Manual of Aeroelasticity

7/26/2019 Manual of Aeroelasticity

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1 7 1 8 4 8

AG A RD-R-578-

AGARD REPORT No. 578

Manual on Aeroelasticity


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3/2368

NORTH ATLANTIC TREATY ORGANIZATION

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT

(ORGANISATION DU TRAITE DE LATLANTIQUE NORD)

MANUAL ON AEROELASTICITY

~~

SUBJECT AND AUTHOR

INDEX

. _ - -

Edited by

E.C.Pike


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FOREWORD

The Subject Index and A utho r Index cover all the chapters in the six loose-

leaf volumes of the Manual on Aeroelasticity and were up to date in April 1970.,

Since that date new chapters of the Manual have been published in the AGARD

Report series.

The Indexes are published in two forms:

in

the AGARD Report series as

AGARD R eport 578 and in loose-leaf form fo r insertion in Volume VI of th e

Manual.

Entries are given by Volume, Chapter and Page number.

For example, 11/9/56

depotes Volume 11, Chapter

9,

page 56.

The letter S af ter a Chapter number

denotes a Supplement

to

that Chapter.

The letters TG denote the section of Tables

and Graphs

in

Volume VI. The abbreviation INTRO denotes the Introductory

Survey in Volum e

I.


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CONTENTS

FOREWORD

SUBJECT INDEX

AUTHOR INDEX

LIST OF CONTENTS OF MANUAL ON AEROELASTICITY

Page

iii

1

15

23


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1

SUBJECT INDEX

Abels theorem 11/2/40

Ablating plates I/7/37-8

Acceleration effects IV/9/

14-1 5

Acceleration potential II/

1/

13-14

Accelerometers IV/ 1 2 5-6,27

:

IV/5 /3 9 :

I V/ 7 / 2 5 2 6

Accident investigation III/5 /2

Ackeret theory III/7S/10,16,4 1,49

Acoustic resonance 1V /5/5 4: 1V/7/

13

Actuators 1/5/8-19,29-33,354 1

Admittance concept IV/2/3-4,12,2@ 21

Aerodynamic aspects Volum e I1

histor ical review 11/ 1/3 -9

methods

of

ana lys is 111 1/9 -25

Aerodynamic centre position 11/9/ 1

:

Aerodynamic coefficients see Derivatives

Aerodynamic forces

V/ 1 /3 ,5 ,7 : V/6 /19-2 1 , 25 28

approxi mation s 11/5/ 11-55

generalised

definit ion I /INTRO/2

formulae II/Chapter

4:

II /Chapter 7:

III/4/4,27: 111/7/7: III/8/9-12,17-20

geometry III /2/20

measurement II/ 1/22-3

propeller 111/9/5-7,10-13

aerodyn amic aspects Vo lum e I1

classification I/INTRO/

1

7-2

1

design implications III /2/ 9,5 45 : 111/3/

1 8 - 1 9

history I /INTR0/45-8

prac tica l aspects I / I NT R0 /44 5

Aeroelastic phenomena

Altitude effects

f lutter

cont rol surfaces 111/5/10: V/3/21

pane ls 111/7/ 14

wings V/2/25-7

massbalance V/4/7,9-12

models IV/6/11-17,20-23: IV/7/14

panels III/7/1@1 6,18,22,24: III/7S/27-9,33 ,40

cylinders III/7/26-8: III/7S/41

Aluminium

A mpli tude response technique IV/ 10/5-7

Analogue met hods IV/7/ 1-2

Angle of attack, definition III/2/25-6

Ankylosis 1/6/40,5 1

Apparent mass conc ept 11/6/7,12

Approximate methods

aerody nam ic forces 11/5/1 1-55

flutter V/Chap ter 6

static aeroelasticity III/2/12-38: III/3/5-1

1,14

Arrow-head wings 11/5/ 14,36-8:

11/

10125-8

Aspect ratio effects

on buzz V/5/49,50

o n deriva tives 11/ 11127-30,4@41

on divergence III/2 /3

on f lutter

control surfaces VI318

panels III/7/24: III/7S/41,50,5

1

pure pitching V/5 /2 1

wings V/2/10-13: V/6/2 6

on negative damping V/5 /9-10

Asym ptotic solution 1/4/9

Atmosphere line IV/6/ 19,20


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2

Bearings IV/5/7-8

Bending moment

idealised 111/2/ 15 ,20

wing root V/l /3-4

panels 111/7/ 15,17 ,20: III/7S/ 18

Bending rigidity

Bernouillis eq uation 11/7/6,9,13,62,63: 11/8/ 14

Biconvex aerofoils

damping in pitch 11/9/ 14,18

pitching derivatives 11/ 1

O/

17

Bifurcation 1/6/36,37

Binary flutter

approximate formulae V /6 /7 42

control surface V/4/6-15

def ini t ion I / INTR0/24

Biot number IV/6/2 6

Biplanes, f lutter of I /IN TR 0/4 6-7

Blades

flapping 111/9/13-16: III/ lO /lO ,l1

flutter I /INTRO/25-6: III/Chapter 9:

I I I /Chapter 10 : V/5/ 25

ground testing I/4/73-87

Blasius proce dure 11/8/22

Bodies of revolution , slend er 11/7/ 12-16,32 -48

Body-freedom f lut ter V/2/3 ,41-4: V/6 /42

Body freedoms III/6/4,9,11,2 2

Bomb, free-falling IV/6/21: IV/Chapter 9

Bond number 1/8/23,28,70,71

Bonkers I / INTR0/35

Boom -mounted lifting surface V/ 1/9

Boundary conditions

general aerod ynam ic 11/

I / 14-1

5

indicia1 function II/6/2-4

lifting surface II/5/7-9

Cathetometer IV/

I /

15

Cauchy-Riemann equations II/8/ 4

Centre of gravity effect

body-freedom flutter V/ 2/4 1-3

control surface f lu tter V/3/18: V /6/52

Cen tre of pressure effect III/4 /24 : 111/5/9:

V /1 /5 : V /2 /4 : V /4 /13

Characteristic equations I/4/3,6,

I O

Characteristic phase lag I/3/ 1 , 2 4 7

Characteristics, me thod of 11/9/33

Charts, static aeroelasticity III/ 2/2 4: 111/3/ 1 0 - 1 1

Choking frequency, autopilot I1I/ 8/ 23,28

Circulation function

see

Theodorsen function

Collocation method see Kernel function procedure

Comfort stall (blades) III/ 1O/17

Compo nent Analyser Technique IV/2/3,1 8-20

Com pone nt resolvers IV/ 5/5 1-2

Compressibility effects

see

Mach number effects

Compressor blades see Blades

Computers, use in

autopilots 111/8/13

dynamic stability III/6 /29 .

general

III/

I /

13:

III/Chapter

4s

influence coefficien ts 111/7S/10: IV /1 /27

model testing I V/7/ 1

non-linear problems I/6/24-5

panel flutter 111/7S/7

propeller flutter 111/9/21

Cones, circular II/7/43 -5,58-6 1

:

I I /9 /37,49

Conformal mapping 11/2/11,12: II/4/81-4 :

Continuous media, damping I/3/

14-1

5

Continuum methods 1/2/1 ,12,13

Contours, f lutter speed V/ 2/3 3

II/8/3-3 8


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3

Coordinates

transformation of 11/ 2/6 4: 11/3/27

fixed 11/3/36: II/4/3

moving II/3/6-10

slender-body theory II/7/6

elliptical 11/7/26

Coplanar mot ions I /4 /2

Cord, tra ilingedg e 111/5/ 15

Coriolis effects I/8/ 13 : 11/9/28: III/4S/5

Cosine curves IV/3/11 -14

Cosine factor , sweepback V/2 /6,10

Coulomb damping V/3 /3 3

Counter , electronic lV /5/5 3

Coupling

aerodynamic Ill/ I / 10: V/2/3 ,23

coefficients I /INTR0/36-7

frequencies V/3/ 1 5-1 7

inertia 111/5/9,1 1 : V/2/3,27: V/3/6,9-14

Cramer 's rule III /6/3 2

Creep I/7/4-6,27-9

Criteria, flutter

binary systems V/6/9 -

1

1,54

contro l sur faces V/3 /4 ,8

massbalancing V/3/ 14,20

powered controls V/4/6-7

tabs V/3/25,27-8

wings V/2/19

Critical speeds, prediction III/Chap ter 1

Cross inertia V/4/7 ,9

Cross stiffness V/ 3/ 13: V/4/3 ,8 : V/6 /47-8

d'Alembert's principle 1/7/ 19: 11/6/ 13,14

Dampers ll1/5/9,1

1',14:

V/3/9,29-31:

V/ 5153,54 : V/6/ 55

Damping

Dampometer IV/5/ 14-16

Data

aerodynamic III/2/46-52:

M/3/

15-1 7:

inertial III/2/5 1

structural III/2/39-46: lIl/3/ 14- 1 5

analysis IV/9/ 10 13

automat ic IV/

I /

19,26,27

magnetic tape IV/5/14: IV/10/7,17,18

manual IV/ 1/26

methods 1 /4 /30

optical trace IV/IO/ 1 9

photogra phic IV/5/ 13,48,49

III/5/9-1

1

Data recording

Definitive me th od s III/2/24-32: 111/3/

1

1-14

Deflation, metho d of III/6/9,18-21

Deformation

effect on autopilot III /Chapter 8

shear 1/2/14

structural I /Chapter 1 : III/2/29-30

derivatives

III/

10/28,29-33,34,38-40,46-7,s

:

f lutter V/2/ 13,19,37,41-4: V/5/32 ,50

lift distrib ution II/5/ 5 1-5

model tests IV /8/9,1 0

shear deformation I /2/

I4

thickness effects II /9/3

1-3

effe ct on wh irl flu tte r 111/9/ 17-1

8

effect on wing f lutter V/2/25-7

variation in tests IV/5/1 2: IV/6/2,8-17,20-23:

Delta wings

I I / I 1117-19,2 7,3 1-2

Density, air

IV/7 /14

Derivatives

aeroelastic effects II1/2/5-7


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4

Dirichlet problem 11/9/33

Discrete me thod s I/2/ 1-2,12

Displaced frequency metho d I/4/ 17,18,82-3

Displacement

funct ions I / INTR0/6-9

formulation I /7/7

Dissipation func tion I/4/5- 6

Divergence

blades III/ 1O/ (1 2

general I/INTRO/l&l9,21-2: 111/1/1,2:

panel f lutter III /7/27,28

record analysis IV/9 / 10

Donne11 equa tions III/7S /45,4 7

Doppler equipme nt IV/9/3-4

Doublet-sheet me tho d 11/9/30

Downwash

III /Chapter 2: V/Chapter 1

calculation II/5/32-3: 11/8/&9,1 1,1 7

distribution 11/5/ 13,34: 11/6/ 15

mean 11/8/41

points , choice of III/3/24-6 : 11/4/ 14-19

variat ion 11/8/ 13-14

Drag parachutes III /7/37

Duh amd integrals II /6/4,14: III /4/32,33

Duncan functions 1/2/5 : III/4/2 0

Dynamic amplification factors I/3/ 15-2 1

Dynamic balance V/3/9-14,2(128

Dynamic flexibility matrices 1/3 /29

Dynamical

equations I/INTRO/1-5,12-14

systems I/6/3-38

variables I/INTRO/

1-5

Eddy shedding I1/5/8: III/ 10/ 21: V/5/2,22-3

Eddy-curren t damping IV/

5 /

24-5,27

Expansion meth od 11/5/ 13-14,27-9: II/8/ 3

Experimental methods Volume IV

comparison with theory II /Chapter 10:

influence coefficients IV/Chapter 1

sta tic aeroelastic e ffects 111/2/51-2: 111/3/ 17-18

Explosive charges III/4 /29

External stores

III/ 1/22,24-6: I11/9/ 14-16: IV/ l0 / 2 5

effect on derivatives I I / l 1/63-6: III/I/ 18

effect

on

divergence III/2/4

effect o n wing f lutter

III/S/5

models 111/1/19: IV/7/8,17: IV/8/6,12

optimum position III /2/55

rotatory inertia I /2/ 9

vibration analysis 1/2/9,13

Failure

models IV /8/5: IV/9 /7

power controls IV/4/8

s t ru c tur a l I I I / l / I : I I I /5 /2

Fatigue IV/ 10/3-4: V/3 /29,3 3

Feedback

effect on flutter 111/4/12

force IV/4/ 11,13

structural IV/4/5

Fi lte ring 1 /4 /35 40: I I I /8 /4 ,26 : IV/ lO/I 7 -19

Fin and rudder

derivatives II/ 1 1/60-66

f lutter V/3/24: V/4/9,11,20

Finite-difference equations I/ I / 15,19 ,20

Finite-element method 1/7/17: II1/2/45:

Flaps

III/7S/6

buzz

V/ 5 28-3 2,36-9,43,5 0 52

hinge mom ents I l l 1 1/34


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causes I /INTRO/26-30: V/3/6,17-21:

classical V/2/ 17: V/5/1 2-14

coefficients V/6/ I 1

control surfaces III / l /7: III /4/22-3:

coupled V/S/53,54: V/6/28-55

criteria

V/3 /2

1-3

III/5/8-13,16: V/Chapter 3: V/6/28-54

approximate V/6/9,10,27,36,38,54

control surfaces V/3/4-5

panels III/7S/54-5

v/5 /53-4

III /4S/4: V/6/6,8

diagnosis and cure III/Chap ter

5 :

I l l /

IO/

18-1

9:

elevator III /S/S: V/3/24-5

equations 11/5/9- 1 1: 111/4/ 1,4-9,1 2-18 :

f in and rudder III /5/7-8: V/3/24-5: V/4 /9,11 ,20

fundamental V/2/28-3 1,35

general description I/INT RO / 19-20,23-38

helicopter blades III/Chapter IO

historical review IV/ 10/2-3

large amplitude 111/7/

I O

main surfaces 111/5/3-8,16: V/ 6/ 11-28,58-60

overtone V/2/28-32,3 5,38

panels III /Chapter 7: III/Chapter 7s : V/5/2

parameters III/4/23-5

prediction I /INT R0/3 6-8: III /Chapter 5 :

propeller-rotor III/Chapter

9

shells II1/7S/41-7

single-degree-of-freedom V/Chapter

5

stalled V/5/23-6

stall ing I /IN TR 0/3 0: 11/9/51-3: III / l0/1 3-19 :

tabs l l l / 5 / I 3- l 6 : V/3/25-31: V/6 /47-54

Ill/ 1O 18-19: V/3/32-3

IV/6/7: V/5/2,1 1 - 1 5

5

displacement IV/3/24-7

measurement IV/5/

53

natural

choice of IV/3/27

definition I/3 / 19-20: II1/8/7

determination 1/3/33

pseudo

-

1/4/24

ratio V/3/

15-1

7,1&21

reduced, effect on derivatives VI/T G

requirements V/3/8-9

control surfaces V/3/7-8

definit ion I /INTRO/ 1 1

history I l l 1

/3-4

liquids I/8/39-67

Frequency parameter

Frequency sweep IV/3/1: IV/ 10/7,16

Friction, solid I/INTR0/9,44-5: I/4/ 19,40,5 1-3:

Froude number 1 /8 /70

Fuel sloshing I /6/ 2: ] /Chapter 8: 111/1/8:

1V/6/7: V/2/22

Fuel tanks

see

Tanks

1/6/2 ,22 : I l I / l /7 ,9 : IV/3 ,21-3,30: V / l /9

Galerkin method

dynamic stabili ty III /6/23,24,32

panel flutte r III/7/4-8,12-2 1,29,3 0:

stati c aeroelasticity III/2/34-5

Galloping V/5/23

Gauges see dial gauges, strain gauges

Gaussian integr ation 11/3/ 16-18 ,3 3

Gaussian points IV /l /8

Gauss-Seidel process 1/3/34

Geared surface me thod I /5/35-41 : V/4 /3

Generalised coordinates

111/7S/4-7,14-15,20-25,39,42-4,47,49-53


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6

Helmholtz

equation 11/7/

1

vorticity theorem 11/8/4,12

Hermitian matr ices l lI /4S /l 1 ,24: III /6/2 4

Hessen berg m atrix ,

I1

1/48/27

Hinge moment

derivatives

11/ 10/34,47-8: l I / 1 1/7,33-60

effect on buzz V/5/44-50,54

effect on impedance 1/5/19-22

predic tion of 111/3/ 17: V/5 /44

Hinge posit ion, effect on buzz V/5 /50,5 1

Hinge stiffness, effect on buzz V/ 5/4 2,4 3,4 6

Hookes Law 1/7/3 ,22

Horn balance V/3 / 14

Hsus method II/3/34-7

Hyperbolic radius II/9/3 1-2

Hypersonic flow

indicia1 response 11/6/4 6,53

osci l la t ions I I /9 /248

damping

Hysteresis

curves I /3 /45 ,9-

10,

I 2

measurement IV/S/ 1 1,22

magnet ic IV/5 /28

stabili ty boundary V/5 /30

structural non-linearity I /6/ 2 l-3,39,

49-5 1 IV/ I / I O

Impedance

complex I/3/ 1 1

experimental determination I /5/29-33

manual controls I /5/6-8

match ing V/4 /5

models IV/8/ 1 1

powered controls I /5/& 33: II1/5/6:

moment o f

control surfaces V/3/ 12,14,18-23,27

determination I /4/64-6,72

fuselage V/2/4 1-4

roll ing V/2/38

spars IV/7/ 16

tab V/3 /2 7

parameters 111/4/24

product of

control surfaces V/3/ 13, I4

t ab V/3 /2 7

rotatory 1/2/9,14

ta b linkage 111/5/13-14,15

Inexorable forcing see Rigid drives

Inflow angle 11l/9/ 12-13: II1/10/19- 20

Influence coeff icient method I /IN TR 0/5,6 :

Influence coefficients

accuracy III/4/8

dyn am ic stabili ty I11/6/4-17,24

high temperature structures III / l /2 3

measurement IV/Chap ter 1

panel flutte r II1/7S/5,41

static aeroelastic pheno mena I11/2/26-5

1

:

three - dimensional supersonic theory

I/2/6-14: 11/1/20: 111/1/6: I I I /4 /5

111/3/1 1, 14 15

II/S/ 1 1,26-7

Influence points IV/1/7-8

Instability

conditions for V/5/3-4

prediction of III /Chapter

1

regions 11/2/27

flight flutter tests I I I / S / l , 12,16: IV/lO/2

1-5

ground resonance tests IV/2/ I O - I4

Instrumentation


13/2368

7

I tera t ion methods

auto ma tic processes 111/4S/

13-1

9

dynam ic stability III/6/2,3-20,26-9

non-linear prob lem s 1/6/ 25-8

panel f lutter III /7/9-10

stat ic aeroelasticity II1/2/36-8

Jacks

circuit diagram IV/4/ 14

equations of mo tion 1V/4/

18-19

impedance IV/Chapter 4

load application IV/

I /

14

operation IV/4/2-4

stall ing III /4/24

stiffness

III /S /

1 1

Joukowski profile II /8/3,18-20,23,29,30,3

538

Ju mp p h eno men on I /6 /3 6 7 : I/8/ 1 1

Kelvin circulation theorem

II/8/4

Kelvin mod el 1/7/4,5

Kernel function method

Ill

10/

19,33,36

comparison of theory and experiment

lifting-surface theory III/4S/ I O

panel flutt er II1/7S/5

stat ic aeroelasticity III/2/33,47 -8

thickness effects I1/8/3

three-dimensional supersonic theory

I1/5/3 1,33-4,4&42,5 1-5

Kinetic heating

effect on divergence and reversal V/

1

/ I O

general e f fec ts l / IN TR 0/4 l

non-linearity I/6/3

simulation of IV/6 /25-6

Kirchhoff s formula 11/6/38

Lenzs law 1/4/76

Levers, measuring lV/ 1/23-5,27

Liapunov me tho d II1/7S/6,17,20

Lift-curve slope

effect on f lutter V/5/23-6

tail V/1/5

wing V/1/5

Lift functio ns 11/5/34-40,49-50,60

Liftinglin e theory I1/ 1/20: H/3/ 1 : 11/6/21 :

I l / I

1/19:

I11/4S/lO

Lifting-surface methods

autom atic processes III/4S/8-1

1

matri x form 111/4/5-6

oscillating finite wings I I / 1/20-22

comparison with experiment

Ill

I O / 19,25,

derivatives 11/8/37

three-dimensional

Lifting-surface theory

28,29,43

incomp ressible I1/6/ 27

so n ic l l / 4 / l , l 1-36

subsonic 1I/3/1

two-dimensional subsonic 11/6/16

Lifting surfaces, thickness effects 11/9/7-20

Light aircraft , f lutter l l l / l / 26

Limit cycle

panel flu tter 111/7S/47,5 1,52,55

single-degree-of-freedom flutter

V/5/5,30-35,46-50

Linear d i fferen t ia l equation I I / I / l l - l2 , l33

Linear superposit ion lII /2/2 8

Linear systems 11/1/23

Linearised equation

11/

1O I O

Linearised theory

comparison with experiment I l /Chapter I O


14/2368

8

Longitudinal-symmetric mot ion I/INTRO/S

Lorentz coordinates 11/2 /64

Lumped parameter metho d

I I /

1/23-4

Mach number, critical II/l0/ 12-1 4

Mach number effects on

buzz

V/ 5 / 2 9-3 6,3 9

control surface flutter V/3/7-9.18:

derivatives I/INTRO/I

1 :

II/10/28,32:

divergence III/2/3

dyna mic pressure V/ 1/2,3

gust response II/6/4 9,5

1

lateral control V/ 1/7,8

models IV/6/9-17: IV/7/13-14: IV/8/7-11

panel f lutte r 1ll/7/IO,l 1 : IIl/7S/I8,24-33,40,41

powered controls V/4/8,12- 13

root bending moment V/1/3 ,4

sonic theory 11/4/91

1

stalling flutte r V/5/ 15

wing flutt er V/2/3-5,9,16,20,25-7

:

wing stiffness require ment s V/2/ 19-21

V/6/37,41

II/11/30-32: V/6/19-22,35: VI/TG/I

1-138

V/6/ 22-8

Magnetic analysis method 1/4/3540

Magnetic tape lV/S/ 13,14,17

Manoeuvrability, rolling V/ 1 / 6 4

Marguerres equ atio n II1/7S /49

Mass

added to small models I/4/74-5,85-6

and spring systems I/4/5

1-60

distribution I/4/ 17: ll l / 6/4 : V/2/23-7

equivalent lV/3/24

generalised

I/4/

16,6 1-2,82-3,86

Mirrors see Optical

Mises me tho d III/4S/ 13-14,20,21,22

Mises profiles l l /8 / 19,21,33,37,38

Missiles

Ill /8/

14-28

Modal me tho ds III/2/32-3 ,38: III/8/4,5-8,28

Model tests

see also

Rayleigh-Ritz me thod

comparison with theory I l l / 1/24-6

propeller f lutter ll l / 9/

1

, I 1 1 1,13,21-2

representation of full-scale I/INT R0/3 2-5,

uses of I / INT R0/4 2: IV/7/2-3

buzz V/5/54

construction IV/Chapter 7

control surfaces V/3/5,6

failure IV/8/5 : IV/9/7

falling-body IV/6/2 1: lV/C hapte r

9

flexible 1V/5/45: V/2 /8,14

f lut ter

l l l /5 /8: IV/Chapter

7:

IV/Chapter

8:

V/2/2,5,8,9

full-scale 1V/9/ I O

high-speed 1V/7/20-21

history of types IV/7/3 - 12

instabilities lV/8/4-5

layouts IV/9/7-IO

light-weight IV/7/5,6-7,19,25

low-aspect-ratio IV/7/ I5

low-speed 1V/7/16-19

materials IV/7/ 16-2 1

mathematical I /3/3-15: l l l /2 / 12,13-24:

mechanical 1/3/3-15: I /8/48,5 1,55,56

rigidity 1V/7/15,36

42-4 : l l l / l /3 , I7 -2 l

Models

III/3/5-1

:

l l l /4 /2: I11/8/3,4: l l l / 9 / l 1 , I 7


15/2368

9

powered controls V/4/9-14

prescribed 111/6/2 1,2 2

representation of III/8/ 3

rigid-body 11/7/22-5,45-8,73: III/1 /12- 18

separation of Ill/8/

13

suspension effects I/4 /5 1-62,66-71

twist V/6/ 14

wing V/Chapter 2

complex I /3 /8

spring I/3/7

V / I / I

Modu

Ius

Monoplanes , , f lu t ter l / INTR0/46:

lI/

114:

Mullers me tho d II1/4/ 18

Multhopps meth od 11/3/ 1,2,30-33

Nacelles

damping l I l /9 /9 ,10,1

1

effect on derivatives I I / l 1/63-6

flexible Il1/9/3-4

underslung 111/3/2

see

also External stores

Neumanns prob lem 11/2/

1

1

Newton ian theory 11/9/24,25,27-8,38

Nodal l ines , points l l l / l / l8 , l 9 : 111/4/14:

V/2/3 ,29,37: V/3/ 14

Noise loading I/ INT R0 /4 1

Non-dimensional parameters

Non-linearities

aerodynamic

V/5/4-6,27-8,39,43-6,48

impo rtance of I/INTRO/ 12

incidence and Mach number effects

t yp es o f l l / 9 / l : l l l / l / 6 - 7 .

Ill 1o/ 12- 14

Oscillations

bending

V /S /

I O - I

I

,26

control surface V/5/26 -54

decaying IV/3/5,18 -19,23: IV/5/10 -14:

flapping Il/ 10/2 8

flutt er IV/S/ 18-20

forced V/5/4

I

,46

harmonic I1/2/8-9: III/4 S/7,9 : l11/6/ 1

:

v / 5 / 5

modes, definitions

Ill

10 /4

POGO

1/8/

19,65

pure pitching V/5/6-10,15-2

1

quasi-periodic V/5/32,33

relaxation 1/6/33-4

self-excited V/

5/

6,22-6,4 1-2,46- 7,s 0

short-period V/6/44

sinusoidal IV/5/4: V/ S/l 6, I8,28,33,34

small 11/7/65-8

types of 1/6/35

IV/ 1

O/

16-21

Oscillator, electronic 1V/2/

I O :

IV/5/26

Oscilloscopes lV/S/ 14-1 6,2 1,26,52,53: IV/8 /3

Ovary ellipsoid 11/7/46

Panel f lutter I /INT R0 /25: II/9/42,49-5 1 :

Per turbat ion methods I /6 /7-16

Phase-angle sweep IV/3/ I O -

1

1

Phase criterion I/4/ 15

Phase-plane me tho d I/6/3-7

Phase port rait s I/6/3-7,3 1,32

Phase resonance, excitation at IV/5/26-3

1

Phase-shifting netw ork IV/S/ 15,2 1,49 ,53

Phase stabilisation III/8 /27

Pick-ups IV/2/

I O :

IV/Chapter 5 : 1V/7/25

I l l / l / 6 : I I I /4 /25: I I I /Chapter 7 : I I I/Chapter 7 s


16/2368

Potential functions II/Chapter

8

Potent iometers IV/7/25

Power plant, representation of III/9/3-4

Powered controls

buzz prevention III/S/

1 1

control rotation frequency V/6 /32

flutter V/Chapter

4

impedance m easurement

HI/

/24: IV/Chapter

4

non-linearity I/6/2:

Ill/

1 7 , 8

special problems I/IN TR 0/4 5: III/5/6

Prandtl number IV/6/26

Pressure

difference, formulae II/2 /3 1-2

differential (panels) II1/7S/49,5 1,52

distribution, measurements

11/

10/23

dynamic

and stiffness ratio IV/8 /10,1 2

a t co ntr ol reversal III/3/2,7-8,12,17- 18

at divergence III/2/24 ,5 1-2

compressibility and sweep effects V/ 1/2-3

panel flu tter III/7/ 15- 17,20: III/7S/ 18,

loading II/9/24,25

perturbation II/5/6-7

plotting IV/5/43,44-6

Pressure potential procedure II/5/3 1-3

Prolate spheroid 11/7/46

Propellant dynamics I/Chapter 8

Propeller flutter III/Chapter 9

Proper vectors I/4/5

Pro tot yp e flutt er investigation III/1/14-15,17

Pulsation see Frequency, angular

30-45

Quasi-static

approximation III/7/6,7,29

Represen ta t ion

of aerodynamic forces I/INT R0/ 9-I 2

of controls I / INTRO /8

of damping I/INTRO/8-9

of structure I/INTRO/5-9: I /2/ 1

of structural deformation I/Chapter

1

of suspension, in groun d tests I/4/51-6 2

semi-rigid I/INTR0/6

ampli tude 1/4/9

curves 1/4/8-10,19-20: IV/3/7-9,10

effect of dam ping I/Chapter

3

many degrees of freedom 1/3/21-37

modes I / INT R0/6,7: I /4 /5

1-60

phase 1/3/20,23,32-3: I /4/9 ,19-2 0,804

1

position of IV/

1

O 1

0

14

principle

I/3/3

1-5

pseudo- I/3/33-5

single-degree-of-freedom I/3/ 1 5-2

1

testing in flight I /IN TR 0/3 5

Resonance

Resonance tests see

Ground resonance tests

Response

amplitude

I/4/

1 9

calculations, in practice III/Cha pter

4

curves IV/5/23

dynamic III/4/26-35

forced I/3/35-7

indicia1

11/6/2,6,14,15,30,33,38,50

jacks IV/4/1

measurement IV/8/2: IV/l0 /21-3

prediction III/Chapter

1

quadrature IV/2/ 19,20

to atmospheric turbulence III/4/33-5

to single impulse 111/4/29-33

Restraint, variable I/ 5/33-4


17/2368

Safety fac tor , f lu t te r V/6 /2 7

Safety margins I V/8 /12

Saint Venant to rs ion l / l / 5 : IV/7 /16

Sand me thod, vibration testing 1/4/7 6

Scale factors IV/6 /2

Schmitt tr igger circuit IV/5 /30,4 9

Secondary effects, structura l I/2/ 14

Seco nd-ord er theorie s 11/9/34-8

Self-excitation IV/5 /27-3 1,42-4

Sensor-analysers 1/4/20: 1V/3 / 1 1-14,27

Sensors I /5/41-6

Separation

effect on unsteady forces 11/9/38

localised I l I / l / 7

models IV/6/7

panels III /7/23

shock-induced lI l / 5/3 ,lO ,l1: V/S/21,

slender wings II/7 /6 1-74

stalling flutte r I1/9/51-3: V/5/14-15

Se rv o co nt ro l s I l I / 4/1 l - 1 2 : l l l / 5 / l3 , l 5 , l 6 :

III /Chapter

8

Shakers 1/3/31-6: IV/2/4-11,14-18: IV /7/ 25

Shapes, natural

30,31,42,48,53

definition I/4/4

determination of I /4/25,85-6

excitation of 1/4/

14-1

6

blades 1/4/85

suspension effects 1/4/6@6 1

I /7 / 17

conical

Ill /

7 /3 3

:

III /7S/47,55

copper 111/7S/43

cylindrical III/7/23-3 3: I11/7S/7-8,14,15,

Sheet-and-stringer structures, thermoelasticity

Shells

static aeroelastic pheno men a II1/2/49

thickness effects II/9/33-8

Slender-wing theory

comparison with experiment 11/ 10/30 ,43

general 111/4/6

indicia1 aerodynam ics lI/6/6,7,3 2-3,36

thickn ess effects 11/9/33-8

Slotted tunnels 11/ 10/4@4 1

Slow oscillation assumption

111/7/

17

Small p e rtu rb a tio n me th od l I / l / l l : 11 /5 /5 :

Snaking I / INTR0/20 ,44

Somm erfeld radiation H/2/ 10,2 1

Sonic f low

II/8/3

two-dimensional theory II/2/33-4 I

three-dimensional theory l l /Ch apter 4

Spars, mod el 1V/7/ 16,17-18,20-2 1

Split ter-plate V/5 /5 1,52

Sp

o

ers

Spray, propellants I/8 /2 1-2

Spring

V/

1

/ 7: V /5/4 1,42,52-3

bearings IV/5/8,37

constants III /2/20

constraint IV/5/ 10,20,25,34

rate Cjacks) 1V/4/6,17,19

tabs I/6/2,39:

I l l /

l /7 ,8: l l l /5/ 1,14-16:

VI6153

Spr ing suppor t technique V/2 / 40

Springs

calibrated IV/1/22

cubic hardening I/6/41-3

cubic softening I/6/43-4

elastic I/3/3-15

Stabiliser (of oscillations) IV/5/2 9,30,3 1


18/2368

12

Target towing II1/7/37

Telemetry IV/ 10/2 6

Temperature distribution in structure I/7/

1

Ternary flutter I /INTR0/24: 111/4/

16:

Test fun ctio ns II1/4/14-16

Tests

V/4/ 19: V/6/7,42-54

equipment IV /l / l1- 26 : IV/2/4-14:

IV/4/8-13: IV/5/6,7

full-scale 1/ IN TR Ol 3 5-6,42

impedance IV/Chapter

4

techn iques IV/2 / 14-2 1

:

IV/Chapter

5

types I / INT R0/42

vibration IV/7/23-6

see

also

Model tests, Ground resonance tests

Theo dorsen functio n 11/2/

I5 :

11/6/ 14;2

I

,22:

Theory

II I /6 /30 : VI/TG/2-4

comparison with experiment II/Chapter 10:

III/ I/2 2,24 -6: 111/9/ 14-16: IV / I0/25

Thermal stresses I/IN TRO /4

1

: I/2/

1

: I/7/

1

0-16,

Thermistors IV/5/30

Thermoe lasticity ]/Chapter 7

Thickness effects (aerofoil)

32-4: I11/4/25: V/l/lO

II/Chapter

8:

]]/Chapter 9: V/2 /

15-16:

V/5/9-10,3 1,43,48

Thru st, prop eller 111/9/ 1 1-12

Thrust orienta tion III/8/1,2,14-28

Thrust rods IV/2/14,15,16

Time parameter I /4 /2

Torq ue mo tor 111/8/21

Torque tube I /5 /27-9

Transducers IV/

I /

19: IV/2/ 12:

Unsteady theory Il/Chapter 8: I11/6/30

U-shaped interco nnect ions V/4/2 0-I

Valves (powered controls) I/S/ 1

1-1

7,23-7:

Vane, auxiliary oscillating IV/

IO/I5

Variational me tho d 1/2/2-6,12,13

Vector response plot IV/

I O/

2-1

3

Vectorial analysis technique IV/ 10/5,7-14

Velocity measureme nt, mode ls IV/9/3-4,5-6

Velocity potential

IV/4/2-7,15-

18

del ta wings 11/4/7443

expansion I I / S /

13-1431-5

in half-space 11/5/11-29

in whole spac e 11/5/30-31

low-aspec t-rati o wings I1/4/ 6 9- 78 ,9

8-

10 2

method 11/2/

10-15

perturbation

11/7/6 8 10 12 14-l6 17-18 6

rectangular wings 11/ 4/3 668

wing-body combinations I1/4/78-98

analysis I/4/3

1-40

Vibration

by inversion (magnetic analysis) 1/ 4/ 35 40

graphical

I/4/3

2,33-5

spectral I /4/32-3

beams 1/7/30-38

engine III/5/2,3

ground testing I/Chapter

4

plates I/7/30-38

propeller III/5/2,3

still-air III/6/22-5

structures I/Chapter 2

thermally induce d 1/7/30-32

types of III/5/2-3


19/2368

13

control circuit V/ 4/ 1,7,14-15

derivative IV/5/4,28

determinat ion of I / INT R0/8

distribution, wing I I I / S / 5

effect on wing f lutter V/2/ 14,17-23,26-7

elastic IV/5/8

errors in data I I I / S / 1 1 -1 2

fin III /5/7,8

in f lu t te r p revention I / INT R0/36 ,37

measurement

of IV/

1 / 1 : I V/4 /1 5 : I V /7 /2 3

non-linearities 1/6 /4 1-5 1

plates 1/7/30-38

*

propellers III/9/8-9

requirements III /2/54: 111/7/16,17: V/3 /18

scale IV/6/8-17,20,21,22,23: IV/7/

13

springs 1/3/&9

static, definition IV/4/ 17

structural

Ill /

l / 3 , 1 4

tests l11/5/6: HI / 1/23

torsional I I I /

1/8:

I I l /5 /6 :

Still-air tests

IV/S/

12,22,30,37

Strain

IV/8/ 10-1

1

components I / 1/7-8,19

energy I / l /8 -10 ,19 : 1 /2 /24

b ea ms I V / l / l P 2 3 : l V / 7 / 25

pick-ups IV/5 /4 7 : IV/8 /2 ,3

S rain-gauge

Stress formulation I/7/7-8

Strip derivatives

11/

1 1 / 4 7 : Ill/ I / 17-1 8:

Str ip theory

I I I / 4 / 4 5 : V / 6 / 1 1

general 11/1/19: II/2 /1: III/4/4-5

in approximate formulae V/6 / 1 1

indicia1 aerodynamics lI/6/2 7,53

piston theory l lI / 4/7

three-dimensional theory I I / 10/42-3:

two-dimensional theory 11/2/28-33: I I / 10/14-18

Su p p o r t , mo d e ls l l l / l / l 9 : I II / 2 /5 2 : I V /5 /7 :

IV/6 /6

Support , structure

ground tests

IV/

1 /8 ,9: IV/2/ 14

see

also

Suspension

II/Chapter

5

'

Surface integrals 11/5/43-9

Surface methods I I I /2 /3@32,40: l I l /3 / 14

Surface theory 111/7/16: III/7S /23

Suspension (ground testing) I/4/50-72

Sweepback effect

on approximate formulae V/6/ 12,24-6,29,32

on bending oscillations

V/S/ lO-I

1 15

on body-freedom flutter V/ 2/4 2

o n

buzz

V/5 /5 0

on derivatives 11/

1

1/27-30

on dynamic pressure V / 1/2,3

on lateral control V/1/7-9

on

loss

of l if t

V /

1

/

5

on negative damping V/S/9-10

on panel flutte r I11/7S/20,2 1,22,39,41

on.root bending mom ent V/1 /3,4

on static aeroelastic phenomen a 111/2/2-3,

on wing flut ter V/2/5-15,24,29-3 1

experiments 11/ 10/24 ,28 ,46 ,50

two-dimensional treatment 11/ I / 1 8

5-6,16,19

Sw ept wing

Swir l 1 /8 / l

1 - 1

2

Tabs

dampers V/3 /29


20/2368

1 4

Weber num ber 1/8/70

Wedge profiles

comparison of theory with experiment

hypersonic flow II/9/46-9

oscillating I I/9 / 23-7

Weight fun ctio ns l1/3/ 19-24

Weighting methods lI1/2/33-6

Weissinger me tho d III/ 2/4 9

Whirl flutte r III/Chap ter

9

Wielandts m eth od III/4S/ 17-1 9,25: ll l/ 6/ 19

Wind tunnel tests

I I / 1O 16,18

comparison with theory 11/Chapter 10

derivatives 11/11 27-30: IV/Ch apter 5

high-speed IV/6/9-20

low-speed IV/6/20

media othe r than air IV/6/24-5

techniques IV/Chapter

7:

IV/Chapter 8

see also Models

blow-down IV/7/6,20: IV/8/4,1 1

interference

I I / I

O

1,10,40-41:

IV/5/53-4:

operation IV/8/3-4

resonance II/ 1

O

I O , ] 1

Wind tunnels

IV/7 /13 : IV/8 /11-12

Wind-induced vibrations V/ 5/ 25

Wing theory Volu me I1

Wing tips

Wing-body com binations

effect of shape

on

f lutter V/2/9-10

sonic theory 11/4/78-98

slend er H /7 / 14-16,48-61

Wings

arrow-head Ills/ 14,368: 11/ 10/25-8


cro ppe d delta 11/7/24-5,58-61

deformation I/

I / 10-18

delta

1/2/14: II/Chapter I O


indicial aerodynamics 1I/6/3 1-3,41-3,52

influence coefficients 1/2/6

slender-wing theory 11/7/29

three-dimens ional sonic theo ry 11/4/7443

1/2 /14

derivatives I l l 11/8-32: VI/TG/4-5,11-14,

f lutter V/Chapter 2: V/5/6-26: V/6/10 ,11,

low-aspec t-ratio 1/2/6-7: II/4/69 -78,

26-4 1

13-28,58-60

98-118: I / I 1/19-26: 11/2/5,6,30,45-6:

lI l /3 / 14,16

raked I l / 10/43 ,44

rectangular


indicial aerodyn amics lI/6/30-3 1,34,43-5

slender-wing theory II/7/23-4,29

three-dimensional sonic theory JI/4/36-68

slender 1/2 /6: lI/7/10-13,17-3 1,61-74: II/9/9-20

see also Wing theory, Wing-body combinations

lI/ 10/25,37,38,43,50


21/2368

AUTHOR INDEX

Abbot t ,

F.T.

Jr . I I I /9 /24

Abrams on, H.N. I/Chap ter 8:

1/8/28,29,30,3 1,32,50:

II1/7S/64

Ackeret, J. 11/1/9: 11/9/20:

III /7S/10,16,41,49

Acum , W.E.A. II/3/2,37,4 0,41:

11/4/ 1 19: II /5/3 1,58:

II /Chapter

10:

I I /10 /55 ,57 :

II / l1/32,67: II1/7S/58,60,61 :

I V/5 /5 8

Adams 1/6/24

Adams, J . V/5 /41 ,59

Adams, M.C. 11/4/69,71,80,100,

120:

11/7/ 12,74: II /9/3 3,57

Aiken, W.S. Jr . I I I /3 /20 : V / l / l 1

Aitken, A.C. 111/4S/l3,23,24,36

Alexander, A.J. 11/10/25,30

Alexander, H.R. 1/6/46,5 4

Alfrey, T. 1/7 /39

Alksne, A.Y. II /9/2 ,20,5 4,55

Allen, D.I. II/3/2,41

Allen, H.J. 11/1/19

Amba rtsumyan, S.A. III /7S/68,

Anderson, M.S. III/7S/80 ,83

Anderson, R.A. I/2/ 15

Anderson, W.J. II/9/42,45 ,5 9:

III /7S/ I O , 1 1,12,44,67,70,73,

74 ,80 ,8 1 ,86 ,89

69 ,77

Andreopoulos, T.C.

11/

10/53:

Barboni, R. III /7S/85

Barling, W.H. II/1 1/ 67

Barmby, J .G. IV/7 /27 :

Baron, M.L. I/2/ 17

Barr, G. III /7S/86,89,90

Barrek ette, E.S. 1/7/40

Barrett , S. I V/1 /2 8

Basile, B. 1/3 /2,3 1:

Batem an, H. 11/2/ 1 1,4 2

Bauer, H.F. 1/8/28,2 9,3 1

Beam, B.H. II /10 /32,4 7,58:

Beatr ix, C. I /Cha pter 4(C):

Bellerby, P.J. IV/ 10 /2 8

Belubekian,

M.

II1/7S/84

Benham, P.P. 1/7/3 9

V/ 2/ 9,4 4

1/41

12,20 ,82

IV/ 5 / 5 5

1/4 /49

Bennet t, R .M. h1 /9 /7 ,10 ,1 l , I3 ,

22,24,25

Benscoter , S.U. I /2/8,1 6:

Benun, D. I/Chap ter

5:

V/1 /1 2

Bergh, H.

II /

10/6,52: 11/

1

1/8,

I V/1 /2 7

34 35 48 52 56 66 67 68:

111/9/ 19,25: V/ 5/5 7:

VI/Tables and Graphs

Berlot, R.R. 1/8/30

Berman, J.H. II /2/35 ,44:

II /5/57,58:

I I / I

0/53 ,59 :

Bohon, H.L. III /7S/7 1,73,76,

Bolas, H. I/In tro /48

Boley, B.A. I /Chapter 7:

I /7 /38 ,39 ,40 ,4 1

Bollay,

W.

IV/7 /3 ,26 : V/5 /56

Bolotin, V.V. III/7/47:

111/7S/59,62,63,64,65,67,70

Bosschaart. A.C.A. V /3 /36

Bratt. J.B. 11/9/ 1,54,6 0:

77,78,80,89

11/10/6,17,23,28,35,40,52,

54,56,57,58: III /10/22:

IV/Chapter 5: V/5/54,55,

56,51: V/5/18,20,55,56,

57,61

V/6 /5 6

11/5/56

Brebner, G.G. II/ 1

1/68:

Bremm ei, H. 11/2/45:

Brewer, Griff ith. II /Intro /49

Bridgeman, K.B. I 1/10 /40

Broad bent, E.G. 1/4/49:

III /Chapter 1 : I lI /Chapter 4:

II1/4/36,37: IV/ 10/8 ,27:

V/ 2/ 14,19,2 1,45: V/3 /2 3 ,3

5

:

V/4 /2 0 ,2 1 : V /6 /2 5 ,5 5 ,5 6

Brock, J.E. I /6/25 ,54

Broglio, L. 1/7/40: IV/ 1/28

Brooke Benjamin, T.

Brooks, G.W. I I I /9 /25 :

111/7S/ 1 1,94


22/2368

1 6

Calligeros, J. III/7S/75

Carls on, W.C.A.

11/

1O/S8

Carslaw, H.S. 1/7/3 9

Carter , L. III /7S/83,84,86

Carts, F. Il l / 1 0 /2 2

Chaikin, C.E. I/ 6 /5 5

Cha ng, C.C. 11/6/56

Chapple, E.W. I I / I 1/29,67:

V/2 /6 , IO, l3 ,15 ,44

Chastenet de

GCry,

J. I I /8/4,43

Chawla, J.P. 11/9/19,55

Cheilek, H.A.

11/

1

1/34: V/3 /25

Chen, C.F . 11/9/2,55

Chen , M.M. IV/ 1/28,30

Chin neck , A. 11/9/134:

11/ 1

O/

1 6 , 3 3 3 4 : Ill 1 1/45:

IV/5/54: V/5/

I8

Chu , W.H. I /8/28 ,29,3 1

SO:

I I I /7S/64

Chuan, R.L. II /9/5 3,60

C h u b b , R.S. III /2/56

Cicala, P. I /Intro /48,5 0:

I /2/ 16: 11/ l / 8 ,2 0 :

11/3/ 1,40: 11/6/

15

:

I V/7 /3

Clarke, J.F. IV/5 /56

Clauser, F.H. 1/6/55

Clerc, D. I11/6/5,33

Clevenson, S.A. I1 10/32,

54,5 8: 11/11/65,66,69:

1V/5 /55 : V/3 /35 :

V/5 /5 9 ,6 0

Clymer, A.B. IV/ 1/ 29

Coales, J.D. V/1 /23,5 8

Cunningham, H.J. I l l5 / 1 4 , 5 6 3 9 :

111/7/8,l 1,12,44: III/7S/IO,

58 ,73 ,85 : V/2 /9 : V/5 /56

IV/5 /56

Curran, J.K.

Ill

10/20,56:

Czuba, T.W. II /10/16,55

DAiutolo, C.T. Ill 10/40 ,59

Dalzell, J.F. 1/8/24

Danghaday, H.

HI /

1 0 /2

1

Dat, R. I /Chapter 4(E):

I /4/41,87: II /10/54,58:

III/7S/ 14,83,88:

IV/5/55

Davenport, W.W. 1/2 /17

Davies, D.E. II/Chap ter 4:

III /7S/ I0,6 I ,89: IV/9/ 14

Davies, R.J. I11/7S/66

Davis, C.J.

11/

10/56: IV/5 /54

Davis, E.L. Jr . IV/5 /57

De Garcia, H.J. III/10/21

de Jager , E.M. II /10/ 52:

V/6 /5 6 : VI /TG/4 ,8

Dengler, M.A. lI1/6/3 1,33:

V/3 /2 5 ,3 6

den Hartog, J.P. 1/6/22,53:

V/5 /5 7 , s8

Derb entse v, D. I11/7S/86

Destuynder, R. I /4/20,87:

II/ 1 0 /5 8

de Veubeke, B.M.F.

I /Chapter 3: 1/3/37,38:

1/4/ 12,21: 1/7/39:

IV/3 /30

Dugundji, J . 1/7/40: 11/5/57:

III /2/57: III /7S/62,70,75,81:

v / 1 / 1 2

Duncan, W .J. I / Introductory

Survey: I /Intro/48,49,50:

I /2 /5 : 11/ 1/4,6,24: II1/3/20:

111/4/20,36: 111/6/ 18:

IV/5 /54 : IV/6 / 1

Du nn , D.W. II/9/50,6 0

Dunsdon, D.V. l l / l 1 /35

Dura nd, W.F. 11/8/43:

11/7/75

Durling, B.J. V/3/3 4:

V/5 /5 8 : V l /TG/5 ,9

Durvasula,

s.

III /7S/41,83,88

Dzygadlo, Z. III /7S/66,70,75,

78,79,80,8 I ,83,85,88

Eagleson, P.S. III/ 7S /74

Eastep, F. III /7S/9 1

Eckhaus, W. V/5/41,59

Eggers, A.J. Jr. 11/9/56

Eisley, J.G . 111/7/

1

1

I

6,2 1,37,

41

:

111/7S/58,60,7

1

Ellen, C.H. 111/7S/5,8 0,90

Ellis, C.W. Ill/ 1 0 /2

1

Emerson, H.F. I l l 10/38 ,59

Epperson, T.B. 1/8/3 2

Ep s te in, A . V / l / l 1

Erickson, A.L. II1/7S/8 3,84:

Etk in, B. 11/1/25

Evans, E.W. III/ 7S /62

Evenson, D.A. III/7S/8 7,89

V/3 /3 4 : V /5 /4 1 ,5 8 ,5 9


23/2368

17

Frazer , R.A. I /Intro /8,46, 48,

4 9 ,5 0 : 1 /6 /5 3 ,5 5: I I / l / 4 ,

24,25: II /2/25,43: 11/6/56:

III/2/57: III/4/36: 111/6/ 18,

33: IV/5 /54 : IV/6 / 1 :

IV/ 10 /27 : V /3 /28 ,36 ,37

Freelin, J.R. IV/ 1/27

Freuden thal, A.M. 1/7/3 8

Fr ick , C.W. 111/2/56

Friedman, E. 1/7/41

Friedmann, P. III /7S/88

Frueh , F.J . I I I /7S/64

Fung, Y .C. I /Intro/ 48,50 :

1/2/17: 11/1/25: 11/9/42,

59: III / 1/6,26,56:

I I I /4 /36 : I I I /Chapter 7:

111/7/9,10,11,12,17,37,39,

40,42 : I I I /7S/6 ,7 ,10 ,1 1 ,

14,44 ,45 ,58 ,60 ,61,65,68,

71,73,74,88,91,93:

I V /1 / 28 : V / l / l O

Gainer , T.G. V/5 /60

Gaji,

B.

II1/7S/85

Gallagher, R.H. III/7S /5,93 :

IV/ 1/30

Gardner , C . I I /6 /43 ,57

Ga rne r, H.C. 11/ 1 2 1 :

II /3/2,37,40: 11/5/3439:

I I /10 /53 ,55 ,57 : I I / I 1/68

Garrick, I .E. II /Chapter 1 :

11/1/8,9,19,22,26,28,41,44:

II /3/2,41: 11/5/ 12,56 :

11 /6 /2 ,1 1 ,3 33 5: I I /9 /8 ,55 :

I I / l 1/68: I I I /4 /36 :

Giltner, T.A. III/7S /6 1,62

Glauert , H. I /Intro/47,48,50:

II /1/5,6,9,18,20: 11/3/31:

I I I /2 /49 : IV/7 /3 : V/2 / 13 ,44 :

V/5 /6 ,5 5,58

Glaz ebrook , R.T. 11/I 4

Goland, M . I I I /6 /3

1 :

111/7/8,

42: 111/7S/57: IV/1/2 7:

V/3 /25 ,36

Golden, C.T. III /7S/79

Goldenveiser, A.L. III/7/2 8,29 ,

32,42: II1/7S/8,94

Go ldm an, R.L. 111/7/36:

III /7S/61: IV/8/ 13: V/3/35

Goldstein, S. V/5 /5 7

GBllnitz, H. III /4S/10,13,3 5

Gontkevich, V. III /7S /82

Gonzales, R. 1/8/3 1

Goodier , J.N. IV/1 /29

Good man, L.E. 111/7/2 ,45,47:

Good man, T.R. 11/6/58

Gossard, M . L . 1/2/8,16:

Gbther t , B. I I /1 /18 ,20

Gourbil, L. II /10/38,59:

Gracey,

W.

11/6/56

Graham , E.W. 1/8/3 0

Gra y, A. 11/1/6

Greenberg, J.M. III / 10/22

Greene, R. III /7S/87

Greenspon, J.E. III /7/36 :

III/ 7S /6 1

Greidanus, J.H.

11/ 1/

18:

I I I /7S/65 ,66

1/7/40: IV/ 1/27

IV/ 10/28

Hall, W.E. Jr . 111/9/ 13 ,25

Ham, N.D. II /9/53 ,60:

Hanim, M. II1/7S/88

Harmon,

S . M .

V / l / l 1

Harper, C.W.

II/ I

1/67

Harris, G.J. II1/7S/82

Harris, R.C. V/S/S5

Hartley, D.E.

l I / l

1/63 ,66 ,69

Hartley, E.V. IV/10/27 :

Hartree, D.R. IV/ 1/2 9

Haskind, M.D. 11/2/43

Hayes, W.D. 11/1/15: 11/9/1 8,

25,26,28,40 ,55,56: 111/7/17,

37,42: III /7S/57

He ad, A.L. 111/9/21,25:

IV/7 /27 : IV/8 /14 : V/3 /8 ,34

Heard, W.L. III/7S /79, 8 1

Heaslet, M.A. 11/1/26: 11/2/28:

I I /6 /46 ,47 ,56 ,57: 11/7/75:

III /2/56,58

III/Chapter 10: 11I/ 10 /2 2

V/4 /2 1

He ath, B.O. II1/4/36

Hedgepeth,

J .M .

I/Chapter 2:

I /2 /

16:

III/3/20: 111/7/8,10,

14 ,15 I 7,19,24,25,26,27,28,

29 ,32 ,35 ,36 ,42 ,43

:

III /7S/6,

16,17,18,32,35,57,59,60,61:

I V / 1 / 2 9 : v / 1 / 1 2

Hedman, S. I I /9 /30 ,56

Helmholtz, H.L.F. (von)

He mp , W.S. I/Ch apte r

1 :

11/1/14: II /2/9: II /8/4,12

1/1 /20


24/2368

18

Hou ghton, D.S. II1/7S/68

Hovanessian, S.A. 1/6/54

Hoyle, R. 1/7/39

Hsu, C.C. 1/6/53

Hsu, K.H. III /7S/89

Hsu, P.T. II /3/2,34,37,41

I1/5/34,59: II /9/33,57

Huang,

T.C.

I /6/8,55

Huckel, V. II /2/33,44:

11/5/56: V/3/ 1,18,20,

34.35: V/5/58:

VI/TG/5,9

Hudson , M.L. I I I /7S/87

Hunsaker , J .C . l I / l /4

Hut ton, R.E. 1/8/30

Ijff, J. I I /11/8,53,56 ,66,69:

III /6/3 1,33: VI/TG/5,8

Isaacs, R.P. 111/7 /17,37 ,43:

III /7S/57

Ishii, T. III/7S/6 8,81,87

Izmailov,

A .

III /7S/9

I

Jaeckel, K. 11/3/33

Jaeger, J.C. 1/7/ 39

Jahn, H.A. I1/2/28,4 4

Jeffreys, H. 1/3/ 37: 11/7/75

Jeffreys,Lady. 11/7/75

Johns, D.J. III /7/18,20,21,43,46:

III /Chapter 7s: 111/78/8,62,65,

66 68 70 74 75 76 77 79 8

1 3 3 ,

9 2 ,9 3

Johnson, H.C. 11/9/60: II /10/35:

V/5 /1 6 ,2 5

Kacprzynsk i, J.J. 11/9/3 1,32,33,35, Lall,

T.R.

I11/7S/8

1

Lamb, H. 1 /8 /29 : I I / I /4 :

7 ,57 ,58

8 2 ,8 8

Kaliski, S. III /7S/66,7 1,78,80,

Kalnins, A. 1/8/ 3

Kana, D.D. 1/8/3 1,32

Kantorovich, L.V. III /7S/6,35,93

Kaplan, S. 11/9/54

Kappus, R. III /6/5,33

Karamcheti , K. III /7S/86

Kariappa. III /7S/90

Kell, C. IV/9/

15

Kell, R.J. III/3/ 20: V/ I / 12

Kelsey, S. I I I /2 /2 6

Kelvin, Lord. 11/1/4,5 ,6,14:

II /8/4: III /7/34

Kennedy, C C. I /3/20,3 5,38 :

1V/7/25 : IV/8 /3 : IV/10/8 ,27

Kennet t , H. I I I /7S/65

Ketter , D.J. 111/7S/76,85

Keune, F. 11/1/13

Kind, R.J. 11/9/4,9,59

Kinnaman, E.B. IV/7 /27:

Kirkby, W.T. 1/4/49:

Kliauz, L. 111/7S/85

Klotter , K. 1/6/53

Knechtel , E.D. V/5 /61

Kobayashi, S. II1/7S/45,72,75,

Ko b e t t ,

D.R.

I I I /7S/10 ,73 ,76 ,

Konditsina, E. 111/7S/87

1V/8/ 13

IV/Chapter IO:

IV/

10/27

76,79

77,83,84

I1/5/32,58

Lambourne, N.C. I I / I / 17:

I I /10 /33 ,58 : I I / l1 /45 ,68 :

IV/Chapter 6 : IV /7/ 12:

V/2/28,34,35,38.45:

V/Chapter 5: V/5 /5 7 ,5 8 ,5 9

Lamper, R.E. I11/7S/65,74

Lanchester, F.W. I / In t ro /45 ,

Lanczos, C. III /2/57

Land , N.S. II1/7S/8 9

Landahl,

M .

l l / l / l 5 , l 9 :

11/2/ 1,42: II /4/2,7,49,52,

61,119,120: 11/7/75:

II /Chapter 9: 11/9/13,20,

22,3 1,54,55,57,58:

II/ 10/36 ,37 ,38 ,39 ,42 ,53 :

II1/7S/ I4,94: V/ 5/4 3:

V/5 /6 0

49: 11/ 1 /4

Langley, R. III /7S/78

Laschka, B. III/4S/ I0,35

Lauten,

W.T.

I V/C h ap te r 1 :

Lawrence, H.R. I I / 1/20:

IV/ 1/29: IV/9 / 1 5

II /6/55,57: I I / 10/23 ,30 ,32 ,

56 : l l / l l / l O , l I , l 2 ,1 8 ,2 1 ,

26,27,3 9,66: V/6 / 5

Lazennec, H. III /Chapter 8

Leadbetter . S.A. I1/10/32,58:

I I /11 /65 ,66 ,69 : V/3 /35

Leclerc, J. I/Chap ter 4(D)

Lee, E.H. 1/7/ 39


25/2368

19

Lighthill , M.J. II / l /I 1 ,15,26:

11/2/23: 11/7/75: 11/9/1,8,19,

25,34,35,37,39,54,55,58,59:

I I /10 /54 : I I I /2 /58

Lin, C.C. 11/1/18: II/2/1 ,42:

11/4/ 1

19:

I I /9 /50 ,60

L in , H . V / l / l I

Lindholm, V.S. I /8/ 3 1 :

Linebarger , J. I I /9/50 ,59

Lisunov, A.D. III /7S /66

Livanov, K.J. II1/7S /64,78

Lock, M.H. l11/7/ 12,4 4:

II1/7S/94

III/7S/10,62,63,68,71,72,

7 8 ,7 9

Loewy, R.G. lI l /9 / 1 1,24,25:

Ill/

10/2 1

Lofts,

M.

I I / I 1 /68

Lohmann, K. III/4S/ 10,35

Loiseau, H. 1/4/20,41,87 :

V/

S / 50 s

9 ,6 0

Lom ax, H. II / 1/26 : 11/2/28,

44: II/Chapter 6: 11/6/55,

56,57,58: 11/7/75: III /2/58

Love, A.E.H. 1/1/2 0:

111/7S/7,93: IV/ 1/2 8

Lowson, M.V. 11/7/75

Luce, R.G. III /7S/75

Luessen, G. III /7S/7 1

Luke, Y .L. III /6 /3 1 : 111/7/8,

16,18,42,44,46: III /7S/57,

58 ,59 ,61 : IV/1 /27

Luscombe, P.D.R. IV/1 0/27

Lyo n, H.M. II1/2/56:

1II/3/20: 113/7S/92

h-ahortikh, Zh.K. I lI /7/ 1

Malain, E. III/7S /90

II1/7S/63,65

47 :

Mangler, K.W. I1/3/34 ,42:

II/4/2 7,1 19: 11/5/42:

11/

10/36 ,39 ,59

Mannes, R.L. V/S /58

Mansfield, E.H. III /4/2 6,36

Manson, P.W. 1/4/ 86

Marchenko, G. I I I /7S/84

Marguerre, K. 1/7/27 ,40:

Markorov, B.P. III/7S /67,6 8

Marshall,

P.L.

V/5/61

Martin, D.J. 11/ 10/54:

I I I /7 /23

IV/Chapter 1 : IV/1 /29 :

V/6 /55

Martucelli, J.R.

I I /

1

O/

6 3 5

Mar tz, C .W. I I / l 0 /5 8 :

V/5 /32 ,58 ,60

Mathews, C.W. III /7S/92

Mathews,

G.B.

11/1/6

Matsensaki,

Y.

III /7S/79

Mayo , A .P . I V /1 /3 0 : V / l / l I

Mazelsky, B. I I / 1/19:

11/6/55,56

Mazet, R. Edi tor of Manual:

1/4/ 12,2 1,72: lI /8/3, 42:

IV/5 /54 : IV/ 1O/ 7,19,28

Meek ishef, G.N. 111/7/47:

III /7S/63

Melan, E. 1/7/3 8

Mendelson, A. V/5 / 14,5 6

Menees, G.P. 11/ I 0 /2 3

Menkes, E. III /7S/89

Minhinn ick, I.T. I/2 /

15:

I1/10/53,54: lr / l1/19,21,31,

32 : V/6 /56 : VI /TG/4 ,5 ,8 ,9

Mirow itz, L.I. 111/7S/72

Mirsky, 1. I11/7/43

Mitchell, C.G.B. III/ 4/3 7

Mitchell , D.H. III /7/37 ,44:

Mitchell, R.R. III/7S/91

Moiseev, N.N. I/8 /28 ,3 1

MolloChr is tensen , E . 111

I /

18:

l1/2/

1

:

II /4/

1

19: IV/ 1 /5 ,29:

V/5 /41 ,59

Molyneux, W.G. II /10/2 3,33,

56 ,58 :

l I /

11/29,30,67:

IV/S/S4,5 5,56,57 : lV/6 /25 :

IV/Chapter 9: IV/9 /15 :

V/2/5,l0,13,14,23,28,40,43,

44,46: V/Chapter 6: V/6/25,

55 ,56 ,57

III /7S/6 1

Monfor t , J .C . I I / l 0 /5 3

Moore, F .K. I I /9 /39 ,41 ,53 ,59 ,

Moore, J.A. 11/10/46,47,60

Moore, M.T. III/7S /74

Morgan, H. II1/7S/61

Morins,

L.

II1/7S/84

Morse, P.M. 11/3/3,8,41

Moseley, W.C. II/1 0/5 9:

V/S/60

Moss, G.F. II/ I0 /30 ,57 :

IV/5 /57

Movchan, A.A. l11/7/ I0,17 ,29,

44: III /7S/6,16,20,59,60,

65 ,72

6 0


26/2368

2 0

Ni ble tt, L1.T. "Chapter

5

Niesytto, J . III/7S /68

Nixon, D. V /2/4 6

Noll,

R.B. III/7S/70

Novichkov, 1u.M. III/7S/67,7 I

Novozhilov, V.V. I II/7 S/8 ,93

Nowacki, W. 1 /7 /39

O'Brien,

T.F.

III/7S/65

Oberhettinger, F. 11/2/44

Odqvist, F.K.G. 1/7 /39

Ogibalov, P. III/7S/82

Oglesby, T.H. IV/

1/30

Olson, J .J . III/7S/6,10,45,76

Olson, M.D. II/9/5 0,59:

u1/7S/80,83,87,88,89,9

1

Olsson, C.O. II/10/ 39,59 :

IV /5 /54

Orlik-Ruckem ann, K. 11/9/41,

42,46,48,49,59:

I I /

10/39,47,

48,59,60: IV/5/54,57

Osgood, W.R. 1/7 /39

Ostrach, S. 11/9/413 9

Oswatitsch, K.

11/

I / 13

Ott o, E.W. 1/8/3 2

Owen, T.B. IV/5 /57

Pai,

S.1.

I I I /2 /56

Paidoussis, M.P. III/7 S/8 5

Pancu, C.D.P. 1/3/20,3 5,38:

IV/7/25: IV/8/3: IV/10/8 ,27

Parks, P.C. III/ 7/4 6: III/7S/ 17,

66,80,87,88,89,90,94

Parkus, H. 1/7/3 8

Presnell, J.C. II1/7S/68,74

Press,

H.

I I I /4 /37

Preston , J.H. 11/1/14

Price, G.W. V/ 5/ 60

Pride, R.A. III/7S/77

Pritchard, A.J. III/7S/20,89,

Probstein, R.F. II/9/28,40,56

Pugh, P.G. I1/10/18 ,55:

Pugsley A.G. I/Intro/47

SO:

Puttick , E.B. V/ 2/ 14,21:

90,94

v/s/ss

I I I /2 /56: I I I /3 /20

V/6 /25

Quinn, J .F . IV/1/30

Quoz zo, G. 111/7S/76,77,91

Raab, A. I/Intro /49

Rab inovic h, B.I. 111/78/63

Rabinovich,

F.I. I/8/

15,3

1

Rabinowitz,

S.

I I /2 /26,44:

VI/TG/4,8

Rainey, A.G. II/9/5 2,60:

Ill 10/54: HI/ 0/22:

VIS/ 14,26,56

IV/S/SS: v/3/34:

Ramberg, W. 1/7/39

Randall, D.G. 11/7/75:

Rand als, W.C. II1/7S /58

Ransleben, G.E. Jr . 1/8/3 2

Rattayya, J .V. 1/8/3 0:

II1/7/2 1,22,45,4 6,47:

I I /9 /38,58

Rich, R.L. III/7S /79

Richardeau, IV/ 10/2 8

Richardson, J.R. 11/1/21:

11/3/2,3,10,37,41: 11/4/1 19 :

I I /5 /34,58:

11/10/55:

111/7S/92: 111/9/ 13,1 4,16 ,25

Richey, G. I/6/4 6,54

Riley,

1/8/50

Ripley, J . I I I /2 /56: I I I /3 /20:

III/7S/92

Roberson, R.E. I /6/25 ,54

Robinson, R.C.

II/

10/38,59:

v /5159

Rodden, W.P. 1 11/7 /9, l6, l7 ,18

19,35,36,44,45,47: III/7S/5,

7,41,61,63,70,78,93:

IV/ 1/28

Rodriguez, A.M. 1 /8/ 30

Rogers,

M .

1/8/32

Roos, H. IV/1 0/27

Rose, R. 11/10/40,59

Rosenbaum, R.

I I /

1/26:

Rosenberg, R.M. I/6/5 4,55

Rosencrans,

M.

I I I /7S/64

Roshko, A. 11/1/26: V/5 /23,58

Rost , J . IV/3/21,30

R o t t , N . l l / l / l 5 , l 8 : 1 1/ 2/ 36 ,

37, 44 : 11/9/5 1,60

Row , P.V. II1/7S/75

Routh , E . J . I / In t ro / lS -16

Roxbee Cox,

H.

I / In tro/38,47,

49,SO: III/3/20: V/

I / 1 1

Rubbert, P.E. II/ 9/20 ,22,23 ,

IV/ 1/28


27/2368

21

Schaeffer, H.G. III/7S/79,8

1

Schindler, A . 11/2/45: V/6/56

Schmieden, C. 1/6/37,41,53

Schnittger,

J.R.

III/10/22:

Schuchardt, H. 1/6/54

Schuerch,

H.U.

I /2 / 16 :

I I I /2 /57:

IV/

1/27

Schult,

E.D.

V / l / l 1

Schwartz, I. II/I 1 /68

Schwartz, L. 11/2/ 16,4 2:

I I /8 /3 , 4 , 42 , 43 : VI /T C/5 , 8

Schwarz, M.D. 1/4/40

Schwarzchild,

K.

11/4/38,120

Scruton, C . 11/10/16,25,30,52,

55,57,58,60:

I I / I

1/35,68:

IV/5/55,56: IV/Chapter 6 :

IV/7/

1

2,27

:

V/5/23,5

5 , s

7

58

Sears, W.R. 11/ 1/8 ,9: 11/4 /69,

71,80,100,120: II/6/47,55,

57: I I /7 /12,74: I I /9 /33,57:

I I I /2 /56

V / 5 / 5 6

Sep, Z. III/7S/68

Sethna, P.R. I /6 /8 , 54

Sewall, J.L. IV/1/28: V/2/45:

Shal'da, L.M. I I I /7S/81

Shandarov, L.G. III/7S/74,89

Sharpe, G.D. V/3/27,28,36:

V / 6 / 5 5

Shen, S.F. 1/6/22,53: 111/7/10

1

1,36,37,40,45: III/7S/57,

59,63

v / 3 /

1

Shenhman, A.M. III/9/25

Sobey, A.J. III/7S/83

Sohngen, H. II/2/16,42:

11/6/55: III/2/58

Sokolnikoff,

E.S. IV/

1 /30

Sokolnikoff , I S . IV/1/28,30

Solarz,

L.

III/7S/7 1,78,83,85

Somashekar

,

B. R.

III /

7S / 9 0

Sommerville,

D .

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Sorensen, R.M. II / 1O/ 4 3 4 :

V/5 /48 , 5 9

Souriau,

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11/4/27,] 19

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Spriggs,

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III/7S/90

Squire, H.B. 11/1/14

Stahle, C.V. IV/2 /21: V/3/ 35

Stark,

V.

III/7S/94

Stearman, R.D. III/7/36,37,

38,45: III/7S/ 10,63,7

I

,73,

76,79,84,86,89,90

Stein, M . 1/2/13,14,16:

II1/2/57: IV/1/28

Stenton, T.E. II/9/33,57

Stepanov, R.D. III/7/25,26,28,

29,32,45: III/7S/60,64,65,67

Stephens, D.G. 1/8/29,30,50

Stephenson, J.D. V/5 /41 , 58

Stepniewski, W.Z.

HI /

10/2

1

Sterne, L.H.G. IV /5 /56

Steuding, H. 11/8/43

Stevens, J.E. 11/6/57:

I I / I

1/9,

Testa, R.B. 1/7/41

Theodorsen, Th. I /Intro/47,5

0:

11/1/6,8: II/2/10,42: 11/6/14,

2

1

: 11/8/30: 11/ I0/6:

11/ 1 1/6 8: 111/9/ 1

1 :

IV/7/3,

26 : V /3 /18 , 34 : V /6 /55 :

VI/TG/ 1 ,2 ,3

Thielemann, W . 1/6/46,55

Thomas,

H.H.B.M. I I / I

1 /68

Thomas, M . III/7S/68

Thompson, R.F. I I / l 0 / 5 9 :

Thomson,

R.G.

III/7S/72

Thomson, W.T. I I I /3 /20

Tijdeman, H. VI/Tables and

Graphs

Timman, R. 11/

I /

18: 11/2/26,

43 : 11/3/ 16,4 1: 111/9/

I I

,24:

I I I /10/22: IV/5/58

Timoshenko,

S.

1/7/40:

III/7S/8,93:

IV/

1/29

T obak ,

M.

11/6/58: II/9/38,58:

II/ 1

0 / 32,3 3,46,47,5 8,60 :

v / 5 / 1 0 , 5 5

V/5 /60 , 6

1

Tolins, I.S. 1/7 /39

Tommassoni, J.E. V/2 /45

Toulson, K.W. I11/9/9

Traill-Nash, R.W. 1/3/35,38:

Trembath. 1/8/50

Trilling, L. 11/1/17: V/5/41,59

T rou tm an , J.L.

11/

10 /23

Truber t , M . I I /10/54: IV/5/55

Tsein, H.S. 11/1/18: 11/2/1

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Vlasov, B.F. 111/7S/62

Vlasov, V.S. II1/7/4 6

Voight, H. IV/7 /3 : V/3 /25 ,

28.36

Volkof, A.N. III/7S/62,9 1

Volterra, E ., I /3/ 14,37

von Baumhauer, A.G. I /Intro /46

. von Borbely, S. I I /2 /28 ,44

von Gorup , G. I I /8 /3 ,42 ,43

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III /7S/49: V/3/35

von Mises, R. II /8/19 ,21,3 7,38:

III/4S/13 17 19 20 21 25

von Schlippe, B. IV/10/ 2,27

Voss, H.M. 11/1/21: 11/5/15:

III /7/28,32,33,46:

III /7S/8,42,44,65,67,

74,75,76,77

Wagner, H. I /Intro /47,50 :

11/

1/5 ,8 : I I /6 /2 ,5 ,10 , 1 ,55:

II/8/13,43: 111/4/31,32:

I I I /6 /3 1 : I V/7 /3

Walker, P.B. V/ 6/55

Walker, R.W. III/ 7S /80

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Walshe, D.E.J. V/ 5/2 3,5 8

Walter, F. V/3/25 ,28 ,36

Walters, R.E. V /l / l

1

Walton, W.C. Jr. 1/8/30:

Waner, P.G. 1/2/16

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Webb, G.R. III/7S/88

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Weeks, G. III /7S /94

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2 1,22,23,25,3 6: 111/6/ 19,20,

33:

II1/7/46

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55: II /1/21,42,43: 11/4/1 19:

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54,56,57: 11/ I0 /20 ,25 :

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Zeydel, E.F.E. III/7/23,24,4 7:

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23

MANUAL ON AEROELASTICITY

VOLUME I INTRODUCTORY SURVEY

PART I

STRUCTURAL ASPECTS

VOLUME I1 PART

I1

AERODYNAMIC ASPECTS

VOLUME I11 PAR T 111

PREDICTION O F AEROELASTIC PHENOMENA

VOLUME IV PART IV

EXPERIMENTAL METHODS

VOLUME V PART V

FACTUAL INFORMATION ON FLUTTER CHARACTERISTICS

VOLUME

VI

PART VI

COLLECTED TABLES AND GRAPHS

General Editor

R.Mazet

C ONTENTS O F VOLUME I

W.J.Duncan Intro duct ory Survey

PART I - STRUCTURAL ASPECTS

Aug.1959*


30/2368

D.E.Williams Three-Dimensional Subsonic Th eor y

D.E.Davies Three-Dimensional Son ic Th eory

C.E.Watkins Three-Dimensional Supersonic Th eor y

H.Lomax Indicia1 Aerodyn amics

D.L.Woodcock Slender-Body Th eory

Revision

H.G.Kussner Non-Stationary Theory of Airfoils of Finite

Thickness in Incompressible Flow

Thickness and Boundary-Layer Effects

.T.Landahl and

24

CHAPTER 3

CHAPTER 4

CHAPTER 5

CHAPTER

6

CHAPTER 7

CHAPTER

8

CHAPTER

9

CHAPTER 10

CHAPTER

11

Jan. 196 1

Nov. 196 0

Nov. 196 0

Nov. 1960

Apr. 1962

Nov. 196 7

Dec. 196 0

Mar. 19 69

H.Ashle y

A revision of he original chapter by H.Ashley and G.Zartarian,

Nov.1960

W.E.A.Acum

The Compar ison of Theory an d Exper iment

for Oscillating Wings

P.R.Guyet t Empirical Values of Derivatives

May 1962

Mar. 196

1

Feb. 1963

Sep. 1967

Nov. 1963

CONTE NTS O F VOLU ME I11

PART I11 - PREDICTION O F AEROELASTIC PHENOMENA

CHAPTER

1

E G B r o a d b e n t

An Introduction to the Prediction of

Aeroelastic Phenomena

Revision

Divergence and Related Static

Aeroelastic Phenomena

CHAPTER

2

F.W.Diederich


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.-

PART IV

-

EXPERIMENTAL METHODS

CHAPTER

1

CHAPTER

2

CHAPTER 3

CHAPTER

4

CHAPTER 5

CHAPTER 6

CHAPTER

7

CHAPTER

8

CHAPTER

9

CHAPTER

10

D.J.Martin and

T.Lauten

R.C.Lewis and

D.L.Wrisley

H.Gauzy

J.C.Hall

J.B.Bratt

C.Scruton and

N.C.Lam bourne

L.S.Wasserman and

W.J.Mykytow

L.S.Wasserman and

W.J.Mykytow

W .G

. oly neux

M.O.W.Wolfe and

W.T.Kirkb y

Measurement of Structural Influence

Coefficients

Ground Resonance Test ing

Measurement of Inertia and Structural

Damping

Experimental Techniques for the

Measurement of Power -Co ntro l

Impedance

Wind Tunnel Techniques for the

Measurement of Oscillatory Derivatives

Similari ty Requirements for Flut ter

Model Testing

Model Construction

Wind Tunnel Flut ter Tests

Rocke t Sled, Ground-Launched Rocke t and

Free-Falling Bom b Facilities

Flight Flut ter T ests

C ONTENTS OF VOLUME

V

25

Oct . 196

1

Dec. 196

Feb. 196

June 1964

Jan. 196 1

Nov. 1960

Jan.

I

96

1

Jan. 1961

Jan. 196

1

Dec. 196

1


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Documents

Manual of Aeroelasticity