounds on the Flight Speed of Hydrocarbon-Fueled Scramjet-Powered Vehicles
1199
Paul J. Waltrup
Domain of the Scramjet 1205
L. H. Townend
Significance of Fuel Selection for Hypersonic Vehicle Range 1214
Mark J. Lewis
Structural Mechanics and Materials
Experimental Study of Scramjet Module 1222
Marat A. Goldfeld; Alexey V. Starov; Viacheslav V. Vinogradov
System Performance Analysis and Concept Studies
Strutjet Engine Performance 1227
Bryan T. Campbell; Adam Siebenhaar; Thong Nguyen
Structural Mechanics and Materials
Development Study of a Precooler for the Air-Turboramjet Expander-Cycle Engine
1233
Kenya Harada; Nobuhiro Tanatsugu; Tetsuya Sato
Combined Engine for Reusable Launch Vehicle (KLIN Cycle) 1239
V. V. Balepin; P. A. Czysz; R. H. Moszée
Advancement of Scramjet Magnetohydrodynamic Concept 1247
B. M. Burakhanov; A. P. Likhachev; S. A. Medin; V. A. Novikov; V. I.Okunev; V. Yu. Rickman; V. A. Zeigarnik
Fundamental Mechanisms: Combustion and Fuel Management
Initiators for Endothermic Fuels 1253
D. T. Wickham; J. R. Engel; B. D. Hitch; M. E. Karpuk
Thermal Stability of Energetic Hydrocarbon Fuels for Use in CombinedCycle Engines
1258
K. Wohlwend; L. Q. Maurice; T. Edwards; R. C. Striebich; M.Vangsness; A. S. Hill
Investigation of Kerosene Combustion Characteristics with PilotHydrogen in Model Supersonic Combustors
1263
G. Yu; J. G. Li; X. Y. Chang; L. H. Chen; C. J. Sung
Historical Survey on Enhanced Mixing in Scramjet Engines 1273
John M. Seiner; S. M. Dash; D. C. Kenzakowski
Effect of Flame-Holding Cavities on Supersonic-CombustionPerformance
1287
Ken H. Yu; Ken J. Wilson; Klaus C. Schadow
Newly Developed Direct-Connect High-Enthalpy SupersonicCombustion Research Facility
1296
Combustion Research Facility
Mark Gruber; Jeffrey Donbar; Kevin Jackson; Tarun Mathur; RobertBaurle; Dean Eklund; Charles Smith
Supersonic Combustion Experiments with a Cavity-Based FuelInjector
1305
Tarun Mathur; Mark Gruber; Kevin Jackson; Jeff Donbar; WayneDonaldson; Thomas Jackson; Fred Billig
Dual-Mode Combustion of Hydrogen in a Mach 5, Continuous-FlowFacility
1313
C. P. Goyne; J. C. McDaniel; T. M. Quagliaroli; R. H. Krauss; S. W.Day
Numerical Simulation of Supersonic Airflow with Transverse HydrogenInjection
1319
E. von Lavante; D. Zeitz; M. Kallenberg
Effects of Swirl and Skew Upon Supersonic Wall Jet in Crossflow 1327
A. D. Cutler; S. E. Doerner
Skin-Friction Measurements in a Supersonic Combustor withCrossflow Fuel Injection
1333
H. Tanno; A. Paull; R. J. Stalker
Thermal Analysis of Fluid-Structural Interaction in High-Speed EngineFlowfields
1339
Birgit U. Reinartz; Wolfgang W. Koschel
Fundamental Mechanisms: Inlet and Nozzle
Optimal Design of Plug Nozzles and Their Thrust Determination atStart
1347
A. N. Kraiko; N. I. Tillyayeva; S. V. Baftalovskii
Computation of a Nonequilibrium Expansion Flow in a SingleExpansion Ramp Nozzle
1353
Thomas Link; Wolfgang W. Koschel
Testing Technologies and Flight Experiments
Experimentation, Test, and Evaluation Requirements for FutureAirbreathing Hypersonic Systems
1361
Dan Marren; Mark Lewis; Lourdes Q. Maurice
Quasi-One-Dimensional High-Speed Engine Model with Finite-RateChemistry
1366
Timothy F. O'Brien; Ryan P. Starkey; Mark J. Lewis
Volume 17 Number 5 September 2001
Full-Length Papers
Hybrid (Particle-Fluid) Modeling of Pulsed Plasma Thruster Plumes 945
Nikolaos A. Gatsonis; Xuemin Yin
Heating and Plasma Properties in a Coaxial Gasdynamic PulsedPlasma Thruster
959
Stewart S. Bushman; Rodney L. Burton
Quasi-Steady Magnetoplasmadynamic Thruster PerformanceDatabase
967
E. Y. Choueiri; J. K. Ziemer
Electrospray as a Source of Nanoparticles for Efficient ColloidThrusters
977
M. Gamero-Castaño; V. Hruby
Impact of Energy Gain and Subsystem Characteristics on FusionPropulsion Performance
988
S. Chakrabarti; G. R. Schmidt
Development of a Resonance Igniter for GO2/Kerosene Ignition 995
Mario Niwa; A. Santana Jr.; Khoze Kessaev
Nonlinear Control of a Reusable Rocket Engine for Life Extension 998
Carl F. Lorenzo; Asok Ray; Michael S. Holmes
Flame-Spreading Phenomena in Fin Slots of a Solid Rocket Motor 1005
K. K. Kuo; R. A. Kokal; M. Paulauskas; P. Alaksin; L. S. Lee
Effects of Oxidizer Particle Size on Propellants Based on ModifiedPolyvinyl Chloride
1012
Vladica S. Bozic; Marko V. Milos
Burning-Rate Modifier Effects on a Modified Polyvinyl Chloride-BasedPropellants
1017
Vladica S. Bozic; Djordje Dj. Blagojevic
Development of Thermal Barriers for Solid Rocket Motor Nozzle Joints 1023
Bruce M. Steinetz; Patrick H. Dunlap Jr.
Flexibilized Novolac Epoxy Resin for Inhibition of CompositePropellants
1035
J. P. Agrawal; N. T. Agawane
Russian Research on Experimental Hydrogen-Fueled Dual-ModeScramjet: Conception and Preflight Tests
1041
Donat A. Ogorodnikov; Viacheslav A. Vinogradov; Yurii M. Shikhman;Vitaliy N. Strokin
Magnetohydrodynamics Energy Bypass Scramjet Performance withReal Gas Effects
1049
Chul Park; Unmeel B. Mehta; David W. Bogdanoff
Ignition and Flame Studies for an Accelerating Transonic Mixing Layer 1058
X. Fang; F. Liu; W. A. Sirignano
Underexpanded Jet for Testing Laser-Based Combustion Diagnostics 1067
K. G. Klavuhn; J. C. McDaniel
Effect of Ambient Pressure on an Airblast Spray Injected into aCrossflow
1076
May Y. Leong; Vincent G. McDonell; G. Scott Samuelsen
Ignition Delays in MMH + CH4 + O2 + Ar Mixtures 1085
Laurent Catoire; Gabrielle Dupré; Claude Paillard; Abdelkrim Elaissi
Acoustic-Wave/Blade-Row Interactions Establish Boundary Conditionsfor Unsteady Inlet Flows
1090
for Unsteady Inlet Flows
Miklos Sajben; Hazem Said
Mechanisms and Prediction Methods for Fan Blade Stall Flutter 1100
M. Vahdati; A. I. Sayma; J. G. Marshall; M. Imregun
Experimental Investigation of Lobed Mixer Performance 1109
A. Abolfadl; M. A. Metwally; A. M. El-Messiry; M. A. Ali
Optimum Fan Pressure Ratio for Bypass Engines with Separate orMixed Exhaust Streams
1117
Abhijit Guha
Optimization of Turbomachinery Airfoils with a Genetic/ Sequential-Quadratic-Programming Algorithm
1123
Brian H. Dennis; George S. Dulikravich; Zhen-Xue Han
Technical Notes
Mixing of Supersonic Jets in a Strutjet Propulsion System 1129
S. Muller; Clark W. Hawk; P. G. Bakker; D. Parkinson; M. Turner
Modular Ignition System Based on Resonance Igniter 1131
M. Niwa; A. Santana Jr.; K. Kessaev
Experimental Investigation of Pulsatile Flow in Circular Tubes 1133
Josef Adamec; Ji í No i ka; Daniel Hanus; Josef Ko ená
Volume 17 Number 4 July 2001
Full-Length Papers
Direct Flight to Pluto Using Solar Electric Propulsion 753
J. S. Meserole; W. R. Richards
Low Mass Components for Mars Ascent Propulsion 758
Keith Dyer; George Yankura; Jesus Acosta
Triple Langmuir Probe Measurements in the Plume of a Pulsed PlasmaThruster
762
Robert Eckman; Lawrence Byrne; Nikolaos A. Gatsonis; Eric J. Pencil
Computation of Hall Thruster Performance 772
L. Garrigues; I. D. Boyd; J. P. Boeuf
High-Pressure Bipropellant Microrocket Engine 780
A. P. London; A. H. Epstein; J. L. Kerrebrock
Experimental Study of Major Species and Temperature Profiles ofLiquid Oxygen/Gaseous Hydrogen Rocket Combustion
788
Serdar Yeralan; Sibtosh Pal; Robert J. Santoro
Propellant Atomization and Ignition Phenomena in LiquidOxygen/Gaseous Hydrogen Rocket Combustors
794
Wolfgang O. H. Mayer; Blazenko Ivancic; Axel Schik; Ulf Hornung
Combustion Behavior and Flame Structure of XM46 Liquid Propellant 800
Y.-P. Chang; E. Boyer; K. K. Kuo
Analysis of In-Flight Behavior of Truncated Plug Nozzles 809
F. Nasuti; M. Onofri
Evaporation of Sprays of Liquid Fuels and Liquid Oxidizers in a ShearLayer
818
D. Katoshevski; Y. Tambour
Sensitivity of Mixed Subsonic-Supersonic Turbulent Mixing Layers 823
D. Chad Cottrell III; Michael W. Plesniak
Computation of Compressible Flows Through a Chemical Laser Devicewith Crossflow Injection
836
James H. Miller; Joe S. Shang; Robert F. Tomaro; William Z. Strang
Convergence Behavior of Surface Evolver Applied to a GenericPropellant-Management Device
845
Steven H. Collicott
Combustion of Magnesium with Carbon Dioxide and Carbon Monoxideat Low Gravity
852
Angel Abbud-Madrid; Abhijit Modak; Melvyn C. Branch; John W. Daily
Combustion Characteristics of a Liquid-Fueled Ramjet Combustor 860
Takao Inamura; Mamoru Takahashi; Akinaga Kumakawa
Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets:An Overview
869
Adela Ben-Yakar; Ronald K. Hanson
Internally Mixed Liquid Injector for Active Control of AtomizationProcess
878
A. Kushari; Y. Neumeier; O. Israeli; E. Lubarsky; B. T. Zinn
Random Packs and Their Use in Modeling Heterogeneous SolidPropellant Combustion
883
S. Kochevets; J. Buckmaster; T. L. Jackson; A. Hegab
Blade-Row Interaction in a High-Pressure Turbine 892
V. S. P. Chaluvadi; A. I. Kalfas; M. R. Banieghbal; H. P. Hodson; J. D.Denton
Hub Wall Rotation Influence on High-Speed Compressor CascadePerformance
902
A. Doukelis; K. Mathioudakis; K. Papailiou
Nonlinear Dynamic Combustion in Solid Rockets: L* Effects 909
K. C. Tang; M. Q. Brewster
Actuator Duct Model of Turbomachinery Components for Powered-Nacelle Navier-Stokes Calculations
919
Entsung Hsiao; Mahmood Naimi; Jeffrey P. Lewis; Keith Dalbey; YifangGong; Choon Tan
Aeroacoustic Measurement of Transient Hot Nozzle Flows 928
Daniel R. Kirk; Douglas O. Creviston; Ian A. Waitz
Technical Notes
Downstream Gas Effect on Nozzle Flow-Separation Location 936
John W. Murdock; Richard P. Welle
Adaptive Analysis of the Inviscid Supersonic Flow over a Backward-Facing Step
938
S. Y. Yang
Effect of Reynolds Number on Pitot-Pressure Distributions inUnderexpanded Supersonic Freejets
940
Hiroshi Katanoda; Taro Handa; Yoshiaki Miyazato; Mitsuharu Masuda;Kazuyasu Matsuo
Numerical Evaluation of Inelastic Mechanisms in a Nitrogen Arcjet 943
Shigeru Kuchi-Ishi; Michio Nishida
Volume 17 Number 3 May 2001
Full-Length Papers
Laser Doppler Anemometry Measurements in an Axial CompressorStage
481
Thierry M. Faure; Guy-Jean Michon; Hubert Miton; Nicolas Vassilieff
Shape Parameterization and Optimization of a Two-Stroke Engine 492
Angelos P. Mimis; Malcolm I. G. Bloor; Michael J. Wilson
Mars-Earth Rapid Interplanetary Tether Transport System: I. InitialFeasibility Analysis
499
Gerald D. Nordley; Robert L. Forward
Spectral Content of Solar Radiation on Martian Surface Based on MarsPathfinder
508
J. Appelbaum; A. Steiner; G. A. Landis; C. R. Baraona; T. Segalov
Ion Propulsion Development Projects in U.S.: Space Electric RocketTest I to Deep Space 1
517
James S. Sovey; Vincent K. Rawlin; Michael J. Patterson
Development and Validation of Fluid/Thermodynamic Models forSpacecraft Propulsion Systems
527
Henry C. Hearn
Safe Testing of Nuclear Rockets 534
Steven D. Howe; Bryan Travis; David K. Zerkle
Search for Nuclear Isotopes for Use in a Nuclear Battery 540
B. D. Guenther; H. R. Weller; Jennifer L. Godwin
Review of Refractory Materials for Alkali Metal Thermal-to-ElectricConversion Cells
547
Jeffrey C. King; Mohamed S. El-Genk
Stress and Buckling Analyses of Multitube, Vapor-Anode, Nb-1Zr/C-103AMTEC Cells
557
Jeffrey C. King; Mohamed S. El-Genk
Analysis of Heat-Driven Jet-Pumped Cooling System for SpaceThermal Management
566
J. W. Nord; W. E. Lear; S. A. Sherif
Computational Optimization of a Hypersonic Rectangular-to-CircularInlet
571
John W. Sabean; Mark J. Lewis
Sidewall Interaction in an Asymmetric Simulated Scramjet InletConfiguration
579
D. V. Gaitonde; M. R. Visbal; J. S. Shang; A. A. Zheltovodov; A. I.Maksimov
Manipulation of Shock/Boundary-Layer Interactions in Hypersonic Inlets 585
D. Schulte; A. Henckels; R. Neubacher
Theoretical Performance of Frictionless Magnetohydrodynamic-BypassScramjets
591
Chul Park; David Bogdanoff; Unmeel B. Mehta
Propulsive Performance of Hypersonic Oblique Detonation Wave andShock-Induced Combustion Ramjets
599
J. P. Sislian; H. Schirmer; R. Dudebout; J. Schumacher
Effects of Fuel Preinjection on Mixing in Mach 1.6 Airflow 605
Michael Owens; Sudarshan Mullagiri; Corin Segal; Viacheslav A.Vinogradov
Thermal Choking Analyses in a Supersonic Combustor 611
M. G. Owens; S. Mullagiri; C. Segal; P. J. Ortwerth; A. B. Mathur
Thrust, Lift, and Pitching Moment of a Scramjet Engine 617
Takashi Shimura; Noboru Sakuranaka; Tetsuji Sunami; Kouichiro Tani
Small-Bore Ram Accelerator Operation 622
A. Sasoh; Y. Hamate; K. Takayama
Aerothermal Model for Real-Time Digital Simulation of a Mixed-FlowTurbofan Engine
629
Vivek Sanghi; B. K. Lakshmanan; R. Rajasekaran
Unified Treatment of Flow Instabilities of Turbomachines 636
Yoshinobu Tsujimoto; Kenjiro Kamijo; Christopher E. Brennen
Tip Leakage Flow in a Radial Inflow Turbine with Varying Gap Height 644
R. Dambach; H. P. Hodson
Analysis of Unsteady Blade Row Interaction Using Nonlinear HarmonicApproach
651
T. Chen; P. Vasanthakumar; L. He
Development and Validation of a Massively Parallel Flow Solver forTurbomachinery Flows
659
Jixian Yao; Antony Jameson; Juan J. Alonso; Feng Liu
Redesigning Gas-Generator Turbines for Improved UnsteadyAerodynamic Performance Using Neural Networks
669
Nateri K. Madavan; Man Mohan Rai; Frank W. Huber
Influence of Compressor Exit Conditions on Combustor AnnularDiffusers, Part 1: Diffuser Performance
678
A. G. Barker; J. F. Carrotte
Influence of Compressor Exit Conditions on Combustor AnnularDiffusers Part II: Flow Redistribution
687
A. G. Barker; J. F. Carrotte
Turbojet and Turbofan Engine Performance Increases Through TurbineBurners
695
F. Liu; W. A. Sirignano
Pressure Waves in Volume Effect in Gas-Turbine Transient-Performance Models
706
Y. G. Li; N. R. L. MacCallum; P. Pilidis
Pressure Drop Across a Double-Outlet Vortex Chamber 711
Georgios H. Vatistas; Peter Sakaris
Parametric Study of the Swirler/Venturi Spray Injectors 717
Kyoung-Su Im; Hoisan Kim; Ming-Chia Lai; Robert Tacina
On the Breakup of Viscous Liquid Sheets by Dual-Mode LinearAnalysis
728
Sushanta K. Mitra; Xianguo Li; Metin Renksizbulut
Mixing Mechanisms in a Pair of Impinging Jets 736
Nasser Ashgriz; William Brocklehurst; Douglas Talley
Technical Note
Studies on Performance of Airblast Atomizer Under Varying Flow andGeometric Conditions
750
S. N. Sridhara; B. N. Raghunandan
Volume 17 Number 2 March 2001
Full-Length Papers
Gear Fault Detection in Rocket Engine Turbomachinery 225
S. J. Dimaggio; S. Rubin; B. H. Sako
Oscillating Airfoil Aerodynamics of a Rotating Compressor Blade Row 232
Kuk Kim Frey; Sanford Fleeter
240
Michael K. Fabian; Eric A. Falk; Eric J. Jumper
Control of Blade Flutter by Smart-Casing Treatment 248
Xiaofeng Sun; Xiaodong Jing; Hongwu Zhao
Comparison of Methods for Calculating Turbine Work in the AirTurborocket
256
K. L. Christensen
Upstream-Propagating Potential Disturbances in the F109 TurbofanEngine Inlet Flow
262
Eric A. Falk; Eric J. Jumper; Michael K. Fabian; Jerry Stermer
Analysis of a Device for Generating Perturbations in Supersonic WindTunnels
270
Kevin J. Melcher; Mounir B. Ibrahim
Experimental Testing of a Hypersonic Inlet with Rectangular-to-EllipticalShape Transition
276
M. K. Smart
Mole-Fraction-Sensitive Imaging of Hypermixing Shear Layers 284
J. S. Fox; A. F. P. Houwing; P. M. Danehy; M. J. Gaston; N. R.Mudford; S. L. Gai
Combustion Tests of a Staged Supersonic Combustor with a Strut 293
Sadatake Tomioka; Atsuo Murakami; Kenji Kudo; Tohru Mitani
Combustion Efficiencies of Supersonic Flames 301
Albert Ratner; James F. Driscoll; Hwanil Huh; Rodney A. Bryant
Reaction and Mixing-Controlled Combustion in Scramjet Engines 308
Tohru Mitani; Nobuo Chinzei; Takeshi Kanda
Scramjet Fuels Autoignition Study 315
Meredith B. Colket III; Louis J. Spadaccini
Comparison of Thermodynamic Loss Models Suitable for Gas TurbinePropulsion
324
Bryce A. Roth; Dimitri N. Mavris
SCCREAM: A Conceptual Rocket-Based Combined-Cycle EnginePerformance Analysis Tool
333
John R. Olds; John E. Bradford
High-Energy-Utilization, Dual-Mode System Concept for Mars Missions 340
Mohamed S. El-Genk
Structural Dynamic Analysis of Solid Rocket Motor Resonant Burning 347
K. W. Dotson; J. M. Womack; P. J. Grosserode
Vorticity Dynamics in Isobarically Closed Porous Channels Part I:Standard Perturbations
355
J. Majdalani
Vorticity Dynamics in Isobarically Closed Porous Channels Part II:Space-Reductive Perturbations
363
J. Majdalani; T. S. Roh
Periodic Propellant Flames and Fluid-Mechanical Effects 371
T. L. Jackson; J. Buckmaster; A. Hegab
Study of a New Kind of Multipulse Rocket Motor 380
Mingde Song; Dingyou Ye
Numerical Modeling of Pressurization of a Propellant Tank 385
Alok Majumdar; Todd Steadman
Response Surface and Neural Network Techniques for Rocket EngineInjector Optimization
391
Wei Shyy; P. Kevin Tucker; Rajkumar Vaidyanathan
Mixing Characteristics of Coaxial Injectors at High Gas/LiquidMomentum Ratios
402
P. A. Strakey; D. G. Talley; J. J. Hutt
Advanced Sub-Model for Airblast Atomizers 411
Y. Liao; S. M. Jeng; M. A. Jog; M. A. Benjamin
Near-Field Ion Energy and Species Measurements of a 5-kW HallThruster
418
Frank S. Gulczinski III; Alec D. Gallimore
Internal Plasma Properties and Enhanced Performance of 8-CentimeterIon Thruster Discharge
428
John E. Foster; Michael J. Patterson
Plasma Confinement in the Whistler Wave Plasma Thruster 433
B. W. Stallard; E. B. Hooper Jr; J. L. Power
Thermal Decomposition of RDX in the Presence of Added K2B12H12 441
Michael A. Schroeder; Robert A. Fifer; Pamela J. Kaste; Shirley A.Liebman
Direct Evidence of Spatial Burning Rate Variation as Cause of MidwebAnomaly
449
Desh Deepak; R. Jeenu; P. Sridharan; M. S. Padmanabhan
Combustion of Kerosene in Counterflow Diffusion Flames 453
P. M. Patterson; A. G. Kyne; M. Pourkashanian; A. Williams; C. W.Wilson
Surrogate Mixtures to Represent Complex Aviation and Rocket Fuels 461
Tim Edwards; Lourdes Q. Maurice
Analysis and Design of the Inductor-Current-Sensing Peak-Power-Tracking Solar-Array Regulator
467
Yoon-Jay Cho; Bo-Hyung Cho
Technical Notes
Optimal Geometry of Self-Field Magnetoplasmadynamic Thrusters 472
Guido Colasurdo; Lorenzo Casalino
Transonic Compressor Influences on Upstream Surface Pressures withAxial Spacing
474
Peter J. Koch; Douglas P. Probasco; J. Mitch Wolff; William W.Copenhaver; Randall M. Chriss
Thermodynamic Cycle Analysis of Magnetohydrodynamic-BypassHypersonic Airbreathing Engines
477
Ron J. Litchford; John W. Cole; Valentine A. Bityurin; John T. Lineberry
Volume 17 Number 1 January 2001
Editorial
A Distinguished Career. . .and a New Beginning 1
Roger L. Simpson
To Everything There Is a Season 2
R. H. Woodward Waesche
Thank You and Best Wishes to Dr. R. H. Woodward Waesche 3
Vigor Yang
Reviewers for October 1999-September 2000 8
Editorial Policy Statement on Numerical Accuracy and ExperimentalUncertainty
9
Ethical Standards for Publication of Aeronautics and AstronauticsResearch
10
AIAA Manuscript Review Process 11
Full-Length Papers
Erosion Resistance of Carbon-Carbon Ion Optics 12
J. S. Meserole
Magnetohydrodynamics Generator with Plasma Layers as PowerSource Aboard a Hypersonic Airplane
19
Vadim S. Slavin; Valery M. Gavrilov; Nikolay I. Zelinsky; Alexandr R.Bozhkov
Development of Ultraviolet Raman Diagnostics for Rocket EngineInjector Analysis
27
Joseph A. Wehrmeyer; John M. Cramer; Richard H. Eskridge; Chris C.Dobson
Fuel Regression Rate in Hydroxyl-Terminated-Polybutadiene/Gaseous-Oxygen Hybrid Rocket Motors
35
Philmon George; S. Krishnan; P. M. Varkey; M. Ravindran; LalithaRamachandran
Upstream Wake Influences on the Measured Performance of aTransonic Compressor Stage
43
Steven E. Gorrell; William W. Copenhaver; Randall M. Chriss
Flow and Acoustic Properties of Underexpanded Elliptic-Slot Jets 49
S. B. Verma; E. Rathakrishnan
Studies on Combustion of Metallized RDX-Based Composite ModifiedDouble-Base Propellants
58
C. N. Divekar; S. N. Asthana; Haridwar Singh
Transient Force Reduction in Electromechanical Actuators for Thrust-Vector Control
65
Dale E. Schinstock; Douglas A. Scott; Tim A. Haskew
Flame Spread with Sudden Expansions of Ports of Solid PropellantRockets
73
B. N. Raghunandan; V. R. Sanal Kumar; C. Unnikrishnan; C. Sanjeev
Scalar Variance Transport in the Turbulence Modeling of PropulsiveJets
79
N. Chidambaram; S. M. Dash; D. C. Kenzakowski
Optimization for Aircraft Engines with Regression and Neural-NetworkAnalysis Approximators
85
Surya N. Patnaik; James D. Guptill; Dale A. Hopkins; Thomas M.Lavelle
Multidisciplinary Approach to Linear Aerospike Nozzle Design 93
J. J. Korte; A. O. Salas; H. J. Dunn; N. M. Alexandrov; W. W. Follett; G.E. Orient; A. H. Hadid
Regression-Rate and Heat-Transfer Correlations for Hybrid RocketCombustion
99
Martin J. Chiaverini; Kenneth K. Kuo; Arie Peretz; George C. Harting
Computational Assessment of Afterburning Cessation Mechanisms inFuel-Rich Rocket Exhaust Plumes
111
William H. Calhoon Jr
Gun Interior Ballistic Performance with Ammonium Nitrate-AlcoholPropellants
120
Akihiro Sasoh; Toshihiro Ogawa; Kazuyoshi Takayama; Kazunari Ikuta;Nobuo Nagayasu; Shinobu Ohtsubo
Model of Particulate Interaction with Plasma in a Teflon Pulsed PlasmaThruster
125
Michael Keidar; Iain D. Boyd; Isak I. Beilis
Mach 8 Testing of a Scramjet Engine Model 132
Takeshi Kanda; Tetsuji Sunami; Sadatake Tomioka; Kouichiro Tani;Tohru Mitani
Effect of Sides-Spillage from Airframe on Scramjet Engine Performance 139
Kouichiro Tani; Takeshi Kanda; Kenji Kudo; Daisuke Akihisa
Fundamental Studies of Cavity-Based Flameholder Concepts forSupersonic Combustors
146
M. R. Gruber; R. A. Baurle; T. Mathur; K.-Y. Hsu
Effect of Reynolds Number on Separation Bubbles on CompressorBlades in Cascade
154
Garth V. Hobson; Denis J. Hansen; David G. Schnorenberg; Darren V.Grove
Amine Sensitization Studies of Secondary Explosives Using Laser-Induced Ignition
163
A. L. Ramaswamy; T. Mukundan; M. M. Chaudhri
Effects of Interjet Spacing on Burning Multiple Sprays 169
K. Parvez; S. R. Gollahalli
Application of Artificial Neural Networks to the Design ofTurbomachinery Airfoils
176
Man Mohan Rai; Nateri K. Madavan
Novel Electroexplosive Device Incorporating a Reactive LaminatedMetallic Bridge
184
Thomas A. Baginski; Steven L. Taliaferro; Wm. David Fahey
Pressure Effects on Geometry and Structure of Gas Jet Flames inCrossflow
190
Ahsan R. Choudhuri; S. R. Gollahalli
Velocity and Temperature Statistics in Reacting Droplet-LadenHomogeneous Shear Turbulence
197
Farzad Mashayek
Origins of Accelerator Grid Current: Analysis of T5 Grid Test Results 203
Mark W. Crofton; Iain D. Boyd
Technical Notes
Fluid Property Effects on Sheet Disintegration of a Simplex Pressure-Swirl Atomizer
212
I-Ping Chung; Cary Presser
Characteristic Gap: A New Design Criterion for Solid Rocket Motors 216
Daniel Chasman
Concentration Measurements in a Mixing Module for Lean, Premixed,Gas-Turbine Combustors
218
R. V. Ravikrishna; D. Douglas Thomsen; Clayton S. Cooper; YananJiang; Normand M. Laurendeau
Radiation and NOx Pathways in Nonpremixed Turbulent Flames 222
D. Lentini; I. K. Puri
Volume 16 Number 6 November 2000
Full-Length Papers
Optimization of Orifice Geometry for Crossflow Mixing in a CylindricalDuct
929
J. T. Kroll; W. A. Sowa; G. S. Samuelsen; J. D. Holdeman
Comparison of Spray/Wall Impingement Models with ExperimentalData
939
Seong Hyuk Lee; Hong Sun Ryou
Numerical Study of Fuel Mixing Enhancement Using an ObliqueShock/Vortex Interaction
946
Ashish Nedungadi; Mark J. Lewis
Maximum Mixing Times of Methane and Air 956
Dan Brasoveanu; Ashwani K. Gupta
Multicomponent-Fuel Film-Vaporization Model for MultidimensionalComputations
964
Yangbing Zeng; Chia-Fon Lee
Soot Patterns Around Suspended n-Heptane Droplet Flames in aConvection-Free Environment
974
C. Thomas Avedisian; Gregory S. Jackson
Effect of Sauter Mean Diameter on the Combustion RelatedParameters in Heavy-Duty Diesel Engines
980
Stanislav N. Danov; Ashwani K. Gupta
Predicting Effectiveness of H2O Injection for NOx Reduction inStationary Gas Turbines
988
A. M. Mellor
Broadband Infrared Absorption Sensor for High-Pressure CombustorControl
994
J. M. Seitzman; B. T. Scully
Computation of Gas-Liquid Droplet Cascade Flows Using MultigridAdaptive Unstructured Grid
1002
Ki-Cheol Park; Keun-Shik Chang
Performance of Evaporative Cycle Gas Turbines Derived fromAeroengines
1011
Sergio Mario Camporeale; Bernardo Fortunato
Determination of Triggering Condition of Vortex-Driven AcousticCombustion Instability in Rocket Motors
1022
Wen-Jing Wu; Li-Chung Kung
Computational Analysis for Rocket-Based Combined-Cycle SystemsDuring Rocket-Only Operation
1030
C. J. Steffen Jr; T. D. Smith; S. Yungster; D. J. Keller
Starting Envelope of the Subdetonative Ram Accelerator 1040
E. Schultz; C. Knowlen; A. P. Bruckner
Work Interaction in Quasi-One-Dimensional Flows 1053
Thomas Scott; David W. Riggins
Longitudinally Stratified Combustion in Wave Rotors 1060
M. Razi Nalim
Solid-Fuel Ramjet Regulation by Means of an Air-Division Valve 1069
Deborah Pelosi-Pinhas; Alon Gany
Impingement Heating and Ignition of Condensed-Phase EnergeticMaterials
1075
Mohammad K. Alkam; P. Barry Butler
Development of the Low-Power Xenon Ion Thruster for LightweightSatellites
1083
O. A. Gorshkov; V. G. Grigor'yan; V. A. Muravlev
Mass Spectral Measurements in the Plume of an SPT-100 HallThruster
1086
Lyon B. King; Alec D. Gallimore
Electrical Characteristics of Magnetohydrodynamic-GeneratorSidewalls with Segmented Z-Bar Design
1093
Carlson C. P. Pian; Stanley W. Petty
Pulsed Fusion Propulsion System for Rapid Interstellar Missions 1100
Terry Kammash
Regenerative Solid Oxide Fuel Cells for Mars Exploration 1105
K. R. Sridhar; R. Foerstner
Optimal Allocation with Network Limitation for Autonomous SpacePower System
1112
James A. Momoh; Jizhong Zhu; Jim L. Dolce
Application of Bethe-Zel'dovich-Thompson Fluids in Organic RankineCycle Engines
1118
Brady P. Brown; Brian M. Argrow
Performance Analysis for High-Speed Missile Inlets 1125
Christophe Bourdeau; Michaël Blaize; Doyle Knight
Automated Design of a Three-Dimensional Subsonic Diffuser 1132
Wei-Li Zhang; Doyle D. Knight; Don Smith
Simulation of Coupled Unsteady Flow and Heat Conduction in TurbineStage
1141
Douglas L. Sondak; Daniel J. Dorney
Mechanical Coupling Effects on Turbomachine Mistuned Response 1149
James A. Kenyon; Charles J. Cross; Gregory R. Minkiewicz
Hub-Based Vibration Control of Multiple Rotating Airfoils 1155
György Szász; George T. Flowers; Roy J. Hartfield
Linear Versus Quadratic Amplitude Feedback in Active Control ofCompressor Rotating Stall
1164
Nikos Markopoulos; Yedidia Neumeier; J. V. R. Prasad; Ben T. Zinn
Three-Dimensional Automatic Optimization Method forTurbomachinery Blade Design
1174
K. F. C. Yiu; M. Zangeneh
Technical Note
Thixotropic Effect of Inorganic Gel Fuels 1182
Shai Rahimi; Benveniste Natan
Volume 16 Number 5 September 2000
Full-Length Papers
Optimization of Jet Mixing into a Rich, Reacting Crossflow 729
M. Y. Leong; G. S. Samuelsen; J. D. Holdeman
Propagation of Spinning Acoustic Modes in Turbofan Exhaust Ducts 736
M. Nallasamy; D. L. Sutliff; L. J. Heidelberg
Unsteady Viscous Flow Causing Rotor-Stator Interaction in Turbines,Part 1: Data, Code Pressure
744
B. Lakshminarayana; A. Chernobrovkin; D. Ristic
Unsteady Viscous Flow Causing Rotor-Stator Interaction in Turbines,Part 2: Simulation, Integrated Flowfield, and Interpretation
751
A. Chernobrovkin; B. Lakshminarayana
Analytical and Experimental Assessment of Two Methods ofDetermining Turbine Efficiency
760
Susan T. Hudson; Hugh W. Coleman
Unsteady Blade-Row Flow Calculations Using a Low-Reynolds-NumberTurbulence Model
768
Chang Ho Choi; Jung Yul Yoo
Fluid Circuit Model for Long-Bearing Squeeze Film DamperRotordynamics
777
Paul A. Schallhorn; David A. Elrod; David G. Goggin; Alok K. Majumdar
Bleed Valve Rate Requirements Evaluation in Rotating Stall Control onAxial Compressors
781
Simon Yeung; Yong Wang; Richard M. Murray
Dynamic Simulation of a Wave-Rotor-Topped Turboshaft Engine 792
R. B. Greendyke; D. E. Paxson; M. T. Schobeiri
Survey of Advancements in Jet-Engine Thermodynamic Simulation 797
Vivek Sanghi; B. K. Lakshmanan; V. Sundararajan
Analysis of Transient Thermal Choking Processes in a Model ScramjetEngine
808
S. O'Byrne; M. Doolan; S. R. Olsen; A. F. P. Houwing
Design and Control of Solid-Fuel Ramjet for PseudovacuumTrajectories
815
S. Krishnan; Philmon George; S. Sathyan
Injection and Mixing Processes in High-Pressure LiquidOxygen/Gaseous Hydrogen Rocket Combustors
823
W. Mayer; A. Schik; M. Schäffler; H. Tamura
Analysis of Gaseous Fuel and Air Mixing in Flames and FlameQuenching
829
Dan Brasoveanu; Ashwani K. Gupta
Effect of Inlet Turbulence and Premixer Length on Fuel Distribution inSwirling Gas-Turbine Premixer
837
S. F. Frey; A. R. Eaton; D. M. Cusano; M. W. Plesniak; P. E. Sojka
Role of Oxygen-Enriched Atomization in Kerosene Spray Flames 845
A. K. Gupta; T. Damm; S. R. Charagundla; C. Presser
Overview of World Space Launches 853
I-Shih Chang
Oscillatory Combustion of Fine-AP/HTPB Propellants: DisproportionatePyrolysis Response
867
S. R. Hickman; M. Q. Brewster
Prediction of the Dissipation of a Solid-Rocket Contrail 874
Eugene Miller
On-Orbit Demonstration of a Pulsed Self-Field MagnetoplasmadynamicThruster System
880
K. Toki; Y. Shimizu; K. Kuriki
Applied-Field Magnetoplasmadynamic Thrusters, Part 1: NumericalSimulations Using the MACH2 Code
887
Pavlos G. Mikellides; Peter J. Turchi; Norman F. Roderick
Applied-Field Magnetoplasmadynamic Thrusters, Part 2: AnalyticExpressions for Thrust and Voltage
894
Pavlos G. Mikellides; Peter J. Turchi
Computation of the Plume of an Anode-Layer Hall Thruster 902
Iain D. Boyd
Investigation of the Operating Characteristics of a High-Power HallEffect Thruster
910
Boris Arhipov; Leonid Krochak; Nikolay Maslennikov; Fabrizio Scortecci
Ion-Energy Diagnostics in the Plasma Exhaust Plume of a Hall Thruster 916
Lyon B. King; Alec D. Gallimore
Antimatter Requirements and Energy Costs for Near-Term PropulsionApplications
923
G. R. Schmidt; H. P. Gerrish; J. J. Martin; G. A. Smith; K. J. Meyer
Volume 16 Number 4 July 2000
Editorial 545
Norio Arai; Kuni Kitagawa; Ashwani K. Gupta
Advanced Terrestrial Energy Conversion
Advanced Power Generation 545
R. H. Woodward Waesche
Utilization of High-Density Strained Hydrocarbon Fuels for Propulsion 546
Gabriel D. Roy
Analysis of Combustion Characteristics of Coaxial Jet Diffusion Flamewith Steam Addition
552
D. Zhao; H. Yamashita; T. Furuhata; N. Arai
Power Generation Analysis for High-Temperature Gas Turbine inThermodynamic Process
557
Hiroshi Taniguchi; Sigehiro Miyamae; Norio Arai; Noam Lior
Double Reheat Rankine Cycle for Hydrogen-Combustion, TurbinePower Plants
562
Masafumi Fukuda; Yoshikazu Dozono
Enhancing Direct-Fired Power Plants Performance by Use of GasTurbine Technology
568
Mikhail Korobitsyn
Status and Perspective of Externally Fired Gas Turbines 572
J. Yan; L. Eidensten
Miniaturization Technologies for Advanced Energy Conversion andTransfer Systems
577
Timothy A. Ameel; Ian Papautsky; Robert O. Warrington; Robert S.Wegeng; M. Kevin Drost
Gas Turbine Heat Transfer: Past and Future Challenges 583
Ralf Schiele; Sigmar Wittig
Investigation of Regenerative Combustion Using a Heavy Fuel Oil 590
I-Te Huang; Wen-Chen Chang; Wei-Min Chern; Rey-Chein Chang
Visualization of Fuel Jet in Conditions of Highly Preheated AirCombustion
595
S. Lille; T. Dobski; W. Blasiak
Characteristics of Pulverized Coal Combustion in High-TemperaturePreheated Air
601
Takashi Kiga; Kunio Yoshikawa; Masaru Sakai; Susumu Mochida
Gasification Characteristics of Biomass Wastes in Fluidized BedGasifier
606
Ping Liu; Xiaofen Guo; Chuangzhi Wu; Yong Chen; Norio Arai
Modeling of Oxy-Natural Gas Combustion Chemistry 609
Anders Brink; Mikko Hupa; Frederic Breussin; Nicolas Lallemant;Roman Weber
Thermal Destruction of Cellulose and Surrogate Solid Wastes 615
Ashwani K. Gupta
Stability of Plane Liquid Sheets in Compressible Gas Streams 623
Jianming Cao; Xianguo Li
Recent Advances in Soot Formation from Spherical Droplet Flames atAtmospheric Pressure
628
C. Thomas Avedisian
Influence of Exhaust Aftertreatment Devices on Heavy-Duty DieselEngine's Particulate Emissions
636
George Toussimis; Euripides Lois; Hartmut Lüders
Fire Development Calculations 641
David G. Lilley
Minimum Safe Distance from Pool Fires 649
David G. Lilley
Transition in Boundary Layers on a Concave Surface 653
S. H. Winoto; D. H. Zhang; Y. T. Chew
Full-Length Papers
Localized Thermal Buckling Due to Hot Streaks in a Combustor Liner 661
W. Z. Zhuang; N. S. Swansson
Thermal State-of-Charge of Space Solar Dynamic Heat Receivers 666
Carsie A. Hall III; Emmanuel K. Glakpe; Joseph N. Cannon; Thomas W.Kerslake
Effect of Initial Velocity Profile on the Development of Round Jets 676
E. Ferdman; M. V. Ötügen; S. Kim
Feasibility Study for Performance Prediction of CircumferentiallyCompound-Stage Model Turbines
687
André P. Saxer; Hélène M. Saxer-Felici; Damian M. A. Vogt; MichaelSell; George Gyarmathy
Numerical Investigation of Installation Effects in Turbofan Engines 697
W. G. Joo
Energy Management in Rocket Propulsion 705
Guido Colasurdo; Lorenzo Casalino
Comparison of Supersonic Combustion Between Impulse and Vitiation-Heated Facilities
709
R. R. Boyce; A. Paull; R. J. Stalker; M. Wendt; N. Chinzei; H. Miyajima
Technical Notes
Unstarted Inlet for Direct-Connect Combustor Experiments in a ShockTunnel
718
R. R. Boyce; A. Paull; R. J. Stalker
Reference Spray Combustion Facility for Computational FluidDynamics Model Validation
720
John F. Widmann; S. Rao Charagundla; Cary Presser
Role of Curing Agents on Decomposition and Explosion of GlycidylAzide Polymers
723
Surendra P. Panda; Sanjay K. Sahu; Dinkar S. Sadafule; Jyotsna V.Thakur
Numerical Simulation of Axisymmetric Solid Rocket Motor IgnitionTransient with Radiation Effect
725
In Hyun Cho; Seung Wook Baek
Volume 16 Number 3 May 2000
Full-Length Papers
Effects of Radial Location on the Migration of Hot Streaks in a Turbine 377
Karen L. Gundy-Burlet; Daniel J. Dorney
Viscous Three-Dimensional Simulation of Transonic Compressor Stageon Parallel Hardware
388
Gerd Fritsch; Martin Hoeger; Cristoph Blaha; Dirk Bauer
Incidence Effects on Wake-Induced Transition on an Axial CompressorBlade
397
W. J. Solomon; G. J. Walker
Experiment to Support the Formulation and Validation of Compressor-Face Boundary Conditions
406
Donald Freund; Miklos Sajben
Adiabatic Interaction of Particles with a Compressible Flow: BasicMechanics
415
Francisco Ruiz
Experimental Investigation of Rotor-Inlet Guide Vane Interactions inTransonic Axial-Flow Compressor
421
Albert J. Sanders; Sanford Fleeter
Evaluating Efficiencies of Turbofan Jet Engines: A Data EnvelopmentAnalysis Approach
431
Sean Bulla; William W. Cooper; Dennis Wilson; Kyung Sam Park
Scarfing and Scalloping Effects on Lobed Forced Mixer at Low-SpeedConditions
440
S. C. M. Yu; Y. Hou; W. K. Chan
Transverse Injection from Circular and Elliptic Nozzles into aSupersonic Crossflow
449
M. R. Gruber; A. S. Nejad; T. H. Chen; J. C. Dutton
Flow of Gel Fuels in Tapered Injectors 458
Shai Rahimi; Benveniste Natan
Streamline Tracing: Technique for Designing Hypersonic Vehicles 465
Frederick S. Billig; Ajay P. Kothari
Wall Drag in Internal Mach-2 Flow with Cavity and TranspirationInjection
472
Linda A. Castiglone; G. Burton Northam; Ned R. Baker; Larry A. Roe
Restricted Shock Separation in Rocket Nozzles 478
Manuel Frey; Gerald Hagemann
Combustor Model for Simulation of Combustion Instabilities and TheirActive Control
485
Rajendran Mohanraj; Yedidia Neumeier; Ben T. Zinn
Convergence of Two Analytical Flowfield Models Predicting aDestabilizing Agent in Rocket Combustion
492
J. Majdalani; G. A. Flandro; T. S. Roh
Nonpremixed Periodic Flames Supported by HeterogeneousPropellants
498
T. L. Jackson; J. Buckmaster
Line-of-Sight Variations of Temperature and Species in Solid PropellantFlames
505
Carl F. Mallery Jr.; Stefan T. Thynell
Flame/Stretch Interactions of Premixed Fuel-Vapor/O2/N2 Flames 513
O. C. Kwon; M. I. Hassan; G. M. Faeth
Ultrasonic Method Applied to Full-Scale Solid Rocket Motors 523
Franck Cauty
Measurements of Ions from High-Current Hollow Cathodes UsingElectrostatic Energy Analyzer
529
Ikuya Kameyama; Paul J. Wilbur
Three-Dimensional Numerical Simulation of Field-Emission-Electric-Propulsion Neutralization
536
M. Tajmar; J. Wang
Volume 16 Number 2 March 2000
Full-Length Papers
Confined Swirling Flows with Heat Release and Mixing 169
David S. Underwood; Ian A. Waitz; Edward M. Greitzer
Numerical Investigation of Twin-Nozzle Rocket Plume Phenomenology 178
Houshang B. Ebrahimi; Jay Levine; Alan Kawasaki
Detailed Chemical-Kinetic Model for Aviation Fuels 187
R. P. Lindstedt; L. Q. Maurice
Thrust Vector Control for (Clustered Modules) Plug Nozzles: SomeConsiderations
196
H. F. R. Schöyer
Optimizing Subcritical-Flow Thrust-Vectoring of Converging-DivergingNozzles
202
Nozzles
Erich A. Wilson; Dan Adler; Benjamin Z. Bal-Or; Valery Sherbaum;Michael Lichtsinder
Direct Computation of Jet Noise Produced by Large-ScaleAxisymmetric Structures
207
R. R. Mankbadi; H. Shih; R. Hixon; L. A. Povinelli
Flowfield near a Mulitiport Injector Array in a Supersonic Flow 216
L. S. Jacobsen; J. A. Schetz; W. F. Ng
Ignition Characteristics of Plasma Torch for Hydrogen Jet in anAirstream
227
Kenichi Takita; Tomokazu Uemoto; Takahiro Sato; Yiguang Ju; GoroMasuya; Katsura Ohwaki
Two-Dimensional Nonadiabatic Injection into a Supersonic Freestream 234
Rodney D. W. Bowersox; K. Colin Tucker; Christopher D. Whitcomb
Propulsion System for Hypersonic Space Planes 243
Michael Zeutzius; Toshiaki Setoguchi; Kunio Terao; Hideo Miyanishi
Pulse Detonation Magnetohydrodynamic Power 251
Ron J. Litchford; Bryan R. Thompson; John T. Lineberry
Magnetocombustion: A Thermodynamic Analysis 263
John Baker; Kozo Saito
Optimization of Ram Accelerator Systems Design 269
Xiaojian Wang; Elyeser Spiegler; Yaakov M. Timnat
Experimental Investigation of the Evaporation of Droplets in AxialAcoustic Fields
278
R. I. Sujith; G. A. Waldherr; J. I. Jagoda; B. T. Zinn
Effect of Inlet Conditions on Endwall Secondary Flows 286
Kristina S. Hermanson; Karen A. Thole
Effect of Inner and Outer Airflow Characteristics on High LiquidPressure Prefilming Airblast Atomization
297
J. S. Chin; N. K. Rizk; M. K. Razdan
Progress in Modeling Pressure Oscillations in Regenerative LiquidPropellant Guns
302
T. P. Coffee
Eulerian Approach for Unsteady Two-Phase Solid Rocket Flows withAluminum Particles
309
Eric Daniel
Combustion Experiments in Hydrogen Peroxide/Polyethylene HybridRocket with Catalytic Ignition
318
E. J. Wernimont; S. D. Heister
Time-Accurate Three-Dimensional Navier-Stokes Analysis of One-and-One-Half Stage Axial-Flow Turbine
327
Thomas W. Volmar; Bernard Brouillet; Heinz E. Gallus; HannesBenetschik
Modeling of Turbine Engine Axial-Flow Compressor and TurbineCharacteristics
336
Marek Orkisz; Slawomir Stawarz
New Gear-Fault-Detection Parameter by Use of Joint Time-FrequencyDistribution
340
V. V. Polyshchuk; F. K. Choy; M. J. Braun
Feasibility Assessment of Thermal Barriers for Extreme TransientTemperatures
347
Bruce M. Steinetz; Patrick H. Dunlap Jr
Numerical Thermal Model of NASA Solar Electric PropulsionTechnology Application Readiness Ion Thruster
357
Jonathan Van Noord; Alec Gallimore; Vincent K. Rawlin
Technical Notes
Joint Jet-A/Silane/Hydrogen Reaction Mechanism 365
Mark J. Lewis; Jee Su Chang
Lithium Peroxide Fuel Cells for Electric Vehicle Propulsion 367
Gautum Agarwal
Simulations of the Flow in Supersonic Turbines with Straight CenterlineNozzles
370
Daniel J. Dorney; Lisa W. Griffin; Karen L. Gundy-Burlet
Burning Behavior of Composite Propellants with Fast-BurningInclusions
374
A. E. Fogelzang; A. P. Denisyuk; V. V. Serushkin; V. Yu. Egorshev; V.P. Sinditskii; A. D. Margolin
Volume 16 Number 1 January 2000
Editorial
Forward into the New Millennium 1
R. H. Woodward Waesche
Reviewers for October 1998-September 1999 6
Editorial Policy Statement on Numerical Accuracy and ExperimentalUncertainty
7
Ethical Standards for Publication of Aeronautics and AstronauticsResearch
8
AIAA Manuscript Review Process 9
Full-Length Papers
Aerodynamic Analysis of an Installed Thrust Reverser 10
Daniel J. Strash; J. Michael Summa; Joel H. Frank; Robert Standish
Numerical Simulations and Planar Laser-Induced FluorescenceImaging Results of Hypersonic Reactive Flows
16
Kazu Toshimitsu; Akiko Matsuo; Michel R. Kamel; Christopher I. Morris;Ronald K. Hanson
Numerical Investigation of Hydrogen Strut Injections into SupersonicAirflows
22
P. Gerlinger; D. Brüggemann
Fuel Injection into a Supersonic Airflow by Means of Pylons 29
C. Gruenig; V. Avrashkov; F. Mayinger
Self-Ignition and Supersonic Reaction of Pylon-Injected Hydrogen Fuel 35
C. Gruenig; V. Avrashkov; F. Mayinger
Incomplete Mixing and Off-Design Effects on Shock-InducedCombustion Ramjet Performance
41
J. P. Sislian; R. Dudebout; J. Schumacher; M. Islam; T. Redford
Three-Dimensional Flow Analysis of Turbine Blade Cascades withLeading-Edge Ejection
49
Dieter Bohn; Volker Becker; Karsten Kusterer; Leonhard Fottner;Sabine Ardey
Trailing-Edge Blowing for Reduction of Turbomachinery Fan Noise 57
J. M. Brookfield; I. A. Waitz
Computational Analysis of Stall and Separation Control in CentrifugalCompressors
65
Alex Stein; Saeid Niazi; L. N. Sankar
Evaluation of Boundary Conditions for the Gust-Cascade Problem 72
R. Hixon; S.-H. Shih; R. R. Mankbadi
Identifying Optimal Fan Compressor Pressure Ratios for the Mixed-Stream Turbofan Engine
79
Paul T. Millhouse; Stuart C. Kramer; Paul I. King; Edward F. Mykytka
Engine Case Externals Challenges and Opportunities 87
Mike Miller; Jeff Colehour; Ken Dunkelberg
Very-Near-Field Plume Investigation of the Anode Layer Thruster 91
Matthew T. Domonkos; Alec D. Gallimore; Colleen M. Marrese; JamesM. Haas
Third Way of Development of Single-Stage-to-Orbit Propulsion 99
V. V. Balepin; M. Maita; S. N. B. Murthy
Ideal Gas Thermodynamic Properties of Propellants and ExplosiveCompounds
105
Alexander Burcat
Mass Production of Antimatter for High-Energy Propulsion 119
Brice N. Cassenti
Regression Rate Behavior of Hybrid Rocket Solid Fuels 125
Martin J. Chiaverini; Nadir Serin; David K. Johnson; Yeu-Cherng Lu;Kenneth K. Kuo; Grant A. Risha
Phase-Stabilized Ammonium Nitrate-Based Propellants Using Binderswith N-N Bonds
133
Charlie Oommen; Sampat R. Jain
Improvements in the Chemical Stability of Double-Base Solid RocketPropellants
139
M. H. Sammour
Technical Notes
Wall Curvature Effects on External Burning in Supersonic Flow 147
Giuseppe Bussi; Dario Pastrone; Lorenzo Casalino
Three-Dimensional Disturbance Vortex Method for SimulatingRotor/Stator Interaction in Turbomachinery
150
Xian Hong Wu; Mao Zhang Chen
Measurements of Turbulent Flow Structure in Supersonic Curved WallBoundary Layers
153
R. D. W. Bowersox; R. C. Wier; D. D. Glawe; S. Gogineni
Trajectory of a Liquid Jet Traversing Subsonic Airstreams 155
Takao Inamura
Preliminary Mass Spectrometry of a Xenon Hollow Cathode 157
Mark W. Crofton
Study of Boundary-Layer Development in a Two-Stage Low-PressureTurbine
160
Daniel J. Dorney; David E. Ashpis; David E. Halstead; David C. Wisler
Technical Comments
Comment on “Triggering of Longitudinal Combustion Instabilities inRocket Motors: Nonlinear Combustion Response”
164
V. S. Burnley; F. E. C. Culick
Reply by the Authors to V. S. Burnley and F. E. C. Culick 165
J. M. Wicker; V. Yang
Comment on “Shock-Loss Model for Transonic and Supersonic AxialCompressors with Curved Blades”
166
N. A. Cumpsty; C. Freeman
Reply by the Author to N. A. Cumpsty and C. Freeman 168
M.T. Schobeiri
Volume 15 Number 5 September 1999
Full-Length Papers
Mixing of Jet Air with a Fuel-Rich, Reacting Crossflow 617
M. Y. Leong; G. S. Samuelsen; J. D. Holdeman
Aerodynamic Synthesis of a Centrifugal Impeller Using ComputationalFluid Dynamics and Measurements
623
L. M. Larosiliere; G. J. Skoch
Surface Pressure Measurements in Supersonic Transverse InjectionFlowfields
633
M. R. Gruber; L. P. Goss
Expansion and Mixing Processes of Underexpanded Supercritical FuelJets Injected into Superheated Conditions
642
Pei-Kuan Wu; Mehrdad Shahnam; Kevin A. Kirkendall; Campbell D.Carter; Abdollah S. Nejad
Vane Row Indexing for Passive Vibration Control of Axial-FlowTurbomachine Rotors
650
Albert J. Sanders; Sanford Fleeter
Probabilistic Analysis of Aircraft Gas Turbine Disk Life and Reliability 658
Matthew E. Melis; Erwin V. Zaretsky; Richard August
Effect of Variable Axial Chord on a Low-Pressure Turbine Blade 667
C. G. Murawski; K. Vafai
Aerodynamic Effects on Blade Vibratory Stress Variations 675
James A. Kenyon; Douglas C. Rabe; Sanford Fleeter
Individual Cylinder Model of a General Aviation Aircraft Engine 681
Gary Parker; Giorgio Rizzoni
Apparent Failure of Scaling Methods in Ramjet Connected-Pipe Testing 689
John A. Blevins; Hugh W. Coleman
Shock-Tunnel Skin-Friction Measurement 699
C. P. Goyne; R. J. Stalker; A. Paull
Air Turborocket/Vehicle Performance Comparison 706
Kirk Christensen
Industrial Constraints for Developing Solid Propellants with EnergeticMaterials
713
Bruno D'Andrea; Francesca Lillo
Methodology for Analysis of Postshock Oscillations During Pulse-Triggered Instability
719
P. G. Harris; A. De Champlain
Technical Notes 729
Volume 15 Number 4 July 2001
Full-Length Papers
Interferometric Study of Unsteady Passing Shock Flow in a TurbineCascade
489
A. Wesner; J. A. Schetz; H. Grabowski
Fixed-Pitch Propeller/Piston Aircraft Operations at Partial Throttle 497
John T. Lowry
Review of Computational Aeroacoustics in Propulsion Systems 504
R. R. Mankbadi
Numerical Study of Cavitation in the Wake of a HypervelocityUnderwater Projectile
513
Richard Saurel; Pierre Cocchi; P. Barry Butler
Influence of Turbulence Modeling on the Performance Prediction forRocket Engine Nozzles
523
Frank A. Haidinger
Hybrid Monte Carlo-Particle-in-Cell Simulation of an Ion Thruster Plume 530
Douglas B. Vangilder; Gabriel I. Font; Iain D. Boyd
Simulation of Unsteady Flow in Nozzle-Ejector Mixer 539
Thomas Z. Dong; Reda R. Mankbadi
Theoretical Analysis and Engineering Modeling of Flowfields inClustered Module Plug Nozzles
544
Francesco Nasuti; Marcello Onofri
Analysis of a Hybrid Dual-Combustion-Chamber Solid-Propellant GasGenerator
552
Jon J. Freesmeier; P. Barry Butler
Dynamic Modeling of Hybrid Rocket Combustion 562
M. Arif Karabeyoglu; D. Altman
Analyses and Application of Gas Sampling to Scramjet Engine Testing 572
Tohru Mitani; Masahiro Takahashi; Sadatake Tomioka; Tetsuo Hiraiwa;Kouichiro Tani
Drags in Scramjet Engine Testing: Experimental and ComputationalFluid Dynamics Studies
578
Tohru Mitani; Takeshi Kanda; Tetsuo Hiraiwa; Yasutaka Igarashi;Kazuhiro Nakahashi
Closed-Loop Active Control of Combustion Instabilities UsingSubharmonic Secondary Fuel Injection
584
C. M. Jones; J. G. Lee; D. A. Santavicca
Reduced Kinetics Mechanisms for Ram Accelerator Combustion 591
Eric L. Petersen; Ronald K. Hanson
Unified Computer Model for Predicting Thermochemical Erosion in GunBarrels
601
S. Sopok; P. O'Hara; G. Pflegl; S. Dunn; D. Coats; G. Nickerson
Technical Note
Determination of Unsteady Heat Release Distribution in UnstableCombustor from Acoustic Pressure Measurements
613
Timothy C. Lieuwen; Yedidia Neumeier; Ben T. Zinn
Volume 15 Number 3 May 1999
Full-Length Papers
Liquid Jet Atomization in a Compressible Gas Stream 369
Tingbao Chen; Xianguo Li
Ion Beamlet Divergence Characteristics of Two-Grid Multiple-Hole Ion-Accelerator Systems
377
Yukio Hayakawa; Shoji Kitamura
Adaptive Control of Combustion Instability with On-Line SystemIdentification
383
Shozo Koshigoe; Toshihiko Komatsuzaki; Vigor Yang
Computation of Vortex Shedding in Solid Rocket Motors Using Time-Dependent Turbulence Model
390
A. Kourta
Performance Evaluation of Scramjet Combustors Using Kinetic Energyand Combustion Efficiencies
401
Goro Masuya; Tomokazu Uemoto; Yoshihiro Wakana; Kenji Kudou;Atsuo Murakami; Tomoyuki Komuro
Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition
408
M. K. Smart
Free-Flight Experiment and Numerical Simulation for Cold ThrusterPlume
417
M. S. Ivanov; G. N. Markelov; Yu. I. Gerasimov; A. N. Krylov; L. V.Mishina; E. I. Sokolov
Startup Modeling of the Receiver of NASA's 2-Kilowatt Solar DynamicPower System
424
Guido W. Lopez
Experimental Investigation of the Role of Downstream Ramps on aSupersonic Injection Plume
432
Mark P. Wilson; Rodney D. W. Bowersox; Diana D. Glawe
Low-Power Helium Pulsed Arcjet 440
Gary F. Willmes; Rodney L. Burton
Comparative Study of Coupled-Mode Flutter-Analysis Methods for FanConfigurations
447
R. Srivastava; T. S. R. Reddy
Predicted Combined Effects of Purge Flow and Rotor-CasingEccentricity on Ingress Heating
454
Zhou Guo; David L. Rhode
Modified Through-Flow Wave-Rotor Cycle with Combustor-BypassDucts
462
Daniel E. Paxson; M. Razi Nalim
Launch Vehicle Dynamic and Control Effects from Solid Rocket MotorSlag Ejection
468
K. W. Dotson; J. W. Murdock; D. K. Kamimoto
Technical Papers
Biharmonic Three-Dimensional Grid Generation for AxialTurbomachinery with Tip Clearance
476
G. A. Gerolymos; G. Tsanga
Technical Notes
Adaptive Analysis of Oscillating Cascade Flows on a Quadrilateral-Triangular Mesh
479
S. Y. Yang
Theoretical Prediction of Mean Droplet Size of Y-Jet Atomizers 481
H. S. Couto; J. A. Carvalho Jr.; M. Q. McQuay; P. T. Lacava
Optimal Performance of Enthalpy Rocket 485
Lorenzo Casalino; Guido Colasurdo
Volume 15 Number 2 – Not AvailableVolume 15 Number 1 – Not AvailableVolume 14 Number 6 – Not Available
Volume 14 Number 5 September 1997
Editorial
Another Landmark Collection 585
R. H. Woodward Waesche
Space Propulsion Development for the 21st Century 586
Xinmin Ren
Preface 587
Vigor Yang; Guoqiu Liu; William E. Anderson; Mohammed Habiballah
Full-Length Papers
Cycles for Earth-to-Orbit Propulsion 588
Detlef Manski; Christoph Goertz; Hagen-D. Saßnick; James R. Hulka;B. David Goracke; Daniel J. H. Levack
Combined Rocket and Airbreathing Propulsion Systems for Space-Launch Applications
605
Russell Daines; Corin Segal
Preliminary Analysis of an Airbreathing and Rocket Combined-CycleEngine
613
Feng Qi; Jue Wang; Chien-Pin Chen
Advanced Rocket Nozzles 620
Gerald Hagemann; Hans Immich; Thong Van Nguyen; Gennady E.Dumnov
Dynamic Amplification of Fluid Pressure in a Propellant Feed Line 635
T. V. Nguyen; W. E. Huffman
Propellant Technologies: Far-Reaching Benefits for Aeronautical andSpace-Vehicle Propulsion
641
Bryan Palaszewski; Leonid S. Ianovski; Patrick Carrick
Propellant Management in Booster and Upper-Stage PropulsionSystems
649
Mark F. Fisher
Liquid-Propellant Rocket Engine Health-Monitoring Techniques 657
Yulin Zhang; Jianjun Wu; Minchao Huang; Hengwei Zhu; Qizhi Chen
Quality Issues in Propulsion 664
John P. McCarty; Garry M. Lyles
Status and Issues Related to In-Space Propulsion Systems 669
R. L. Sackheim; D. C. Byers
Nontoxic Orbital Maneuvering and Reaction Control Systems forReusable Spacecraft
676
Eric Hurlbert; John Applewhite; Tien Nguyen; Brian Reed; ZhangBaojiong; Wang Yue
Baojiong; Wang Yue
Spacecraft Electric Propulsion - An Overview 688
M. Martinez-Sanchez; J. E. Pollard
Electric Propulsion for Solar System Exploration 700
John R. Brophy; Muriel Noca
Ion Thruster Development Trends and Status in the United States 708
Paul J. Wilbur; Vincent K. Rawlin; J. R. Beattie
Pulsed Plasma Thruster 716
R. L. Burton; P. J. Turchi
Main Physical Features and Processes Determining the Performance ofStationary Plasma Thrusters
736
Vladimir Kim
Scaling of Thrust in Self-Field Magnetoplasmadynamic Thrusters 744
Edgar Choueiri
Technology and Application Aspects of Applied FieldMagnetoplasmadynamic Propulsion
754
Gerd Krülle; Monika Auweter-Kurtz; Akihiro Sasoh
High-Power Hydrogen Arcjet Thrusters 764
Monika Auweter-Kurtz; Thomas Gölz; Harald Habiger; Frank Hammer;Helmut Kurtz; Martin Riehle; Christian Sleziona
Experimental Performance of Field Emission Microthrusters 774
Salvo Marcuccio; Angelo Genovese; Mariano Andrenucci
Research as a Key in the Design Methodology of Liquid-PropellantCombustion Devices
782
M. Habiballah; L. Vingert; V. Duthoit; P. Vuillermoz
Investigation of Heat Transfer and Coking Characteristics ofHydrocarbon Fuels
789
Keming Liang; Baoe Yang; Zhongli Zhang
Liquid-Propellant Rocket Engine Injector Dynamics 797
Vladimir G. Bazarov; Vigor Yang
Mixing and Spray Formation in Coaxial Jets 807
Emmanuel Villermaux
Effects of Periodic Atomization on Combustion Instability in Liquid-Fueled Propulsion Systems
818
W. E. Anderson; K. L. Miller; H. M. Ryan; S. Pal; R. J. Santoro; J. L.Dressler
Experimental Investigation of Shear Coaxial Cryogenic Jet Flames 826
S. Candel; G. Herding; R. Synder; P. Scouflaire; C. Rolon; L. Vingert;M. Habiballah; F. Grisch; M. Péalat; P. Bouchardy; D. Stepowski; A.Cessou; P. Colin
Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
835
Wolfgang O. H. Mayer; Axel H. A. Schik; Bruno Vielle; ChristianChauveau; Iskender Gökalp; Douglas G. Talley; Rodger D. Woodward
Chauveau; Iskender Gökalp; Douglas G. Talley; Rodger D. Woodward
Modeling High-Pressure Mixing and Combustion Processes in LiquidRocket Engines
843
Joseph C. Oefelein; Vigor Yang
Technical Notes 858
Volume 14 Number 4 July 1998
Full-Length Papers
Modified Fracture Mechanics Approach in Structural Analysis of Solid-Rocket Motors
409
Sook-Ying Ho; Gerard Carè
Experimental Study on Boron-Potassium Nitrate Initiated by Shock 416
Liqiong Wang; Changgen Feng; Changsheng Han
Measurement System for Determining Solid Propellant Burning RateUsing Transmission Microwave Interferometry
421
Vladica S. Bozic; Djordje D. Blagojevic; Bozidar A. Anicin
429
P. G. Harris; A. De Champlain
Modeling and Estimation for Electromechanical Thrust Vector Control ofRocket Engines
440
Dale E. Schinstock; Douglas A. Scott; Tim A. Haskew
Investigation of a Solid Fuel Scramjet Combustor 447
Adela Ben-Yakar; Benveniste Natan; Alon Gany
Flame-Holding Configurations for Kerosene Combustion in a Mach 1.8Airflow
456
Michael G. Owens; Sharam Tehranian; Corin Segal; Viatcheslav A.Vinogradov
New Model for Intense Self-Similar Vortices 462
Georgios H. Vatistas
Shock-Loss Model for Transonic and Supersonic Axial Compressorswith Curved Blades
470
M. T. Schobeiri
Properties of Laminar Premixed Hydrocarbon/Air Flames at VariousPressures
479
M. I. Hassan; K. T. Aung; O. C. Kwon; G. M. Faeth
Strategies for Pulsed Detonation Engine Performance Optimization 489
J.-L. Cambier; J. K. Tegnér
Reflections on Free-Piston Stirling Engines, Part 1: Cyclic SteadyOperation
499
F. De Monte; G. Benvenuto
Reflections on Free-Piston Stirling Engines, Part 2: Stable Operation 509
F. De Monte; G. Benvenuto
Generic Magnetic Fusion Rocket Model 519
John F. Santarius; B. Grant Logan
Simplified Approach to Performance Evaluation of Nuclear andElectrical Propulsion Systems
525
Fernando De Souza Costa; João Andrade De Carvalho Jr
Vortex Formation and Stability in a Scaled Gas-Core Nuclear RocketConfiguration
530
L. E. Thode; M. C. Cline; S. D. Howe
Slingatron Mass Launchers 537
Derek A. Tidman
Effect of Propellant Temperature on Efficiency in the Pulsed PlasmaThruster
545
Gregory G. Spanjers; Jamie B. Malak; Robert J. Leiweke; Ronald A.Spores
Propellant Losses Because of Particulate Emission in a Pulsed PlasmaThruster
554
Gregory G. Spanjers; Jason S. Lotspeich; Keith A. McFall; Ronald A.Spores
Arcjet Anode Plasma Measurements Using Electrostatic Probes 560
Nicholas T. Tiliakos; Rodney L. Burton; Herman Krier
Beamlet Profiles from Multiple-Hole Ion-Extraction Systems 568
Yukio Hayakawa; Shoji Kitamura; Katsuhiro Miyazaki
Technical Notes 575
Volume 14 Number 3 May 1998
Full-Length Papers
Study on Trapped-Vortex Combustor - Effect of Injection on FlowDynamics
273
Viswanath R. Katta; W. M. Roquemore
Transition Characteristics of Flowfield in a Simulated Solid-RocketMotor
282
Tong-Miin Liou; Wan-Yih Lien; Po-Wen Hwang
Determination of Pressure Dependence of Burning Rate in Solid MotorsUsing Ultrasonic Technique
290
Desh Deepak; R. Jeenu; P. Sridharan; M. S. Padmanabhan
Effect of Catalyst Addition on Subatmospheric Burning SurfaceTemperature of Composite Propellants
295
S. Krishnan; R. D. Swami
Temperature and Species Measurements in a Low-ThrustHydrogen/Oxygen Rocket Engine
301
Wilhelmus A. de Groot
Model of Turbulent Mixing and Reaction for H2-Air Combustion 309
Marc A. Cremer; Patrick A. McMurtry
Methodology to Solve Flowfields of Plug Nozzles for Future Launchers 318
Francesco Nasuti; Marcello Onofri
Transport-Property Measurements in the Plume of an SPT-100 HallThruster
327
Lyon B. King; Alec D. Gallimore; Colleen M. Marrese
Surface Modification Measurements in the T5 Ion Thruster Plume 336
L. Najeeb Ahmed; Mark W. Crofton
Load Oscillations Caused by Unstart of Hypersonic Wind Tunnels andEngines
348
Takashi Shimura; Tohru Mitani; Noboru Sakuranaka; Muneo Izumikawa
Symmetry Approach to Extension of Flutter Boundaries via Mistuning 354
B. Shapiro
Numerical Simulation of Incompressible Two-Blade Rotor Flowfields 367
John A. Ekaterinaris
Stability Behavior of a Shaft-Disk System Subjected to LongitudinalForce
375
Lien-Wen Chen; Hong-Cheng Sheu
Heat Transfer in Counterswirled Coaxial Jet Mixing 384
J. L. Sanger; P. A. Dellenback
Sound-Pressure-Level Variations in a Supersonic Rectangular Cavity atYaw
392
Peter J. Disimile; Paul D. Orkwis
Application of Two-Variable Fuzzy-PI Control in an Aeroengine 399
Fang Zhongxiang; Wu Chihua
Analysis of Ar-Cs Magnetohydrodynamics Disk Generator with StrongInteraction
403
Motoo Ishikawa; Takuro Shiomi; Yoshitaka Inui; Hiroyuki Yamasaki
Volume 14 Number 2 March 1998
Full-Length Papers
Jet-Engine Test Cell Augmenter Performance 129
C. A. Kodres; G. L. Murphy
Comparison of Physical and Aerodynamic Ramps as Fuel Injectors inSupersonic Flow
135
Raymond P. Fuller; Pei-Kuan Wu; Abdollah S. Nejad; Joseph A. Schetz
Investigation of Cryogenic Propellant Flames Using ComputerizedTomography of Emission Images
146
Gerald Herding; Ray Snyder; Carlos Rolon; Sebastien Candel
Competitive Reactivity of Stabilizers and Ballistic Modifiers DuringSimulated Aging of Propellants
152
M. H. Sammour
Leading-Edge Flame Detachment: Effect on Pressure-CoupledCombustion Response
160
C. A. Beiter; E. W. Price
Ignition Dynamics of Boron Particles in a Shock Tube 166
Herman Krier; R. L. Burton; M. J. Spalding; T. J. Rood
Spray Structures of Liquid Jets Atomized in Subsonic Crossflows 173
Pei-Kuan Wu; Kevin A. Kirkendall; Raymond P. Fuller; Abdollah S.Nejad
Three-Dimensional Turbine Rotor Forcing Functions and Linear TheoryAnalysis
183
David A. Johnston; Sanford Fleeter
Measured Rotor Wake and Potential Forcing Functions, Including BladeRow Interactions
191
Robert T. Johnston; John M. Feiereisen; Sanford Fleeter
Blading Response to Potential Field Interactions in Axial- and Radial-Flow Turbomachinery
199
Albert J. Sanders; Sanford Fleeter
Preliminary Estimation of Engine Gas-Flow-Path Size and Weight 208
Vivek Sanghi; S. Kishore Kumar; V. Sundararajan; S. K. Sane
Wake Decay: Effect of Freestream Swirl 215
J. M. Brookfield; I. A. Waitz; J. Sell
Aerodynamic Shape Optimization of a Subsonic Inlet Using Three-Dimensional Euler Computation
225
D. R. Reddy; E. S. Reddy; R. E. Moody
Overexpanded Two-Dimensional Convergent-Divergent NozzlePerformance, Effects of Three-Dimensional Flow Interactions
234
A. Hamed; C. Vogiatzis
Aerodynamics Performance Prediction of Thrust-Vectoring Nozzles 241
A. Matesanz; A. Velazquez; M. Rodriguez
Propellant Utilization in Hall Thrusters 247
Y. Raitses; J. Ashkenazy; M. Guelman
Quasisteady Ablative Magnetoplasmadynamic Thruster Performancewith Different Propellants
254
Giorgio Paccani; Ugo Chiarotti; William D. Deininger
Laser Propulsion System for Space Vehicles 261
Aviad Brandstein; Yeshayahou Levy
Technical Notes
Rocket Propulsion Strategy Based on Kinetic Energy Management 270
Merrill K. King
Volume 14 Number 1 January 1998
Editorial 1
Full-Length Papers
Reacting Flow Establishment in Ram Accelerators: A Numerical Study 10
S. Yungster; K. Radhakrishnan; M. J. Rabinowitz
Control of Flame-Holding in Supersonic Airflow by Secondary AirInjection
18
Shuhei Takahashi; Naohiro Sato; Mitsuhiro Tsue; Michikata Kono;Masahiko Nakamura; Hiroshi Kondo; Yasushige Ujiie
Improved Physics Model for the Gasdynamic Mirror Fusion PropulsionSystem
24
Terry Kammash; David L. Galbraith
Modeling Plasma Processes in 1-Kilowatt Hydrazine Arcjet Thrusters 29
Thomas W. Megli; Junqing Lu; Herman Krier; Rodney L. Burton
Thermal Decomposition of 3,3_-Bis-Azidomethyl-Oxetane 37
Young Joo Lee; Ching-Jen Tang; Gautam Kudva; Thomas A. Litzinger
Droplet Combustion, Microexplosion, and Sooting Characteristics ofSeveral Energetic Liquid Propellants
45
T. X. Li; D. L. Zhu; C. K. Law
Characterization of Fuel Regression in a Radial Flow Hybrid Rocket 51
J. R. Caravella Jr; S. D. Heister; E. J. Wernimont
Characteristics of a Trapped-Vortex Combustor 57
K.-Y. Hsu; L. P. Goss; W. M. Roquemore
Assessment of a Radiative Heat Transfer Model for Gas TurbineCombustor Preliminary Design
66
Peter J. Stuttaford; Philip A. Rubini
Digital Simulator for Steady-State Performance Prediction of MilitaryTurbofan Engine
74
Vivek Sanghi; B. K. Lakshmanan; V. Sundararajan
Influence of Inlet Pressure Distortion on a Convertible Engine Fan 82
Tarik Kaya
Numerical Investigation of Inlet Buzz Flow 90
Pong-Jeu Lu; Ling-Tzong Jain
Method for Noise Suppressing Nozzle Calculation and First Results ofIts Implementation
101
S. Bosniakov; S. Fonov; V. Jitenev; A. Shenkin; V. Vlasenko; N.Yatskevich
Experimental Analysis of the Turbulent Shear Stresses for DistortedSupersonic Boundary Layers
110
Joel J. Luker; Chad S. Hale; Rodney D. W. Bowersox
Solar Cell Temperature on Mars 119
E. Matz; J. Appelbaum; Y. Taitel; D. J. Flood
Mars Dust-Removal Technology 126
Geoffrey A. Landis
Volume 13 Number 6 November 2001
FULL-LENGTH PAPERS
Study of a Supersonic Combustor Employing Swept Ramp FuelInjectors
697
Dean R. Eklund; Scott D. Stouffer; G. Burton Northam
Open-Loop Performance of a Fast-Response, Actively Controlled FuelInjector Actuator
705
Yedidia Neumeier; Aharon Nabi; Amos Arbel; Moti Vertzberger; Ben T.Zinn
Effects of Inlet Configuration on Ignition and Fuel Regression Behind aBackstep
714
Cliff Yuh-Yih Wu; Jing-Tang Yang
Laser-Induced Spark Flameholding in Supercritical, Subsonic Flow 721
Lara D. Medoff; Andrew McIlroy
Uncertainty Assessment of Ramjet Performance Determination inConnected-Pipe Testing
730
John A. Blevins; Hugh W. Coleman
Assessment of Jet Noise Analysis Codes for Multistream Axisymmetricand Forced Mixer Nozzles
737
T. J. Barber; L. M. Chiappetta; S. H. Zysman
Zonal Approach for Prediction of Jet Noise 745
S. H. Shih; D. R. Hixon; R. R. Mankbadi
Effect of Wall Roughness on the Flow Through Converging - DivergingNozzles
753
Venkata S. Krishnamurty; Wei Shyy
Absolute Instability in a Supersonic Shear Layer and Mixing Control 763
Long-Shin Lee; Philip J. Morris
Velocity and Temperature Measurements in a Low-Power HydrazineArcjet
768
S. A. Bufton; R. L. Burton
Extensive Validation of a Monte Carlo Model for Hydrogen ArcjetFlowfields
775
Iain D. Boyd
Measurements of Electron Density in the Charge Exchange Plasma ofan Ion Thruster
783
P. C. T. De Boer
Numerical Analysis of a Two-Dimensional MagnetoplasmadynamicArcjet
789
I. Funaki; K. Toki; K. Kuriki
Prediction of Pressurant Mass Requirements for Axisymmetric LiquidHydrogen Tanks
796
Neil T. Van Dresar
TECHNICAL NOTES
Cored Brick Storage Heater Analysis 800
Robert H. Korkegi
Operation of Quasi-Two-Dimensional Projectiles in a Ram Accelerator 802
Xinyu Chang; Andrew Higgins; Eric Schultz; Adam Bruckner
Further Examination of Enthalpy Rocket Performance 804
Merrill K. King
Effects of Kinetic Rate Uncertainty on the Predicted Performance ofSolar Thermal Rockets
806
D. Brian Landrum; Robert M. Beard
Off-Design Performance Prediction of Single-Spool Turbojets UsingGasdynamics
808
Mirza F. Baig; H. I. H. Saravanamuttoo
ERRATA
Compatibility of Gelled Inhibited Red Fuming Nitric Acid with AluminumAlloys
811
Barry D. Allan; and
Volume 13 Number 5 September 2001
FULL-LENGTH PAPERS
Challenge to Create the Space Drive 577
Marc G. Millis
Performance Limits for Projectile Flight in the Ram and ExternalPropulsion Accelerators
583
J. Rom
Performance Optimization of a Supersonic Combustion RamAccelerator Projectile
592
John W. Sabean; Mark J. Lewis
Analytical Solution of the Type IV Shock Interaction 601
Michael J. Frame; Mark J. Lewis
Applications of Algebraic Reynolds Stress Turbulence Models Part 1:Incompressible Flat Plate
610
John R. Carlson
Applications of Algebraic Reynolds Stress Turbulence Models Part 2:Transonic Shock-Separated Afterbody
620
John R. Carlson
Plug Nozzle Flowfield Analysis 629
T. Rommel; G. Hagemann; C.-A. Schley; G. Krülle; D. Manski
Comparison of Scramjet Engine Performance in Mach 6 Vitiated andStorage-Heated Air
635
Tohru Mitani; Tetsuo Hiraiwa; Shigeru Sato; Sadatake Tomioka;Takeshi Kanda; Kouichiro Tani
Flammability Limits and Probability Density Functions in SimulatedSolid-Fuel Ramjet Combustors
643
Tong-Miin Liou; Wan-Yih Lien; Po-Wen Hwang
Performance and Acceleration Process of QuasisteadyMagnetoplasmadynamic Arcjets with Applied Magnetic Fields
651
Hirokazu Tahara; Yoichi Kagaya; Takao Yoshikawa
Experimental Study of Hydrogen Heating in Powerful Electric DischargeLauncher
659
Ph. G. Rutberg; A. A. Bogomaz; A. V. Budin; V. A. Kolikov; A. G.Kuprin; A. A. Pozubenkov
Jet Engine Component Maps for Performance Modeling and Diagnosis 665
G. Sieros; A. Stamatis; K. Mathioudakis
High-Temperature Braided Rope Seals for Static Sealing Applications 675
Bruce M. Steinetz; Michael L. Adams; Paul A. Bartolotta; Ram Darolia;Andrew Olsen
Identification of Continuous-Time, Linear, and Nonlinear Models of anElectromechanical Actuator
683
Dale E. Schinstock; Tim A. Haskew
Theoretical Formulation for Sauter Mean Diameter of Pressure-SwirlAtomizers
691
H. S. Couto; J. A. Carvalho Jr; D. Bastos-Netto
Volume 13 Number 4 July 1997
FULL-LENGTH PAPERS
Measurement System for Determining Solid Rocket Propellant BurningRate Using Reflection Microwave Interferometry
457
Vladica S. Bozic; Djordje Dj. Blagojevi; Bozidar A. Anicin
High-Speed Photographic Study of the Impact Response of AmmoniumDinitramide and Glycidyl Azide Polymer
463
J. P. Agrawal; S. M. Walley; J. E. Field
Mechanism of Burning Rate Enhancement of Composite SolidPropellants by Ferric Oxide
471
Satyanarayanan R. Chakravarthy; Edward W. Price; Robert K. Sigman
Compatibility of Gelled Inhibited Red Fuming Nitric Acid with AluminumAlloys
481
Ramona E. Arndt Hallit; Clark W. Hawk
Experimental Study on Rotating Cavitation of Rocket Propellant PumpInducers
488
T. Hashimoto; M. Yoshida; M. Watanabe
Hybrid Friction - Impact Vibration Damper for Cryogenic RotatingMachinery
495
J. Jeffrey Moore; Alan B.; Ravindera K. Gadangi
Mean Stator Loading Effect on the Acoustic Response of a RotatingCascade
502
Scott Sawyer; Sanford Fleeter
Macroscopic Balance Model for Wave Rotors 508
Gerard E. Welch
Turbulent Mixing of Coaxial Nozzle Flows with a Central-Lobed Mixer 517
S. C. M. Yu; X. G. Xu
Effects of Mixing Schemes on Kerosene Combustion in a SupersonicAirstream
525
M. Owens; C. Segal; A. H. Auslender
Hydrogen Autoignition and Combustion in Supersonic Flow at LowEquivalence Ratio
532
Giulio Riva; Giambattista Daminelli; Adolfo Reggiori
Experimental Studies on Self-Ignition of Hydrogen/Air SupersonicCombustion
538
Li Jian-Guo; Yu Gong; Zhang Yue; Li Ying; Qian Da-Xing
Mach 6 Testing of a Scramjet Engine Model 543
Takeshi Kanda; Tetsuo Hiraiwa; Tohru Mitani; Sadatake Tomioka;Nobuo Chinzei
Uncertainty Assessment of Performance Evaluation Methods for SolarThermal Absorber/Thruster Testing
552
Pete Markopoulos; Hugh W. Coleman; Clark W. Hawk
Solar Space Power System Optimization with Ultralight Radiator 560
A. F. Massardo; L. A. Tagliafico; M. Fossa; A. Agazzani
Biphase Inverter Based on Cesium Plasma Switches 565
N. I. Alekseyev; V. B. Kaplan; A. M. Martsinovskij; S. V. Electrov
United States Laboratory Element Electrical Power System VerificationApproach
570
Herb W. Wallen; S. Johnny Fu
TECHNICAL NOTES
Thrust Enhancement in Hypervelocity Nozzles by Chemical Catalysis 574
D. J. Singh; Mark H. Carpenter; J. P. Drummond
Volume 13 Number 3 May 1997
Full-Length Papers
Unsteady Aerodynamic Flow Phenomena in a Transonic CompressorStage
329
Chunnil Hah; Steven L. Puterbaugh; William W. Copenhaver
Modular Prediction Scheme for Blade Row Interaction Noise 334
A. B. Parry
Skin-Friction Predictions in a Crossing-Shock Turbulent Interaction 342
Datta Gaitonde; J. S. Shang
Stability Testing of Full-Scale Tactical Motors 349
F. S. Blomshield; J. E. Crump; H. B. Mathes; Richard A. Stalnaker; M.W. Beckstead
Nonlinear Stability Testing of Full-Scale Tactical Motors 356
F. S. Blomshield; H. B. Mathes; J. E. Crump; C. A. Beiter; M. W.Beckstead
Beckstead
Modeling and Experiments of Laser-Induced Ignition of NitraminePropellants
367
S. J. Ritchie; S. T. Thynell; K. K. Kuo
Improvements to Steady-State Combustion Modeling ofCyclotrimethylenetrinitramine
375
Jeffrey E. Davidson; M. W. Beckstead
Fiber-Optic Probe for Laser-Induced Fluorescence Measurements ofthe Fuel-Air Distribution in Gas-Turbine Combustors
384
Jong Guen Lee; Domenic A. Santavicca
Optical and Pressure Measurements in Shock Tunnel Testing of aModel Scramjet Combustor
388
T. J. McIntyre; A. F. P. Houwing; P. C. Palma; P. A. B. Rabbath; J. S.Fox
Comparison of Potential Fuels for Martian Rockets Using CO2 395
Evgeny Ya. Shafirovich; Udo I. Goldshleger
Partial Differential Equation Surface Generation and Functional ShapeOptimization of a Swirl Port
398
C. W. Dekanski; M. I. G. Bloor; M. J. Wilson
Thermal Analysis of the Heat Exchangers and Regenerator in StirlingCycle Machines
404
Filippo de Monte
Counterflow Thrust Vector Control of Subsonic Jets: Continuous andBistable Regimes
412
M. R. Van der Veer; P. J. Strykowski
High-Thrust-High-Specific Impulse Gasdynamic Fusion PropulsionSystem
421
Terry Kammash; Myoung-Jae Lee; David I. Poston
Antiproton Catalyzed Fusion Propulsion for Interplanetary Missions 428
B. N. Cassenti; T. Kammash; D. L. Galbraith
Fundamental Constraints on Large-Scale Antimatter Rocket Propulsion 435
Todd H. Rider
Technical Notes
Overexpanded Two-Dimensional-Convergent-Divergent Nozzle FlowSimulations, Assessment of Turbulence Models
444
A. Hamed; C. Vogiatzis
Lobed Mixers Using Simultaneous Laser-Induced Fluorescence andMie Scattering
445
David M. Milam; Mo Samimy; Steven Martens
Combustion and Microexplosion of Han-Based Liquid Gun Propellantsat Elevated Pressures
448
C. Call; D. L. Zhu; C. K. Law; S. C. Deevi
Interpretation of Finite Element Analysis Results of ScramacceleratorThrust
451
Josef Rom; Mark J. Lewis
Technical Comments
Comment on "Intrinsic Combustion Instability of Solid EnergeticMaterials"
454
M. Q. Brewster; S. F. Son
Reply by the Author to M. Q. Brewster and S. F. Son 456
L. DeLuca
Volume 13 Number 2 March 1997
Full-Length Papers
Exit Flowfield of an Embedded Stator in a Multistage Axial FlowCompressor
169
J. Prato; B. Lakshminarayana; N. Suryavamshi
Gust Response Decomposition in a Stator/Rotor Axial Compressor withVarying Axial Gap
178
Andrew M. Wo; Meng-Hsuan Chung; Shu-Tzung Hsu
Multiple-Scales Solution to the Acoustic Boundary Layer in SolidRocket Motors
186
J. Majdalani; W. K. van Moorhem
Flow Analysis of a Solid Propellant Rocket Motor with Aft Fins 194
Bruno Chaouat
Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at theSegment Interfaces
197
K. W. Dotson; S. Koshigoe; K. K. Pace
Effect of Catalyst Mixing Procedure on Subatmospheric CombustionCharacteristics of Composite Propellants
207
S. Krishnan; R. D. Swami
Combustion Initiated by a Porous Ceramic Regenerator in aReciprocating Engine Environment
213
Steven Sepka; Francisco Ruiz
Monte Carlo Probability Density Function Method for Gas TurbineCombustor Flowfield Predictions
218
Anil K. Tolpadi; Sanjay M. Correa; David L. Burrus; Hukam C. Mongia
Partially Premixed Laminar Gas Flames from Triangular Burners 226
S. R. Gollahalli; Samir Subba
Counterflow Diffusion Flame of Methane and Methane/Hydrogen MixedFuel in Supersonic Flow
233
Kenichi Takita; Takashi Niioka
Properties of Laminar Premixed CO/H2/Air Flames at VariousPressures
239
M. I. Hassan; K. T. Aung; G. M. Faeth
Ignition Characteristics of a New High-Energy Density Fuel in High-Speed Flows
246
C. Segal; M. J. Friedauer; H. S. Udaykumar; W. Shyy; A. P. Marchand
Spray Characteristics of Liquid Jet Traversing Subsonic Airstreams 250
Takao Inamura; Nobuki Nagai
Normal, Sonic Helium Injection Through a Wedge-Shaped Orifice intoSupersonic Flow
257
Matthew J. Barber; Joseph A. Schetz; Larry A. Roe
Velocity Measurements of a Jet Injected into a Supersonic Crossflow 264
Juan Gabriel Santiago; J. Craig Dutton
Fuel Stagnation Temperature Effects on Mixing with SupersonicCombustion Flows
274
M. N. Wendt; R. J. Stalker; P. A. Jacobs
Thrust Losses in Hypersonic Engines Part 1: Methodology 281
D. W. Riggins; C. R. McClinton; P. H. Vitt
Thrust Losses in Hypersonic Engines Part 2: Applications 288
D. W. Riggins
Evaluation of Performance Loss Methods for High-Speed Engines andEngine Components
296
D. W. Riggins
Mixing Characteristics of Forced Mixers with Scalloped Lobes 305
Simon C. M. Yu; T. H. Yip; C. Y. Liu
Flow Through a Rectangular-to-Semiannular Diffusing Transition Duct 312
Jeff Foster; Bruce J. Wendt; Bruce A. Reichert; Theodore H. Okiishi
Power System Analysis of Multikilowatt Space/Planet Stations 318
George L. Kusic; Ronald C. Cull
Technical Notes 324
Volume 13 Number 1 January 1997
Editorial 1
Full-Length Papers
Analytical Model of Unsteady Shock Motion on Hypersonic Forebodies 10
Sowmyalatha Jayaraman; Mark J. Lewis
Unsteady Flow and Shock Motion in a Transonic Compressor Rotor 17
W. W. Copenhaver; S. L. Puterbaugh; C. Hah
Tip Clearance Flow-Shock Interaction in a Transonic Compressor Rotor 24
S. L. Puterbaugh; M. Brendel
Computational Study of Rotating-Stall Inception in Axial Compressors 31
L. He
Chordwise Bending Cascade Unsteady Aerodynamics by anExperimental Influence Coefficient Technique
39
Daniel A. Ehrlich; Sanford Fleeter
Secondary Flow Computation Using an Inviscid Multigrid Finite VolumeLambda Formulation
49
Francesco Casalini; Andrea Dadone
Tangential Injection from Overlaid Slots into a Supersonic Stream 59
David P. Lewis; Joseph A. Schetz
Breakup Processes of Liquid Jets in Subsonic Crossflows 64
Pei-Kuan Wu; Kevin A. Kirkendall; Raymond P. Fuller; Abdollah S.Nejad
Stability of Thin Liquid Sheet Flows 74
Marc W. McConley; Donald L. Chubb; Matthew S. McMaster; AbdollahA. Afjeh
Effect of Acoustic Perturbations on Liquid Jet Atomization 82
S. D. Heister; M. W. Rutz; J. H. Hilbing
Droplet Autoignition in a Reactive Oxidant/Fuel-Vapor/InertEnvironment
89
Xianguo Li
Mass-Flux-Based Implicit Multigrid Method for ModelingMultidimensional Combustion
97
Xiaoqing Zheng; Changming Liao; Zhining Liu; Chaoqun Liu
Comparison Between Presumed and Monte Carlo Probability DensityFunction Combustion Models
109
Fernando Biagioli
Prediction of Soot Emissions in Gas-Turbine Combustors 117
A. de Champlain; D. Kretschmer; J. Tsogo; G. F. Pearce
Multidimensional Modeling of Fuel Effects and Split Injections on DieselEngine Cold-Starting
123
Nabil S. Ayoub; Rolf D. Reitz
Numerical Study of Hypervelocity Flows Through a ScramjetCombustor
131
R. Krishnamurthy; R. C. Rogers; S. N. Tiwari
Experimental Studies on Piloted Supersonic Combustion Using thePetal Nozzle
142
Anil K. Narayanan; K. A. Damodaran
Mixed Integer Programming-Based Power Scheduler for the SpaceStation
150
James Momoh; D. Chattopadhyay; James L. Dolce
Optimal Control of Quasi-One-Dimensional Self-FieldMagnetoplasmadynamic Arcjet Flowfields
157
Kyoichiro Toki
Technical Notes 162
Technical Comments 167