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A Collection of the
41st AIAA/ASME/ASCE/AHS/ASC
Structures, Structural Dynamics, and
Materials Conference and Exhibit
AIAA/ASME/AHS Adaptive Structures Forum
AIAA Non-Deterministic Approaches Forum
AIAA Space Inflatables Forum
AIAA Dynamics Specialists Conference
Volume 1
PART 2
Atlanta, GA
3-6 April 2000UB/TIB Hannover 89
120 945 290
3-6 April 2000
Innovative Passive Mechanisms for Control of Sound in a Launch
Vehicle Fairing 741
Clark, Robert L
Griffin, Steven
Gussy, Joel
Kemp, Jonathan D
Lane, Steven AAIA Paper #2000-1436
Validation of Structural Dynamics Models at Los Alamos
National Laboratory 749
Doeblmg, Scott W
Hemez, Francois M AAIA Paper #2000-1437
A Dynamic Finite Element (DFE) Formulation for Coupled Flap-Lab Vibrations
of Propeller Blades 764
Golnaraghi, M F
Hashemi, SeyecJ Mohammad AAIA Paper #2000-1438
A Complex Velocity Solution fo the Flutter Equations N/APitt, Dale M AAIA Paper #2000-1445
Reduced-Order Modeling for Flutter Prediction 773
Beran, Philip S
Pettit, Chris L AAIA Paper #2000-1446
Energy Based Design andAnalysis of Staggered Solvers for Nonlinear Transient
Aeroelastic Problems 784
Farhat, Charbel
Piperno, Serge AAIA Paper #2000-1447
On the Importance ofAerodynamic and Structural Geometric Nonlinearities on
Aeroelastic Behavior of High-Aspect-Ratio Wings 799
Hodges, DeweyPatil, Mayuresh AAIA Paper #2000-1448
Conservative Interpretation of Aerodynamic Loads for
Aeroelastic Compuations N/AHabashi, WG
Lepage, C Y AAIA Paper #2000-1449
Improving the AerodynamicApproximation in Linear Aeroelasticity ..810
Gin, JagannathHartley, DaytonJadic, loan AAIA Paper #2000-1450
Effect of Spar-Rib Orientation on Strain Energy in the Roll Maneuver of a
Wing without Ailerons N/AKnot Narendra S
Veley, Duane E AAIA Paper #2000-1451
American Institute ofAeronautics and Astronautics
3-6 April 2000 Table of Contents - xiii
Evaluation of Equivalent Laminated Plate Solution (ELAPS) in HSCT Sizing N/ABecker, Bradley T
Bhatia, Kumar G
Boyd, William N
Henderson, Joseph L
Nazan, Mark M
Stone, Steven C AAIA Paper #2000-1452
Aeroservoelastic Structural and Control Optimization Using Classical and
Modern Robust Design Schemes 819
Idan, Moshe
Karpel, MordechayMoulin, Boris AAIA Paper #2000-1453
Global-Local Analysis and Optimization of a Composite Tilt-Rotor Wing 829
Clements, Timothy M
Rais-Rohani, Masoud AAIA Paper #2000-1454
Multi-body Dynamics Metamodels for System Level Studies of New
Tilt-Rotor Technologies N/A
Baker, Andrew
Bauchau, Olivier
Mavns, Dimitn
Volovoi, Vitah AAIA Paper #2000-1455
Designing Turbine Blade Internal Cooling Passages Using Response Surface
and Kriging Methodologies N/ADonahoo, Eric E
Simpson, Tim AAIA Paper #2000-1456
Secondary Buckling of Laminated Composite Plates 839
Hyer, M WTiwan, Nachiketa AAIA Paper #2000-1457
A Comparison of Three Algorithms for Tracing Nonlinear Equilibrium Paths
of Structural Systems 850
Gurdal, Z
Ragon, S A
Watson, L T AAIA Paper #2000-1458
Prebuckling and Postbuckling Response of Tailored Composite Stiffened
Panels with Axial-Shear Coupling N/A
Hyer, Michael W
Starnes, James H
Young, Richard D AAIA Paper #2000-1459
Controlling a Nonlinear Solution Procedure During a Progressive
Failure Analysis -861
Brogan, Frank A
Knight, Norman F
Rankin, Charles C AAIA Paper #2000-1460
American Institute of Aeronautics and Astronautics
3-6 April 2000
On Budiansky's Problem in Nonlinear Stochastic Buckling N/AElishakoff, I AAIA Paper #2000-1461
Effect of Residual Stresses on Buckling Localization in a Cylindrical Panel......872Needleman, A.
Tvergaard, V. AAIA Paper #2000-1462
The Development and Application of Titanium 6 AI-4V ELI Beta
Annealed Investment Castings to Fracture Critical Structure of the
F-22 Air Dominance Fighter N/ALane, Jan
Smith, Paul
Gallager, Mike
Travinski, David
Phelps, Henry AAIA Paper #2000-1463
Inclusions in T1-6AI-4V Investment Castings 879Clark, LarryCotton, James
Reinhart, Theodore R.
Spear, Steve
Strabel, G.
Veeck, S. AAIA Paper #2000-1464
Titanium Alloy Sructures for Air Frame Application by Laser
Forming Process N/AArcella, Frank AAIA Paper #2000-1465
Electron Beam Welding of F-22 Structures 888
Zenas, R AAIA Paper #2000-1466
Effects of Dent Removal on the Design Properties of Fuselage Skin Material.... 891Simmons, Frank
Veciana, Jose A.
Wallace, John AAIA Paper #2000-1467
Aluminum Alloys for the Transport Industry: Environmental Degradationand Microstructure Relationship N/A
Alvarez, Alex
Froes, F.H. AAIA Paper #2000-1468
Analysis and Testing of Extension Twist Coupled Composites UsingSymmetric Configurations 902
Armanios, Erian
Gregory, Richard O.
Schleisman, Mike AAIA Paper #2000-1469
American Institute ofAeronautics and Astronautics
3-6 April 2000 Table of Contents - xv
Characteristic-Mode-Based Component Mode Synthesis for Power Flow
Analysis of Complex Structures 908
Castanier, Matthew P
Pierre, ChnstopheTan, Yung-Chang AAIA Paper #2000-1470
Nonlinear Responses of Symmetrically Laminated CompositeCantilever Beams 918
Arafat, H N
Nayfeh,A H AAIA Paper #2000-1471
Predicting the Impact Response ofan Energy-Absorbing CompositeSubfloor Beam 929
Kellas, Sotins
Knight, Norman F
Pmson, Larry D AAIA Paper #2000-1472
Passively Damped Vibration of Composite Plates with Zig-Zag Elements 940
Kosmatka, J B AAIA Paper #2000-1473
Impact Sound Realization of Composite Structures 951
Hwang, Joon Seok
Kim, Seung Jo
Song, Jun Young AAIA Paper #2000-1474
A Higher-Order Sandwich Plate TheoryAccounting for 3-D Stresses 960
Pai, P Frank
Palazotto, Anthony N AAIA Paper #2000-1475
Composite Grid Structure with Near-Zero Thermally Induced Deflection 971
Kim, Chang Keun
Lee, Hyung Ju
Park, Hoon Cheol
Yoon, Kwang Joon AAIA Paper #2000-1476
Nonlinear Analysis of the Cured Shape and Residual Stress of Unsymmetric
Composite Laminates • 977
Cho, MaenghyoYoo, Seungwoo AAIA Paper #2000-1477
PACKS: A Structural Definition Process for Composites N/AHale, RD
Miller, N F
Vasey-Glandon, V M AAIA Paper #2000-1478
Theory of Anisotropic Beams with Hygrothermal Effects and
Integral Actuators N/A
Badir, Ashraf AAIA Paper #2000-1479
American Institute of Aeronautics and Astronautics
3-6 April 2000
Modified Short Beam Shear Test for Measurement of Interlaminar
Shear Strength • N/AAbali, Felix
Shivakumar, Kunigal AAIA Paper #2000-1480
Innovative Deployable Antenna Developments Using Tensegrity Design 984
Crane, Carl D
Duffy, JosephKnight, Byron F
Rooney, Joseph AAIA Paper #2000-1481
Method for Evaluating the Deployment Characteristics of a
Modular-type Reflector N/AAndo, Kazuhide
Ishikawa, Hironon
Watanabe, Mitsunobu AAIA Paper #2000-1483
A New Bonded Wavy Composite Lap Joint 995
Sun,CT
Zeng, Q AAIA Paper #2000-1484
"Dancing" Wind Tunnel Models for the Direct Measurement of Generalized
Unsteady Aerodynamic Loads N/ALivne, Eli AAIA Paper #2000-1485
Expedient Unsteady Transonic Solutions Above and Below Freestream
MachOne .1004
Chen, PC
Liu, D D AAIA Paper #2000-1486
Prediction ofAeroacoustic Noise Generated by Viscous FlowAround
Rectangular Cross Sections 1015
Lee, JongsooYoo, Jungkeun AAIA Paper #2000-1487
Simply Implementing Non-Rational Function Gust Filters for Real Time
Simulation Application 1025
Chnsthilf, David M
Pototzky, Anthony S AAIA Paper #2000-1488
Correction of UnsteadyAerodynamic Influence Coefficients Using
Experimental or CFD Data 1034
Bnnk-Spalmk, Jan
Bruns, Julius M AAIA Paper #2000-1489
Enhanced Damping of Continuous Wave Fiber Composite Sandwich Panels ... 1039
Jensen, David W
Steurer, Keith A AAIA Paper #2000-1490
Simulation of Delamination Buckling and Growth in Composite Structures .... N/ANilsson, Karl-Frednk AAIA Paper #2000-1491
American Institute of Aeronautics and Astronautics
Unified Approach to Modeling Matrix Cracking in Laminated
Composite Structures 1047
Chattopadhyay, Aditi
Thornburgh, Robert AAIA Paper #2000-1492
An Evaluation of Mixed-Mode Energy-Release Rates in the Cracked Sandwich
Beam Specimen n/AShivakumar, K N
Smith, Steven A AAIA Paper #2000-1493
Effects of CPC's and Clamping Force on Fatigue Behaviour of
Bolted Joints N/ADhaman, RubyShankar, Krishnakumar AAIA Paper #2000-1494
Higher-Order Asymptotic Model for a Heterogeneous Beam, IncludingCorrections Due to End Effects .1055
Buannic, Natacha
Cartraud, Patrice AAIA Paper #2000-1495
Nonlinear Bulging Factors for Longitudinal and Circumferential Cracks in
Cylindrical Shells Subjected to Combined Loads .1064
Rose, Cheryl A
Stames, James H
Young, Richard D AAIA Paper #2000-1514
Plane Strain Radial Flow of Rigid/Hardening Solids - Part II: Effects of Material
Non Homogeneity N/ADurban, David AAIA Paper #2000-1515
Influence of Geometric Nonlinearities on the Response and Failure of
Internally Pressurized Elliptical Composite Cylinders .1079
Hyer, M W
McMurray, Jennifer M AAIA Paper #2000-1516
Crack Path Bifurcation at a Tear Strap in a Pressurized Shell .1090
Cowan, Amy L
Davila, Carlos G
Johnson, Eric R
Stames, James H AAIA Paper #2000-1517
Crack Tip Fields in Anisotropic Shells N/A
Yang, S
Yuan, FG AAIA Paper #2000-1518
Damage Progression in Buckle-Resistant Notched Composite Plates Loaded
in Uniaxial Compression N/A
Ambur, Damodar R
Davila, Carlos G
McGowan, David M AAIA Paper #2000-1519
3-6 April 2000
Structural Optimization for Light-Weight Articulated Rotor Blade 1102
Kim, Jong-Eun
Sangul-Klijn, Nesrm AAIA Paper #2000-1520
Optimization of Car Body under Constraints of Noise, Vibration,
and Harness (NVH), and Crash 1113
Kodiyalam, Snnivas
Sobieski, Jaroslaw
Yang, Ren-Jye AAIA Paper #2000-1521
Optimization of Mistuned Biaded Discs Using Gradient-based ResponseSurface Approximations • 1129
Haftka, R T
Petrov, E P
Vitali, R AAIA Paper #2000-1522
Analysis and Optimization of Mid-Plane Asymmetric Sandwich Beams under
Lateral Loading Including Buckling Effects 1140
Satapathy, Nihar
Vinson, Jack R AAIA Paper #2000-1523
Integrated Optimization of Viscoelastic Structures and Active Controllers for
Flexible Space Structures 1148
Onoda, JunjiroUchida, Hideki AAIA Paper #2000-1524
Detection and Correction of Poorly Converged Optimizations by IterativelyReweighted Least Squares 1159
Grossman, Bernard
Haftka, RaphaelKim, HongmanMason, William
Papila, Melih
Watson, Layne AAIA Paper #2000-1525
Dynamic Taxi, Take-Off, and Landing Roll Analyses for Large Business
Jet Aircraft 1177
Brodman, Hank
Freund, Don
Hanson, LarryMcKissack, Doug AAIA Paper #2000-1526
Flexible Multibody Dynamics Equations with Constant "Mass Matrix" N/ABanerjee, Arun K
Chien, L S AAIA Paper #2000-1527
Finite Elements in Time Domain for Optimal Control Using Higher-OrderShape Functions 1188
Kapania, Rakesh K
Kim, Seung Jo
Park, Sungho AAIA Paper #2000-1528
American Institute of Aeronautics and Astronautics
3-6 April 2000 Table of Contents - xix
Modeling of Frequency Dependent Properties of Viscoelastic Materials
Subjected to Shock Loads 1194
Inman, Daniel J
Lesieutre, George A
Rusovici, Razvan AAIA Paper #2000-1529
Transient Response of Contacting Plates Subject to Close ProximityBlast Loads 1205
Coggin, John M
Johnson, Eric R
Kapania, Rakesh K AAIA Paper #2000-1530
On the Understanding of Snap-Through Phenomenon in Aerothermoelasticityof Panels 1215
Udrescu, Radu AAIA Paper #2000-1531
Investigation of Curved Composite Panels Under High-G Loading 1224
Jenkins, S N
Spearing, S M AAIA Paper #2000-1532
Stiffness Tailoring of Tension-Loaded Composite Panels to
Contain Damage 1234
Bhatia, Narain
Ley, Robert P
Lin, Weichuan
Mahler, Mary A
Patel, Nash
Wolf, Ed AAIA Paper #2000-1533
Propagation and Control of Crack-Like Damage in Curved CompositeCombined Loads 1243
Ley, R P
Lin, Weichuan
Mahler, Mary A
Rouse, Marshall
Shah, C AAIA Paper #2000-1534
The Reliability of AdhesiveJoints Under Piezomechanical Loading 1252
Sanders, C
Shaw, M
Spearing, S Mark AAIA Paper #2000-1535
Predictor-CorrectorApproach for the Analysis of Sandwich Panels 1261
Kim, Yong HyupPark, Jin Woo AAIA Paper #2000-1536
Single and Multi-cell Composite Thin Walled Beams N/A
Hodges, DeweyVolovoi, Wall AAIA Paper #2000-1537
American Institute ofAeronautics and Astronautics
3-6 April 2000
Fixed-Order Mixed Norm Designs for Building Vibration Control 1271
Calise, Anthony J
Hsu,CC
Whorton, Mark S AAIA Paper #2000-1538
An Advanced Buffet LoadAlleviation System N/AHopkins, Mark A
Pitt, Dale M
White, Edward V AAIA Paper #2000-1539
Active Control of Airframe Response with Distributed Smart Actuators N/AChopra, InderjitPark, Hun AAIA Paper #2000-1540
Cargo-Pendulation Reduction in Boom Cranes Via
Cable-Length Manipulation 1280
Abdel-Rahman, E M
Nayfeh, A H AAIA Paper #2000-1541
Nonlinear Control of a Parametrically Excited Structural Dynamic Model of an
F-15 Tail Section 1288
El-Badawy, Ayman
Nayfeh, All H AAIA Paper #2000-1542
Cargo Pendulation Reduction on Ship-Mounted Cranes via Boom-Luff and
Slew Angles Actuation 1299
Henry, R J
Masoud, Z N
Mook, D T
Nayfeh, A H AAIA Paper #2000-1543
Fracture Parameter Evaluation of Composite Panels Under
In-Plane Loading 1305
Cai, GaryXYuan, F G AAIA Paper #2000-1544
Prediction of Fretting Fatigue Crack Initiation Based on the Plane of
Maximum Shear Stress Amplitude 1316
Jam, V
Lykins, Chris
MallS AAIA Paper #2000-1545
Influence of Contact Profile on Fretting Crack Nucleation in a
Titanium Alloy .1326
Farns, T N
Hansh, G
Murthy, H AAIA Paper #2000-1546
American Institute of Aeronautics and Astronautics
3-6 April 2000 Table of Contents - xxi
Tests of Braided Composite Fuselage Frames under Radial Inward Load 1334
Boitnott, Richard L
Johnson, Eric R
Perez, Jose G AAIA Paper #2000-1547
Investigation of Impact Damage in aCFRP Wingbox under Load .1344
Clarke, A
Greenhalgh, E S
Millson, B
Thompson, Roy AAIA Paper #2000-1548
Evaluation of Fracture Modes in Mixed Mode Delamination Problems N/AArmanios, Enan
Makeev, Andrew AAIA Paper #2000-1549
On the Use ofEnergy Minimization for CA BasedAnalysis in Elasticity 1355
Hajela, Prabhat
Kim, Byong AAIA Paper #2000-1579
Cellular Automata for Design of Truss Structures with Linear and
Nonlinear Response N/AGurdal, Zafer
Soremekun, Grant AAIA Paper #2000-1580
GeneticAlgorithms for the Optimization of Piezoelectric
Actuator Locations . .1366
Kapama, Rakesh
Sheng, Lizeng AAIA Paper #2000-1581
Genetic Algorithm Approaches to Smart Actuator Placement for
Aircraft Flight Control 1377
Cook, Andrea M
Crossley, W/lliam A AAIA Paper #2000-1582
Using a Genetic Algorithm to Design Beam Cross-Sectional Topologyfor
Bending, Torsion, and Combined Loading .1387
Crossley, William A
Fanjoy, David W AAIA Paper #2000-1583
Genetic Algorithm Based Design of Transonic Airfoils UsingEuler Equations .1396
Jang, MmsungLee, Jongsoo AAIA Paper #2000-1584
Influence of Target and Impactor Parameters on the Nonlinear Response and
Residual Strength of Curved Thin Composite Plates N/A
Ambur, D
StarnesJ AAIA Paper #2000-1591
American Institute of Aeronautics and Astronautics
3-6 April 2000
Failure of Laminated Composites at Thickness Discontinuities under ComplexLoading and Elevated Temperatures n/A
Knauss, WolfgangLee, S AAIA Paper #2000-1592
Size Scales for Accurate Homogenization in the Presence of Severe
Stress Gradients N/APagano, N
Yuan, F AAIA Paper #2000-1593
On the Simulation of Crack-Propagation in Pressurized Shells ................1405
Rankin, C C
Riks, Eduard AAIA Paper #2000-1594
Collapse of Elastic-Plastic Plates with Cracks 1416
Corona, Edmundo AAIA Paper #2000-1595
Analysis and Test of Repair Concepts for a Carbon-Rod
Reinforced Laminate .1421
Baker, Donald J
Rousseau, Carl Q AAIA Paper #2000-1596
Microstructure and Creep Behavior of Self-Reinforced Silicon Nitride Ceramics
Heat-Treated by Furnace and Microwave Annealing .1431
Narayan, JaySankar, JagWei, Quimmg AAIA Paper #2000-1603
Microstructure and Mechanical Evaluations of Sintered Si3N4 1439
Kelkar, A
Russell, LarrySankar, J
Wei, Q AAIA Paper #2000-1604
Mechanical Performance of CF/Polymer Composite Laminates under
Cryogenic Conditions 1448
Aoki, Takahira
Ishikawa, Takashi
Kumazawa, Hisashi
Mormo, Yoshiki AAIA Paper #2000-1605
"In-situ" Characterization of Thermal Degradation in Graphite/Polymeric Composites * 1456
Lin, Kuen Y
Ohno, Satomi
Ohuchi, Fumio S AAIA Paper #2000-1606
Evaluation ofAlpha Case on Titanium Casting Specimens N/A
Phelps, Henry AAIA Paper #2000-1607
I American Institute of Aeronautics and Astronautics