AGARD Report No.578

NORTH ATLANTIC TREATY ORGANIZATION

C ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT

(ORGANISATION DU TRAITE DE L'ATLANTIQUE NORD)

MANUAL ON AEROELASTICITY

SSUBJECT AND AUTHOR INDEX

Edited by

E.C.Pike

This publication is sponsored by the Structuresand Materials Panel of AGARD

Li

Published January 1971

533.6.013.42(083.86)

Printed by Technical Editing and Reproduction LtdHarford House. 7-9 Charlotte St. London, WIP IHD.

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FOREWORD

The Subject Index and Author 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 AGARDReport series.

The Indexes are published in two forms: in the AGARD Report series asAGARD Report 578 and in looseleaf form for insertion in Volume VI of theManual.

Entries are given by Volume, Chapter and Page number. For example, 11/9/56denotes Volume 11, Chapter 9, page 56. The letter S after a Chapter numberdenotes a Supplement to that Chapter. The letters TG denote the section of Tablesand Graphs in Volume VI. The abbreviation INTRO denotes the IntroductorySurvey in Volume 1.

A.JBARRETrChairman, Structures and Materials Panel

ifii

CONTENTS

Paoe

FOREWORD ii

SUBJECT INDEX 1

AUTHOR INDEX Is

LIST OF CONTENTS OF MANUAL ON AEROELASTICITY 23

iv

SUBJECT INDEX

Abel's theorem 11/2/40 Altitude effectsAblating plates 1/7/37-8 flutterAcceleration effects IV/9/14-15 control surfaces 11115/10: V/3/21Acceleration potential 11/1/13-14 panels 111/7/14Accelerometers IV/1/25-6,27: IV/5/39: wings V/2/25-7

IV/7/25,26 massbalance V/4/7,9-1 2Accident investigation 111/5/2 models IV/6/ 11- 17,20-23: IV/7/14Ackeret theory I11/7S/1 0,16,41,49 AluminiumAcoustic resonance IV/5/54: IV/7/13 paneis 111/7/10-16,18,22,24: 1I1/7S/27-9,33,40Actuators 1/5/8-19,29-33,35-41 cylinders 111/7/26-8: III/7S/41Admittance concept IV/2/3-4,12,20-21 "Amplitude response" technique IV/10/5-7Aerodynamic aspects Volume II Analogue methods IV/7/I-2

historical review 11/1/3-9 Angle of attack, definition 111/2/25-6methods of analysis 11/1/9-25 Ankylosis 1/6/40,51

Aerodynamic centre position 11/9/1: Apparent mass concept 11/6/7,12V/ 1/3,5,7: V/6/19-21,25,28 Approximate methods

Aerodynamic coefficients see Derivatives aerodynamic forces 11/5/11-55Aerodynamic forces flutter V/Chapter 6

approximations 11/5/11-55 static aeroelasticity 111/2/12-38: 111/3/5-11,14generalised Arrowhead wings 11/5/14,36-8: 11/10/25-8

definition I/INTRO/2 Aspect ratio effectsformulae i1/Chapter 4: 11/Chapter 7: on buzz V/5/49,50

111/4/4,27: 111/7/7: 111/8/9-12,17-20 on derivatives 11/11/27-30,40!41geometry 111/2/20 on divergence 111/2/3measurement 11/1/22-3 on flutterpropeller 111/9/5-7,10-13 control surfaces V/3/8

Aeroelastic phenomena panels 1!/7/24: II1/7S/41,50,51aerodynamic aspects Volume 11 pure pitching V/5/21classification 1/INTRO/I 7-21 wings V/2/10-13: V/6/26design implications i11/2/9.54-5: 111/3/18-19 on negative damping V/5/9-10history I/INTRO/45-8 Asymptotic solution 1/4/9practical aspects I/INTRO/44-5 Atmosphere line IV/6/19,20prediction III/Chapter I "Automation" of flutter calculationsstatic III/Chapters 2 and 3 lIl/Chapter 4S

Aerofoil section effects Autopilot III/Chapter 8on buzz V/5/48 Axes, reference 111/2/25on pure pitching V/5/21on wing flutter 11/9/1: V/2/5,15-16 Backlash

Aerofoil theory control circuit 111/5/2comparison with experiment 11/10/6-18,48-9 non-linearity 1/4/19: 1/6/1,2,46-9non-stationary (unsteady) lliChapter 8 powered controls IV/4/7

symmetric aerofoils 11/8/18-38 rigid drives IV/5/39supersonic and hypersonic 11/9/9-28 tabs 1/INTRO/44

Aeroisoclinic condition 111/2/16,18,55 tailplane 111/5/7Aeronautical Research Commitbxe I/INTRO/46-7 Baffles 1/8/4-12,44-7,50,51A.G.C. technique IV/5/30 Balance, aerodynamicAileron effect on aileron flutter V/6/37-9,42

buffet 111/5/4 effect on buzz V/5/50.51derivatives 11/11/39 horn 11/11/45-7effectiveness V/1/6-7 nose 11/11/47-52flutter IV/9/12-13: V/3/16,17-23,24: sealed or internal (Irving) 11/ 11/52-9

V/4/8-10,12,13-14 tabs 111/5/15impedance test IV/4/8-13 Balancing of forces 111/2/55inboard 111/3/19: V/1/9 Ballast weights V/3/12,31-32reversal V/1/5-9 Basile's hypothesis 1/3/37: 1/4/11,15,82tip V/I/9 Beam vibration

Airship-flow concept II/1//19 simple beam theory 1/2/5-6,8,14: 1/3/31:All-moving controls see Tailplanes I11/1/4-5,19: 111/2/24-30,40-44: 11/3/14

thermal effects 1/7/12-16,19-21,30-34

2

Bearings IV/5/7-8 Cathetom',ter IV/ 1/15Bending moment Cauchy-Riemann equations 11/8/4

idealised 111/2/15,20 Centre of gravity effectwing root V/I1 /3-4 body-freedom flutter V/2/4 1-3

Bending rigidity control surface fljitter V/3/ 18: V/6/52panels 111/7/15,17,10: 111/7S/ 18 Centre of pressure effect 111/4/24: 111/5/9:

Bernoulilli's equation 11/7/6,9,13,62,63: 11/8/ 14 V/1/5: V/2/4: V/4/13Biconvex aerofoils Characteristic equations 1/4/3,6,10

damping in pitch 11/9/14,18 Characteristic phase lag 1/3/1,24-7pitching derivatives 11/ 10/ 17 Characteristics, method of 11/9/33

Bifurcation 1/6/36,37 Charts, static aeroelasticity 111/2/24.- 111/3/10-11Binary flutter "Choking!' frequen;y, autopilot 111/8/23,28

approximate formulae V/6/7-12 Circulation function see Theodorsen functioncontrol surface V/4/6-15 Collocation method see Kernel function proceduredefinition 1/INTRO/24 "Comfort stall" (blades) 111/10/17

Biot number IV/6/26 Component Analyser Technique IV/2/3,l 8-20Biplanes, flutter of 1/INTRO/46-7 Component resolvers IV/5/51-2Blades Compressibility effects see Mach number effects

flapping 111/9/13-16: 111/ 1 Oj10, 11 Compressor blades see Bladesflutter I/INTRO/25-6: IIl/Chapter 9: Computers use in

III/Chapter 10: V/ 5/25 autopilots 111/8/13ground testing 1/4/73-87 dynamic stability 111/6/29

Blasius procedure 11/8/2 2 general 111/1/13: Ill/Chapter 4SBodies of revolution, slender 11/7/11.16,32-48 influence coefficients 11I/7S/10: IV/l/27Body-freedom flutter V/2/3,41-4: V/6/42 model testing I1/7/IBody freedoms 111/6/4,9,11,22 non-linear problems 1/6/24-5Bomb, free-falling IV/6/21: IV/Chapter 9 panel flutter 111/7S/7Bond number 1/8/23,28,70,71 propeller flutter 111/9/21"Bonkere" 1/INTO/35 Cones, circular 11/7/43-5,58-61: 11/9/37,49Boom-mounted lifting surface V/ 1/ Conformal mapping 11/2/1.1,12: 11/4/81-4:Boundary conditions 11/8/3-3 8

general aerodynamic 11/1/14-15 Continuous media, damping 1/3/14-15indicial function 11/6/2-4 Continuum methods 1/2/1,12,13lifting surface 11/5/7-9 Contours, flutter speed V/2133slender body U/l7/7-9 Controlstructural vibration 1/2/4-5: 111/7/7: 11I/7S/9 irreversible V/3/ 18

Boundary layer lateral V/1/7-9attac-hed 11/9/39-46 law 111/8/12-13,21"compliance" 11/9/42-6,49 linkages V/3/29,33displacement thickness 11/9/39-42,48 loop 111/8/25effects Il/Chapter 9 loss of Ill/Chapter 3

panel flutter III/ 7S/13,14,29-32,44 restraint V/3/ 10idealised 11/9/42,45: 111/7S/ 13,14 torque 111/8/2,12time-dependent 11/9/38-53 Control circuit 111/3/1-3,4,8, 19: 111/5/2:see also Separation P1/9/14

Boundary-value problems Control points, lift functions 11/5/51-5classical 11/1/20 Control reversal see Reversalthree-dimensional 11/4/38: 11/5/1,2,5-9 Control surfacetwo-imensional 11/2/4-6,11 balance 1/4/43-5

Box methods 11/5/19-29: 11/9/31 coupling with airframe 1/5/34-5Bubbles, in propellants 1/8/22 degrees of freedom 111/4/11-12Buckling derivatives lI/Chapter 10: 11/1 1/7,33-60:

Euler Ill/7S/17 VI/TG/4-5, 15-24,42-138panels 111/7/10,12,37-41: III/7S/47-54 flexibility 111/3/2-3,4,8,19skin 111/1/7-8 flutter 111/4/22-3: V/Chapter 3: V/5/26-54:thermal 1/7/19-29,35-7 V/Chapter 6

Buffeting 1/INTRO/20-21 ,40-41; 111/5/1l: pround testing 1/4/42-9V/5/1,14,41,53 linearised sonic theory 11/4/63-8

Buzz 111/5/10-11: V/5/26-54 pressure distribution 111/3/3profile discontinuity 111/5/I11

Calibration of equipment IV/5/33, IV/10/23 Control systemsCantilever wings, flutter 111/1/4: 111/4/2: manual 1/4/46-8: 1/5/1,6-8

V/6/14,16 powered 1/4/48-9:1I/Chapter 5: V/Chapter 4Castigliano's Theorem 1/7/8

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Coordinates Damnpometer 1V/5/ 14-16transformation of 1112/6-8: 11/3/27 Datafixed 11/3/3-6: 11/4/3 aerodynamic 111/2/46-52: 111/3/15-17:moving 11/3!6-10 111/5/9-11Islender-body theory 11/7/6 inertial 111/2/51elliptical 11/7/26 structural 111/2/39-46: 111/3/14-15

Coplanar motions 1/4/2 Data recordingCord, trailing-edge 1111/15/I analysis IV/9/1O-13Coriolis £Xffects 1/8/13: 11/9/28: 111/4S/5 automatic 1'/1//19,26,27Cosine curves IV/3/11-14 magnetic tape IV/5/14: IV/IO/7,17,18Cosine factor, sweepback V1/2/6,10 manual IV/l/26Coulomb damping '1/3/33 methods 1/4/30Counter, electronic 1'1/5/53 optical trace 1V/ 10/19Coupling photographic 1'1/5/ 13,48,49

aerodynamic 111/1/10: V1/2/3,23 Definitive methods 111/2/24-32: 111/3/I11-14coefficients 1/INTRO/36-7 Deflation, method of 111/6/9,18-21frequencies V/3/ 15-17 Deformationinertia 111/5/9,11: V1/2/3,27: V/3/6,9-14 effect on autopilot 111/Chapter 8

Cramer's rule 111/6/32 shear 1/2/14Creep 1/7/4-6,27-9 structural 1/Chapter 1: 111/2/29-30Criteria, flutter Delta wings

binary systems V1/6/9-11,34 derivatives 111/ 10/28,29-33,34,38-40,46-7,5 1:control surfaces W13/4,8 I1/I1/ 17-19,27,31-2mussbalancing V1/3/14,20 flutter V1/2/13,19,37,41-4: V/5/32,50powered controls V1/4/6-7 lift distribution 11/5/51-5tabs W13/25,27-8 model tests IV/8/9,10wings '1/2/19 shear deformation 1/2/14

Critical speeds, prediction 1II/Chapter 1 thickness effects 11/9/31-3Cross inertia '1/4/7,9 Density, airCross stiffness '1/3/13: '1/4/3,8: V/6/47-8 effect on whirl flutter 111/9/17-18

effect on wing flutter '1/2/25-7d'Alembert's principle 1/7/19: 11/6/ 13,!4 variation in tests; IV/5/12: l'1/6/2,8-l 7,20-23:Dampers 111/5/9,11,14: W13/9,29-31: IV/7/14

W15/53,54: '1/6/55 DerivativesDamping aeroelastic effects 111/2/5-7

autopilot 111/8/11 approximations '1/6/1,18-22,35-7coefficient l/INTRO/9: 1/3/19: 11/9/18: calculation of Il/Chapter 5: 11/8/15-18,34-8,42:

1'1/2/ 10-12: 1'1/3/4,7-21 I: '/5/28 III/4S/29decrement 1/4/24 comparison of theory with experimentdistribution 1/4/11-14 11/10/6-51effect on flutter control surfaces

blades 111/9/7: 111/10/13-14,17-20 subsonic '1l/TG/5, 15-19,42-75control surfaces l'1/4/ 15: '13/6-9,33: supersonic '11/TG/5 ,20-24,76. 138

V1/4/8,13-15: '1/5/32,36,47,48: '1/6/55 conversion formulae (notation) '1l/TG/6-7panels 111/7/33,35: 1lI/7S/9,1I7-19,27,39,42-S definitions 1/INTRO/ 10-12: 1/I/l/1,8:wings '1/2/22-3 11/10/5-6: 111/1/17

effect on resonance 1/Chapter 3 empirical values 11/Chapter I Ifuel sloshing 1/Chapter 8 linear systum 11/1/23hereditary 11311,5-11 measurement IV1/Chapter 5hysteresis I'1/5/l 1: IV/1/0/9 pitch-damping 11/9/18loss of 111/5/4,11 propeller 111/9/10-11matrix 1/3/2,22-3: 1/4/5,18,24: 111/4/ 11,27 rigid-body 111/1/18measurement 1/4/38-40: l'12/l 0-12: slender-body theory 11/7/45-8,57,59-60,73-4

I'1/3/ 1-23 slender-wing theory 11/7/23-5mechanical '15/4,25 strip theory 111/4/4-5nacelle 111/9/9 tab 111/5/14negative Vi/5/ 1,2,6-11,26-7,43-5 wingsnon-_linear 1/6/51-3: '1/5/34 subsonic '11/TG/4,l 1-12,26-30parameter 111/4/17 supersonic '11/TG/5,13-14,3 1-41prediction of 11/10/12,13,28-32,44-7: De-sensitising ratio l'1/4/18

111/ 1/3,8-9,17: H1I/4/Il Dial gauges IV1/1//4-l 5,16: lV/7/23ratio 111/8/8,26: 111/10/17: IV1/ 10/ 1,11-14,16,17 Differential transformer '1/ 1/18,19,20:representation of l/INTRO/8-9: 111/1/20 1'1/7/23temperature effect 111/1/23 Dihedral effects 111/2/6-7test equipment 1/4/62: 1'1/5/7,8,24,3 I Dirac delta function 111/6/6

4

Dirichlet problem 11/9/33 Expansion method 11/5/13-14,27-9: 11/8/3Discrete methods 1/2/1-2,12 Experimental methods Volume IVDisplaced frequency method 1/4/17,'8,82-3 comparison with theory 1l/Chapter 10:Displacement 111/1/22,24-6: 111/9/14-16: IV/10/25

functions I/INTRO/6-9 influence coefficients IV/Chapter Iformulation 1/7/7 static aeroelastic effects 111/2/51-2: 111/3/17-18

Dissipation function 1/4/5-6 Explosive charges 111/4/29Divergence External stores

blades 11/10/10-12 effect on derivatives 11/I 1163-6: 111/1/18general h/INTRO/18-19,21-2: 111/1/1,2: effect on divergence IP/2/4

111/Chapter 2: V/Chapter I effect on wing flutter 111/5/5panel flutter 111/7/27,28 models I11/1/19: IV/7/8,17: IV/8/6,12record analysis IV/9/10 optimum position 111/2/55

Donnell equations 111/7S/45,47 rotatory inertia 1/2/9Doppler equipment IV/9/3-4 vibration analysis 1/2/9,13Doublet-sheet method 11/9/30Downwash Failure

calculation 11/5/32-3: 11/8/8-9,11,17 models IV/8/5: IV/9/7distribution 11/5/13,34: 11/6/15 power control3 IV/4/8mean 11/8/41 structural 111/1/1: 111/5/2points, choice of 111/3/24-6: 11/4/14-19 Fatigue IV/10/3-4: V/3/29,33variation 11/8/13-14 Feedback

Drag parachutes 111/7/37 effect on flutter 111/4/12Duhanel integrals 11/6/4,14: 111/4/32,33 force IV/4/!1,13Duncan functions 1/2/5: 111/4/20 structural IV/4/5Dynamic amplification factors 1/3/15-21 Filtering 1/4/35-40: 111/8/4,26: IV/10/17-19Dynamic balance V/3/9-14,20-28 Fin and rudderDynamic flexibility matrices 1/3/29 derivatives 11/11/60-66Dynamical flutter V/3/24: V/4/9,11,20

equations I/INTRO!1-5,12-14 Finite-difference equations 1/1/15,19,20systems 1/6/3-38 Finite-element method I/7/17: 111/2/45:variables I/INTRO/i-S I11/7S/6

FlapsEddy shedding 11/5/8: 111/10/21: V/5/2,22-3 buzz V/5/28-32,36-9,43,50-52Eddy-current damping IV/5/24-5,27 hinge moments 11/1 1/34Edge constraint 111/7/21-2: 111/7S/22,37,39,51 Flat spot 1/6/1-2,20-21,39,45-9Eigenvalue problems 1/2/11: 1/3/23: 111/4S/6-7, Flexibility

11-28,35: 111/6/17-19,26-9: 111/7/9-10 controls 111/3/2-3,4,8,12-13,19Elastic axis 111/6/10,17: IV/1/1: V/3/10-12,20 effect on analysis 111/2/28Elementary system IV/3/ 1,4-5,18-!9 function 111/1/5Elevator flutter 111/5/5: V/3/24-5 helicopter blades 111/ 10/12Empirical methods 111/2/50 influence coefficients IV/1/3-4Energy propellers 111/9/16-18

active 1/3/29 representation of 111/1/4dissipation 111/8/7: IV/3/14-16,19,28-30 vehicles 111/8/24formulations 1/7/8 wings 111/9/19-21kinetic 1/2/2-4,7,8: 111/8/5,6,8-9,16-17: Flexural axis 1/1/4: V/2/21,23: V/6/12,18,

IV/3/5-6,7 19,23-7,40,43potential 111/8/5,6 Flexural centre V/6/75reactive 1/3/29-31 Flight tests 111/1/15-17,24-5: 111/2/53-4:

Energy supplied method 1/4/17-18 III/Chapter 5: IV/Chapter 10Equations, conditioning of 11/1/1 2,14: Fluids, motion in tanks I/Chapter 8

111/4/13-14,20 Flu tterEquations of motion I/INTRO/ 1-5,12-14 aileron V/3/17,24: V/4/8-10,12,13-14"Equivalent profile" technique 11/10/8,12,13 approximations V/Chapter 6"Equivalent" wing V/6/72-5 boundariesErrors, random 11/1//19: 111/4/21-2 model tests IV/6/1&19Eulerian equations 111/4S/9 panels 111/7/4,5: I11I/7S/13,20-53Excitation 1/3/7,27-35: I/Chapter 4 whirl flutter 111/9/10,11: 111/10/11,12

harmonic 111/4/27-9: IV/3/4-5 calculationsin flight tests !11/I/15-16: IV/10/14-21 approximate 111/6/21: V/Chapter 6in wind tunnel tests IV/5/13,20-32,42-4: automatic processes III/Chapter 4S

IV/7/25; IV/8/2-3 in practice 11/Chapter 4points of IV/3/21,29-30 light aircraft 111/1/25

Exciters 1/4/15-16,81,86: IV/3/3,29-30 value of V/3/4,5see also Excitation, Force generators

5

cause. I/INTRO/26-30: V/3/6, 17-21: displacement IV/ 3/24-7V/3/21-31I measurement IV/5/53

classical V12/17: V/3/12,14 naturalcoefficients V/6/ II choice of IV/3/27control surfaces 111/1/7: 111/'4/22-3: definition 1/3/19-20: 111/8/7

111/5/8-13,16: V/Chapter 3: V/6/28-54 determination 1/3/33coupled V/5/53,54: V/6/28-55 pseudo - 1/4/24criteria ratio V/3/15-17,18-21

approximate V/6/9,10,27,36,38,54 reduced, effect on deliiratives VI/TGcontrol surfaces V/3/4-5 requirements V/3/8-9panels 111/7S/54-5 Frequency parameter

diagn.,sis and cure 111/Chapter 5: 111/ 10/ 18-19: control surfaces V/3/7-3V/5/53-4 definition I/INTRO/IlI

elevator 111/5/5: V/3/24-5 history 11/ 1/3-4equations 11/5/9-1 1: 111/4/1,4-9,12-18: liquids 1/8/39-67

111/4S/4: V/6/6,8 Frequency sweep IV/3/7: IV/l0/7,16fin and rudder 111/5/7-8: V/3/24-5: V/4/9,1 1,20 Friction, solid 1/INTRO/9,44-5: 1/4/19,40,51-3:fundamental V/2/28-31,35 1/6/2,22: 111/1/7,9: IV/3,21-3,30: V/1/9general description 1/INTRO/I 9-20,23-38 Froude number 1/8/70helicopter blades I1I/Chapter 10 Fuel sloshing 1/6/2: 1/Chapter 8: 111/1/8:historical review IV/ 10/2-3 IV/6/7: V/-2/22largc amplitude 111/7/10 Fuel tanks see Tanksmain surfaces 1111/5/3-8,16: V/6/11-28,58-60overtone V/2/28-32,35,38 Galerkin methodpanels lu/Chapter 7:111I/Chapter 7S: '11/5/2 dynamic stability 111/6/23,24,32parameters 111/4/23-5 panel flutter 111/ 7/4-8,12-21,29,30:prediction 1/INTRO/36-8: 11I/Chapter 5: 111/ 7S/4-7, 14-15,20-25,39,42-4,47,49-53

111/10/I18-19: V/3/32-3 static aeroelasticity 111/2/34-5propeller-rotor 11I/Chapter 9 "Galloping" V/5/23shells lII/7S/41-7 Gauges see dial gau~ges, strain gaugessingle-degree-of-freedom V/Chapter 5 Gaussian integration 11/3/16-18,33stalled V/5/23-6 Gaussian points IV/l1/8stalling 1/lNTRO/3ý': H1/9/51-3: 111/10/13-19: Gauss-Seidel process 1/3/34

IV/6/7: V/5/2,1 1-IS "Geared surface" method 1/5/35-41: V/4/3tabs 111/5/13-16: V/3/25-3 1: V/6,/47-54 Generalised coordinatestailplanes 111/1/7,2?: 111/4/20,22-3: in calculations 111/4/1-21,9: 111/4S/4

111/5/5-7: V14/ 15-21 in prediction 111/1/6,14,17,18tests HIM/516: IV/Chapter 6: IV/Chapter 8: mass and stiffness 11/1/24: 111/'8/7:

IV/Chapter 10 IV/3/ 15,23-30T-tail V/3/24: V/4/19-20 panel flutter 111/7/1.2types of 1/INTRO/23-6:. 111/5/3: V/3/21-31I Gravitational effects IV/6/7wakc-induced 111/ 10/ 19-20 Green's theorem 11/2/11-13: 11/4/69: 11/5!30:wings 111/5/4-5: 111/9/19-21: V/Chapter 2 11/6/8see alse binary, body-freedom, ternary, Ground resonarice tests I/Chapter 4:111I/1/3,

whirl flutter 8,9,21-4: 111/5/5-7,12,13: IV/Chapter 2:Flutter engine /IANIPO/26,28 IV/4/15: P1/10/12flutter simulators l/1NTR(O 17,31 GustsForce generators I'v/Z'4-9, 12,14,17-1 8 early work 11/ 1/4,8-9Forced oscillation techniques IV/l10/5- 16 response 11/6/47-53: IV/I0/3-4

"Forcing through a spring" method IV/S/20-25 sharp-edged 111/4/29-31Free bodiesthermoelasticity 1/7,110,11 pitching (wing flutter) V/2/28-38Free play V/3/33 control surface V/6/36Freedom, degrees of 1/4/6 Gyros 111/8/1,2,26,27

several 1/6/37-8: IIl/Chapter 6 Gyroscopic forces 111/9/4-5single 1/6/3-7,28-37: IV/:i/: IV/l0/8-9:

V/Chapter 5: V/6/55 Half-span technique IV/5/7,42Freedoms Hanging scale IV//I/1S, 17

choice of l/INTRO/3 1-2 Hard 3wscillator characteristics V/5/S Ilinked IV/5/39,40 Harmonic balance method 111/7S/47.51

Free-free system IV/5/28,29 Harmonic excitation see ExcitationFreon tunnels IV/6/24-S Heat conduction equation (Fourier) 1/7/1Frequency Heating, aerodynamic see Kinetic heating

analysis curve 1/4/36-40 Height effects see Altitude effectsangular 1/4/1 Helicopter blade flutter 1Ill/Ch~apter 10coincidence Vj3j 15-l7 see alto Rotors

6

Helmholtz moment ofequation 11/7/I control surfaces V/3/12,14,IX-23,27vorticiy theorem 11/8/4.12 determination 1/4/64-6,72

Hermifizn matrices 111/4S/11,24: 111/6/24 fuselage V/2j41-4Hessenherg matrix 111/4S/27 rolling V/2/38Hinge moment spars IV/7/16

derivatives Ii/10,34,47-8: I1/I 1/7,33-60 tab V/3/27effect on buzz V/5/44-50,54 parameters 111/4/24effect on impedance 1/5/19-22 product ofprediction of 111/3/17: V/5/44 control surfaces V/3/13,14

Hinge position, effect on buzz V/5/50,5I tab V/3/27Hinge stiffness, effect on buzz V/5/42,43,46 rotatory 1/2/9,14Hooke's Law 1/7/3,22 tab linkage 111/5/13-14,15Horn balance V/3/14 "Inexorable forcing" see Rigid drivesHsu's method 11/3/34-7 Inflow angle 111/9/12-13:!11/10/15,20Hyperbolic radi-b i!/9/31-2 Influence coefficient method I/INTRO/5,6:Hypersonic flow 1/2/6-14: i1/1/20: 111/1/6: 111/4/5

indicial response 11/o/46.53 Influence coefficientsoscillations 11/9/24-8 accuracy 111/4/8

Hysteresis dynamic stability 111/6/4-17,24damping high temperature structures 111/1/23

curves 1/3/4-j,9-10,12 measurement IV/Chapter Imeasurement IV/5/1 1,22 panel flutter 111/7S/5,41

magretic IV/5/28 static aeroelastic phenomena 111/2/26-51:stability boundary Vj5/30 111/3/11,14-15structural non-linearity &/6/21-3,39, three-dimensional supersonic theory

49-51, IV/I/10 11/5/11,26-7Influence points IV/1/7-8

Impedance Instabilitycomplex 1/3/11 conditions for V/5/3-4experimental determination 1/5/29-33 prediction of IlliChapter Imanual controls I/5/6-8 regions 112/27matchirg V/4/5 Instrumentationmodels IV!8/I I flight flutter tests III/5/1,12,16: IV/I0/21-5powered controls 1/5/&33: 111/516: ground resonance tests IV/2/10-14

IV/Chapter 4 load application IV/! / 14-27testing 1/4/18-20: 111/5/6 measurement of deformation 111/8/1-2:transfer 1/4/26-7 IV/1/14-27variation with frequency IV/4/9 measurement of derivatives IV/5/47-53

Impulsive loading I/INTRO/39-40 model vibration tests IV/7/23-6Incidence effects rocket, sled and free-falling tests IV/9/6-7

buzz V/5/42.43,48 Integral equationpure pitching oscillations V/5/16-20 analytical solution 11/3/10-16,43-8stalling flutter V/5/I 1-12,'14 method 11/2/23-6: 111/1/4-5: 111/7/9-10:wing flutter V/2/16-17 III/7S/6

Incompressible flow theory 11/2/10-20 numerical solution UI/3/27-40: 11/4/11-36Indicial three-dimensional sonic M/4/3-1 1

admittance I/ANTRO/39: 111/4/33 three-dimensional subsonic 11/3/3-10aerodynamics II/Chapter 6 three-dimensional supersonic 11, 5/11-55functions 11/6/4-46 Integrationloading II/6/6-9, 2,15,19-30,33-8,44-7 chordwise 11/ 3/ 2 7-97 11/5/43-6method. I/INTRO/I I constants V/6/58-71response II/i/5: 11/6/2,6,14,15,30,33,38, method IV/5/1 7.18

50,53-4 numerical 11(4/19-24Inertia spanwise 11/3/29-33: 11/5/46-9

axis V/2/23-5: V/5/14 Interactioncoefficients 111/4/13,22 aerodynamic and structural Ill/I/I: 111/8/2compensation 1/4/79-83 autopilot and structuire 111/Chapter 8coupling III/1/3,9 shock-wave boundary-layer V/5/2,8,40-41distribution II1/1/3 Interferenceeffect on wing flutter V/2/23-40 ierodynamic 11/11/2forces I/INTRO/I: 111/2/20,29: 111/3/21,4 wind tunnel II/10/1,10,40-41measurement of IV/Chapter 3 wing-tip tanks il/ 11/64

Interpolatio.i functions 11/3/18-19

7Iteration methxods Len's lea 1/4/76

automnatic procsss 111148/13-19 Levers, metamning IV/l/23-5,27dynamic stability 111/6/2,3-20,2&-9 Liapunov method 111/7S/6,1 7.20nan-inear problems 1/6/25-8 Lift-curve slopepanel flutter 111/7/9-10 effect on flutter V/5/23-6static aeroelasticity 111/2/3"- tail V/I/5

wing V/115Jacks lift functions 11/5/34-40,49-50,60circuit diagram IV/4/l4 Lifting-ine theory WO/O2: 11/3/1: 11/6/21:equations of motion IV/4/I8-19 II/I1/ 19: 111/4S/ 10impedance IV/Chapter 4Litn-ufcmehd

loadapplcatin IV1/14automatic processes 111/4S/8-1Ioperation IV/4/2-4 matrix fomin 111/4/5-6stalling 111!4/24 oscillating fiiite wings 9-1l/20-22stiffness 111/5/Ilifigsurc terJoukowski profile 111813,18-20,23,29,30,35,38 coprsnwthexeorimn 1101,5Jump phenomenon 1/6/36-7: 1/8/Il pnwihxpriet9,43/9,5

derivatives 11/8/37Kelvin circulation theorem 11/8/4the-insoaKelvin model 1/71,4.5 'incompressible 11/6/27Kernel function method sonic 11/4/1,11-36

comparison of theory and experiment subsonic 11/3/111/10/19,33,36 two-dimensional subsonic 11/6/16

static aeroelasticity 1/23,78Limit cyclethickness effects 1118/3 panel flutter 111/73/47,51,52,55thre/duriesiona supesoni theory single-degree-of-freedom flutter

11/531,3-4,042,1-5V/5/5,30-35,4(,50Kinetic heating Linear differential equatior' Hl//I1-12,131ctfect on divergence and reversal V/ I/10 Linear superpervidon 1I1...

general effects 1/INTRO/41 Linear system.; lI/l,'23non-linearity 1/6/3 Uinearised eEqation 1111 0/10simulation of IV/6/25-6 Lineauised theoryKirchhoff's for 'mula 11/6/38 compar~son with expecrimznt IIlChapter 10Kfissner effect 111/4/31,32,34 dampirg mo~ent coeffitcier', 11/9/18Kutta condition 11/219-10: 11/6/2,9,16: derivatr.- V/6/ --811/8/2,4,7,39,42 phy- erepirebA.-n 1!j2/18-20

stabia.. ' oundaries 11/9/14Lagrange stotus 11/i/18-19equations three-dimensic-al 11/4/1,4-1 1: 11/5/1aircraft flutter 111/4/1,9,27 two-dimensional lI/Chapter2conservative structure 114/3 Linea-ity, assumption of l/INTRO/2,3, 10:

dissipative structure 1/4/61/1:1//71128:I32geneal AINTO/29: 11/15,6Liquid ctffect on flutter I11/7S/451panel flutter 111/7/7 liquid propellant dynamics I/Chapter 8powered controls V /4/2-8 liquid sur-face motion 1/8/21,27-8,61,68-9

propeller flutter 111/9/4 Lissajous figures 1/4/80: IV/7/25: 1V/8/3vehicle with autopilot 111/8/6,7,1 5-7 Load application IV/ I/I1-14,26-7interpolation formula 1/ 1/ 19 Load c.;'1s IV,'1/ 14multiplier technique 1/2/5 Loading

Laplace acoustic 1/2/ISequation 11/2/10,13: 11/4/80,81,86: aerodynamic 111/2/4-511/6/30,32: 11/7/1,13,20,48:"11/8/4,7: dynamic 1/2/14

1119/28,33 initial 11/6/5,7law 1/4/76 pulse 11/6/12,14,27,30,33operator V/4/4 see also Indicial loadingtransform 1/3/6: 11/2/30,31,40 Loads see Aerodynamic forcestransformation method 111/7/8: 111/7S/6 Local linearisation method 11/9/2,20-23,31,35,41

lateral control, methods of V/ 1/7-9 LogarithmicLateral-antisymmetric motion I/INTRO/5 circuit IV/S/ 16-17Launch acceleration 1/8/65 decrement 111/6/30,31: 111/7/I 2,32:Least-squares method 111/2/35-6,47-8: IV/3/ 19-20: IV/5/ 10,15-1 7IV/ 1/10 increment 111/7/25-6

spiral IV/5/I5

8

LIongitudinal-symmetric motion I/INTRO/5 Minors see OpticalLorentz coordinates 1l/2/6-8 Mkies metnod l1114S/13-14.20.21 .22Lumped parameter method 11/1/23-4 Mise profles H/8/19,21,33,37,38

Misilks II1/8/14-28Mach number critical ll/10/.2-14 Modal methods 111/2/32-3.38: /8/4,S-8,28Mach number effects on see aso Rayletgh-Ritz method

buzz V/S/29-36,39 Model testscontrol surface flutter V/3/7-9.-1: comparsm with themory 111//24-6

V/6/37,41 propeller flutter 111/9/1,10-11,13,21-2derivatives I/INTRO/I i: 11/10/28,32: representation of ful-cas I/INTRO/32-5,

11/ 11/30-32: V/6/1 Q-22,35: VI/TG/I 1-138 424: 111/113,17-21divergence 111/2/3 uses of IINTRO/42: IV/7/2-3dynamic pressure V/I/2,.1 Modelsmust response 11/6/49,51 buzz V/5/54lateral contr•i V/1/7,8 constnction IV/Campter 7models IV/6/9-17: IV!71.3-14: WI87-11 control surfaces VW3/5,6pLnel flutter 111/7/10,11: 1!1/7S/18,24-33,40,41 failure IV/8/5: IV/9/7powered controls VW4/8,12-13 fallin-body IV/6/21: IV/Chapter 9root bending moment V/1/3,4 flexible IV/5145: V2/8,14

soic theory 11/4/9-11 flutter 111/5/8: IV/Chapter 7: IV/Chaprer 8:stalling flutter V//115 VI/25,,8,9wing flutter VW2/3-S,9,16,20,25-7: full-scale IV/9/10

V/6/22-8 high-speed IV/7120-21wing stiffness requirements V/2/19-21 history of types IV1/7/3-12

Magnetic analysi method 1/4/35-40 instabilities IV/8/4-SMagnetic tape IV/5/13,14,17 layouts IV/9/7-10Manoeuvrablity, rolling V11/6-8 light-weight IVT7/5,6-7,19,25Marperre's equation i1i17S/49 low-aspect-ratio IV/7/15M•.s low-speed IV/7/16-19

added to small models 1/4/74-5,85-6 materials IV/7/16-21and spring systems 1/4/51-60 mathematical 1/3/3-1S: 111/2/12,13-24:distribution 1/4/17: 111/6;4: V2/23-7 111/3/5-1I: 111/4/2:111/8/3,4: 11/9/11,17equivalent IV/3/24 mechanical 1/3/3-1S: 1/8/48,5 I,55,56generalised 1/4/16,61-2,82-3,86 rigidity IV/7/15,16ratio V/3/18,20,21,22-3 rocket-carried /IMNTRO/35: IV/6/23:

Massbalancinj IV/Chapter 9: V/1/7aileron IV/9/12-13 similarity IV/Chapter 6: IV/7/12-13blades 111/10/12 slec-carried IV/Chapter 9control surfaces and tabs 111/5/4,8-15: sting-mounted IV/5/31,39

V/3i1,4,9.14,17,21,28,31-3: V/6/53-5 support IV/6/6: IV/7/22-3,24failure of support 111/5/2 small, ground testing 1/4/73-87

Spowered controls V/4/1,6-15 thermoelastic IV/7/22pre-flight cakulations 111/4/23 transonic IV/7/10,11,12,19: IV/8/10-11test apparatus IV/5/34,37-9 Modes

Mathieu functions i1I/118: !1/2/20-23,26: adjoint 111/6/2411/7/26,27 all-moving tailplane V/4/15-21

Matrix methods branch 111/4/20-21admittance concept IV12/20-21 choice ofautomatic processes 111/4S/ 11-28 deformation 1/1/19damping effect on resonance 1/3/1-2,21-37 propeller-rotor 111/9/21dynamic stability 111/6/7-12,17-21 control surfaces V/3/23-5flutter problems i11/4/3-11,13-14:111/6/22-9 damping effects 1/3/1,23-4,27general application !1/1/5-6,9-12 definitions 11/10/4generalised forces 11/4/31-6 determination !11/4S/3-6,29-35generalised masses IV/3/23-6 excitation 1/3/27-35panel flutter 111/7/10,12: 111/7S/5-6,41 flexural, of missile 111/8/14-28static aeroelastic phenomena 111/2/26-32, natural 1/3/23-4,31,35:1/4/4,24

41-3: 111/3/11-14 normalstructural influence coefficients 1/2/6-13: calculation III/1/ 13,22-3: 111/4/9-11,20

IV/ 1/3-7, 10-1I: IV/4/2-1 4,16-18,23-7 Ill/Chapter 6Maxwell model 1/3/1,5-6,9-10,13,17,22:1/7/4 definition 11/1/24Mechanical instability 111/9/17 errors 111/4/21-2: 111/5/I 1-12Membrane excitation IV/2/3

flutter 111/7/36-7,38: 111/7S/53 properties IV!2/3tension 111/7/12,13,16,27: l11/7S/16,17,39

1. +

9

power contros V/4/9-14 Oscilationspinasuibed i16/21.22 bending V/S/IO-1,26representatiom of i1W1/3 control surface V/5/26-54rigid-body IU/7j22-5,45-8,73: III/l/12-18 decaying IV/3/5,18-19,23: IVI5/10-14:separation of !1/8/13 IV/II/16-21

e effects 1/4/51-62,66-71 flappr-g 11/10/28twist V/6/14 flutter IV/5118-20wing V/Chapter 2 forced V/5141,46

Moduluis harmonic II/2/8-9: I1I/4S/7,9: 111/6/1:complex 1/3/8 V/5/5spring !1/3/7 modes, definitions 11/10/4

Monoplanes. flutter IINTRO/46: i111/4: -POGO" !8/19,65V/I/li pure pitching V/5/6-10,15-21

Muller's method 111/4/18 quasi-periodic V/5/32,33Multhopp's method 11/3/1.2,30-33 relaxation 1/6/33-4

self-excited V/S/6,22-6,41-2,46-7,S0Nacelles short-period V/6/44

damping 111/9/9,10,11 sinusoidal IV/5/4: V/5/16,18,28,33,34effect on derivatives I/I 11/63-6 snall 11/7165-8flexible 111/9/3-4 types of 1/6/35underslung 111/3/2 Oscillator, electronic IV/2/l0: IV/5126see also External stores Oscilloscopes IV/5/14-16,21,26,52,53: IV/8/3

Neumann's problem 11/2/11 Ovary ellipsoid 11/7/46Newtonian theory 11/9/24,25,27-8,38Nodal lines, points III1//18,19: 11/4/14: Panel flutter I/INTRO/25: 11/9/42,49-51:

V/2/3,29,37: V/3/14 11111/6- 111/4/25: I11/Chapter 7: 1I1/Chapter 7SNoise loading I/INTRO/41 Perturbation methods 1/6/7-16Non-dimendonal parameters Phase-aigle swep IV/3/10-11

V/5/4-6,27-8,39,43-6,48 Phase criterion 1/4/15Non-linearities Phase-plane method 1/6/3-7

aerodynamic Phase portraits 1/6/3-7,31,32importance of /IINTRO/12 Phase resonance, excitation at IV/5/26-31incidence and Mach number effects Phase-shifting network IV/I515,21,49,53

11/10/12-14 Phase stabilisation 111/8/27types of 11/9/I: 111/1/6-7 Pick-ups IV/2/10: IV/Chapter 5: I/7/25

helicopter blades 111/10/13 Piston theorypanel flutter 111/7/10,40 automatic processes 111/4S/8powered controls 111/5/1,13: V/4/5 general 11/1/]1517: 111/1114: 111/4/7-9single-degree-of-freedom V/I5/13,4,32-5,51 hypersonic I!/t,/46: 11/9/18-19,24-5,40structural 1/4/18&20: 1/5/8: I/Chapter 6: panel flutter III/Chapter 7: I1/Chapter 75

Ii/l/7-9 sonic 11/2/41Non-stationary theory see Unsteady theory supersonic 11/2/18-19: !I/I0/16,43: 111/2/49Normal coordinates 11/1/9-13: i1I/1/9,10-15: Pitching axis V/5/18,20

!11/4/9-11: 111/6122-5 Pitching momentNose shapes (controls) 111/5/13-14 aeroelastic effects 111/2/17,22,24Notation derivatives I/l 10/24,25-33,45,46: H/ 11/7

control surface V/5/27 Planformsderivatives 11/2/46: VI/TG/6-7 effect on flutter V/2/5-15,20flutter equations V/6/6 optimum VW1/7,9in different countries 11/2/46 Plastic behaviour 117/6

Nozzle, rotating 111/8/14,17-18 Plate theory 111/2/45-6: !11/7S/49Nusselt number IV/6/26 PlatesNyquist diagram 111/7/10: 111/8/13,26 ablating 1/7/37-8

thermoelasticity 1/7/12,15-16,21-7One-degree-of-freedom systems vibration and stiffness 1/7/30-38

see Single-degree-of-freedom systems see aLso Panel flutterOperational flexibility 1/3/7 Plotter, automatic III/4S/29Operational methods 11/2/30-31 Plunging wing ll/Chapter 6Operational modulus 1/3/7-8 "POGO" oscillation 1/8/19,65Optical deflectometer IV/1/I5,17: IV/7/23 Possio's equation Il/10/10Optical lever IV/1/23-4,27 Potential energy, minimum 1/2/3Optical methods, vibration testing -,'4/76 Potential flow theory

general 11/1/9-10: 11/5/1in flutter prediction V/5/36-40,43in panel flutter 111/7/10: III/7S/45,46

I:

10

Potential functions I/Cbapter 8 RepresentationPotentiometeus IV/7/25 of aerodynamic forces /INTRO/9-12Power plant, representation of 111/9/34 of controls 1/INTRO/SPowered controls of damping 1/INTRO/S-9

buz prevention 111/5/II of structure 1INTRO/5-9: 1/2/1control rotation frequency V/6/32 of structural deformation /Chapter Iflutter V/Chapter 4 of suspenion, in ground tests 1/4/51-62impedance mearement H1/l/24: 1V/Chapter 4 •-ni-rigid 1/INTRO/6n -linearity 116/2: H11/1/7,8 Resonancespecial problems 1INTRO/4S: 111/5/6 ampStude 1/4/9

Prandd number 1V/6/26 cures 1/4/8-10,19-20: IV/3/7-9,10Premne effect of damping 1/Chapter 3

difference, formulae 11/2/31-2 many degrees of freedom 1/3/21-37differential (panels) I1/TS/49,51,52 modes 1/INTRO/6,7:1/4/51-60distribution, memutements 11/10/23 phase 1/3/20,23,32-3:1/4/9,19-20,80-1dynamic position of .V/10/10-14

and stiffnen ratio IV/8/10,12 1/3/31-5at control reversal 111/3/2,74,12,17-18 1/3/33-5at diergence 111/2124,51-2 " 1/3/15-21compzesbility and sep effects V/1/2-3 testing in flight 1/INrRO/35panel fhutter I11/7/15-17,20: H1/7S/18, Resonance tests see Ground resonance tests

3045 Res-melading 11/9/24,25 amplitude 1/4/19perturbation 11/5/6-7 calculations, in practice 11/Chapter 4plotting IV/5/43.44-6 carves IV/5/23

Prsmu•e potential procede 11/5/31-3 - dynamic 111/4/26-35Prolate qiheroid 11/7146 forced 1/3/35-7Propellant dymis /Cbspter 8 indicial !1/6/2,6,14,15,30,33,38,50Pple gutte In/Ctc r 9 jack IV4 IlProperevectors I/4/5 measurement IV/8!2: IV/10/21-3

Prototype flutter investigation I/I/14-15,17 prediction 11/Chapter 1Palmation see Frequency, angular quadrature !V/2/19,20

to atmospheric turbulence m11/4/33-5

Quki-static to single impulse 111/4/29-33approximation 111/7/6,7,29 Restraint, rariable 1/5/33,4definition I/INTRO/5 Reversal, control I/INTRO/19,22-3: 1H1//2:derivatives l/INTRO/10,38-9: 111/1/15 111/3/2,6-7,18: V/W/1-1Oeffects 11/2/2,3,17,23: Reverse flow theory 11/5/15: 11/6/46:stiffness 1/3/24 11/8/37: 111/2/49theoy 11/6/1: 111/7S/10,49 Reynolds number effects 1/INTRO/I l:

IV/6/6-7: IV/8/i 2: V/5/15,20,21,25"Raft mounting IV/5/41,42 Riemann's method 11/2/28-30Raked wing H/10/43,44 Rigid-body freedoms Ii!/i/12,15Raimberg)qood equation 1/7/6 Rigid drives IV/5/35-42Ranges, aroballistic IV/6/21 Rigidity see StiffnessRayleigh-Ritz method Ring analysis 1/7/18-19

flutter equations 11/5/9-11 Ritz-averaging method 1/6/16general 112/3-5 Rivet slip 1/6/1,2: 111/1/7in automatic processes 111/4S/4 Rocket impulse units 1/4/29-30: IV/10/23-5panel flutter 111/7/4: 111/7S/5,25 see also-Excitationstatic aeroelastic phenomena 111/2434 Rocket model. IV/6/20-21,23: IV/Chapter 9

Rayleigh's principle I/2/3: 1/4/11-12: Rocket tests111/6119,26 buzz V/5/43

Reaction, measurement of IV/5/32-46 Rockets, liquid dynamics 1/8/15-19,62,65-6Relas effects 11/9/28 RollingReciprccity relations (Maxwelt's) 11/6/46-7: manoeuvrability V11/6-8

111/2/25-6: IVi1/4-5,6,7,10 moment 111/2/17:111/3/8,13Record analysis IV19/10.13 Root, wingRecording see Data recording fixed V/2/33,37Rectifier IV/5/50 freedom V/2/40-44Reference axes 1/l/1-3 lift distribution 11/7/53-7Relaxation modulus 1/7/5 Rotor flutter III/Chapter 9

Rotors. non-rigid 111/9/13-18Rudder see Fin and rudder

S. ... • -

II

Sstly faheu, Butr V/6/27 static aeroelastic phenomena 111/2/49Safety anwas WV/IN12 thickness effects 11/9/33-8Subt Vma t tasion 1/1/5: IV/7/16 Slender4wif theo• ySmd medwd vilati. hatift 1/4/76 comprim with experiment 11/10/30,43Scale factors V1612 general 1!i/4/6Sdmitt "W celcud IV/S/30,49 indiciai aerodynanics 11/6/6.7,32-3.36Seccdas effeck sbactufral 1/2/14 thicnes effects 11/9/33-8Second-order theorms 119/34-8 Slotted tunnels 11!f40041Self-excitation IV5/2"7-31,42-4 "Slow oscillation" assumption 111/7/17Sem oema 1/41/20: IV/3/l1-14,27 Smallperturbation method .I/I I11/_5 15:Sensors 1/5141-6 i18/3Separation Snaki i/INTRO/20,44

effect on unsteady forces 11/9/38 Sommerfeld radiation 11/2/10,21localised 1m/i1/7 Sonic flowmodels IV/6/7 two-imineionaj theory 11/2/33-41panels 11/7/23 thieditenionl theory 11/Chapter 4shock-nndaced II1/5/3,10,1i: V/5/21, Spats, model IV/7/16,17-18,20-21

AX31,42,48,53 Splitter-plate V/5/5 1,52*--ftr wiip W7/61-74 Spollersstalling flutter 11/9/51-3: V/S/14-15 V!11?: V/5/41,42,52-3

Seao controls 111/4/I1-12: H11/5/13,15,16: Spray, propellants 1/8/21-2U11/Chapter 8 Spring

Shaken 1/331-6: IV/2/4-11,14-18: J1P7/25 beatings IV/5/8,37Shapes, natural constants 111/2/20

definition 1/4/4 constraint IV/51/0,20.25.34determinaio of 1/4/25,85-6 rate (jaks) IV/4/6, 7.19excitation of 1/4/14-16 tak 1/6/2,39: 111//7,8: 111/5/1,14-16:blades 1/4/85 V/6/53suspenson effects 1/4/60-61 Spring support technique V/2140

Sheet-ad-stinWer strcutues, thermoelasticity Springs1/7/17 calibrated IV/I/22

Sbells cubic hardening 1/6/41-3conical 11/7/33: 111/7S/47,55 cubic softeaing 1/6/43-4copper i][/7S/43 elastic 1/3/3-15cylindrical 111/7/23-33: !!1/757-8,14,15, Stablier (of oscillations) IV/5/29,30,31

41-7,54,55 Stabilitysteel 111/7S/43 analysis 111/8/ 13thickness requirements 11117/23,26,29, boundaries

30,32,41 helicopter blades 111/10/17vibration analysis 1/2115 panels HI/7/35,38-41: 111/7S/15,19,20,

Shock-wave boundary4-yer interaction 24-7,33,39,52V/S/2,8,40-41 propeller 111/9/8-9

Shock waves supersonic thin wing 11/9/14effect on huzz V/5/40.43 calculations 111/6/29-32effect on panel flutter 1,1/7/23 conditions 111/8/25-8

Short-period oscillation 01/1/12 definitions l•/TO/I14-17Similarity determinant 1/5/3741

parameters IV/6/4-6,25-6: IV/7/12-13: Stagnation point, choice of 11/8/38421"€18/7 Stagnation presmre and temperature IV/6/12-17

relations 11/i118 Stalling flutter see Flutterrequirements IV/Chapter 6: IV/7/12-13: Static aeroelastic phenomena III/Chapter 2:

IV/8/? Ill/Chapter 3: V/Chapter ISimulators, flutter 1i1I/13,15 Static balance V/3/1 1-12,17,18-20,22-3,28Sine curves IV13/11-14,21 Static margin V/6/47Singularity Steady-state solution 1/4/9

logarithmic 11/3/33-4:11/4/24-31 Steady-state stresses 111/4/30vortex 11/7/61 Step-by-step methods, non-linear problems

Sinusoidal 1/6/23•forcing IV/4/3: IV/8/3: IV/10/5 Stick jerking 1/INTRO/35generateis IV/5/51-2 Stieltjes integral 11/9/35oscillations IV/5/4: V/S/16,18,28,33,34 Stiffness

"Skeleton line" technique 11/10/8 aerodynamic 111/1/17Skin thickness V/2/22 all-moving tailplanes V/4/1 5-21Sled-carried models IV/6/20-21: IV/Chapter 9 beams 1/7/30-38Slender-body theory bending 111/5/6:111/8/6

general 11/1119: 11/Chapter 7: 111/1/14:111/4/6 compensation 1/4176-83

12

Target towftn 111/7/37 Unsteady theory 11/Chapter 8: M1/6/30Telemetry IV/10/26 U-shaed interconnections V/4120-1Temperature distribution in structure 1/7/1Ternary flutter IIINTRO/24: 1114/16: Valves (poweredcontrols) I/5/1 i-17,23-7:

V/4/19: V/6/7,42-54 IV/4/2-7,15-18Test functions 111/141446 Vane, auxiliary osmilafti IY/lO/ISTests Variational method i/2/2-6,12,13

* equipmnent IV /l/ 11-26: IV/2/4-14: Vector response plot WV/l(Vl2-13IV/4/8-l3: IV/5/6,7 "Vectorial anaysW techniqu P1/1015,7-14

lull-cale 11INTRO/3S-6.42 Velocity inmsanament, models IV,'9/34,-*.6npedarice IV/Chapter 4 Velocity potential

techniques IV/2/14-21: IV/ChapterS5 delta wings W14/7"-"tye 1/INTRO/42 expansion WS/5/13-14,5l1-5vibration IV/7/23-6 in half-space 11/5/11-29

a sho Model tests, Ground resonance tests in whole spac W15/30-31Thaeodonen function 11/2/15: 1[/6114;21,22: low-aspect-rottio wings 1114/69-78,98-102

1116/30: VM/G2-4 method 11/IO-015Theory perturbation W17/6,8,10,12,14-16,17-18.61

comparison with experiment iI/Chapter 10- rectangalar wings 11/4/364S11111/22,24.: 111/9114-16: IV/l0/25 wing-body combinations 11/4/78-98

Thermal stremses 1/INTO/41: 1/2/1: 1/7/10-16, Vibration32-4:11114125: V/1/10 arralyis 1/4/31-40

Thermistors IV/5/30 by inverson (magnetic analysis) 1/4/35-40Thermoelasticity 1/Chapter 7 graphical 1/4/32,33-5Thickness effects (aerofoil) spectral 1/4/32-3

11/Chapter 8: 11/Chapter 9: V/2/15-16: beamts 1/7/30-38V/5/9-l0,3 143,48 engine 111/5/2,3

ThUsta, propefler 111/9/11-12 ground testing 1/Chapter 4Thrust orientation 111/811,2,14-28 plates 1/7/30-38Thrust rods IV/2/14,1-0,16 propeller 111/5/2.3Tine parameter 1/4/2 still-ai 111/6/22-5Torque motor 111/8/21 structures I/Chapter 2Torque tube 1/5/27-9 thermally induced 1/7/30-32Tranrsducers I1/1/19: P1/2/12: types of IW15/2-3

P1/9/6: IV/ 10/22-3 wind-iriduced V/5/25Transfer Function Analysers (TFA) P1/4/ 13 'Victoff", flutter test 111/4/33Trartsfer functions 111/1/21:111/6/31-2:111/8/22,26 Vir'tual. Work principle 1/1/15-16,19-20:Transients 1/4/35-40: P1/3/5,16-23: P1/5/13,17,18: 1/7/8-9: 111/2/34

*IV/9/13-14:IV/ 10/17-28 Viscoelastic behaviour 1/7/4-6Transonic effects ViscosityII control siarface flutter V/3/29: V/4/15 air, effect on derivative 11/11/2

wing flutter V/213-4,1 1,15,16,25 propellants 1/8/26-7,72Transonic flow von Mides method see Mises

~ Icomparison of theory with experiment Vortex distribution method 11/2115-1811O/110-14,35-42 Vortex generators 111/5/10: V/5/53

derivatives W1/11/30-32 Vortex lattice theories 11/9/30general 1 1//12-13,17 Vortex position and strength 11/7/62-5,68incorrect data 111/5/9-11 VTOL 111/9/I,12,13,21-2

Trir circuit P1/5/30,49K T-tail Wwgnr-Kappus Torsion-Bending Theory I/1/5

derivatives 11/ 11/60,62 anefnto /1:1//131143,2flutter 11/ 11/60: HI/11/ 16: 111/5/7: Wake

V/3/24: V/4/19-20 finite 11/1/15models P1/7/7,8,13: IVI8/6 functions 11/8/25-34

Tuned systems I1/5/22-4,3 1: IV/ 10/ 17-29,21 line 11/8/5,7,12Turbulence, atmospheric 111/4/33-5: 111/9/22-3: vortices 11/8/11

IV/10/3-4 Wattmeter P1/5/52-3see also Gusts Wave equation II/1/10-I11

Twist, axis of 111/ 1/2 WavesTwisting momnents 111/2/15,20 standing 1/2/2: liH/7S/32,47,55Two-mode analysis 111/7/16,24: 111/7S/39, travelling 11/7/23-5,33-7: 111/7S/1 1,20,32,

45,49,51,52 41,47,55Two-root procedure 111/4S/14-15,21 Wavy walls 11/9/45,49-51,52: 111/7S/1 11-12Tyres, interference from 111/5/12

13a

control circuit V/411,7,I4-lS piston theory 111/4/7derivative IV/S/4,28 three-dimensional theory 11110/~42-3:determination of 1/INTRO/8 Il/Chapter SAstruitioin, wft mi/s1 two-dimensional theory 11/2/28.33: 11/10/14-18deffc an wing Bertter V/2114,17-23,26-7 Support, models 111/1/19:111/2/52: IV/S/7:elastic NV/S/S IV/6/6error in data 111//11-12 Support, structurefin 111//7,8 gound test~s IV/1/8,9: IV/2/14in flutter prevention 1INTRO/36,37 see also Susiensonmeiasrement of 7N/I/I: 1V/4/ 15: IV/7/23 Surface integrals 11/5/43-9non-lineauities 1/6/41I-S I Stuface methods 111/2/30.32,40: 111/3/14Plates 1/7/30-38 Surface theory 111/7/16: 111/7S/23

prpels 1/9/8-9 Suspension (ground testing) 1/4/50-72requmurenurs 11/2154: 1117/16,17: V/3/18 Sweepback effect

salie IV/6/8-17,20,21,22,23: IV/7/13 on approximate formulae V/6/12,24.6,29,32spring 11318-9 on bending oscillations V/S/ 10-11l,15static, definition IV/4/17 onr body-freedom flutter V/2/42Not H11/5/6: IU11/23 on derivatives 11/ 11/27-30torsional 11/1/8: 111/5/6: on dynamic presuire V/I1/2,3IV/8/10-I I on lateral control V/1/7-9

Stlill-&rtabt IV/5/12,22,30,37 on lossof lift V/I/SStrain on negative damping V/5/9-10

components 1/l/7.8,19 on panel flutter 111/7S/20,21,22,39,41energ 1/l/8-10,19: 1/2/24 on. root bending moment V/1/3,4

Strain-BOWg on static aeroelastic phenomena 111/2/2-3,beams IV/ 1/ 19-23: IV/7/25 5-6,16,19pick-ups IV/5/47: I1/8/2,3 on wirng flutter VW2/5-1 5,24,29-31

Stress formunlation 1/7/7-8 swept wingStrip derivatives WI/11/4-7:111I/1/17-1 8: experiments 11/10/24,28,46,50

111/4/4-5: V/6/ 11 two-dimensional treatment 11/1/18Strip theory Swirl 1/8/11-12

general W1//19:11/211: 111/4/4-Sin approximate formulae V/6/ 11 Tabsindicial aerodynamics 1116/27,53 dampers V/3/29panel flutter 111/7/11,13,14: HI/7S/23 fal-safe V/3/29propellers 111/9/ 10 flutter V/Chapter 3: V/6/47-54,66-7 1validity 111/4S/10 Seared 111/5/15,16with three-dimensional effects 11/5/15-18 hinge moment 11/11!/7,33,34

Structural mass-balancing V/3/28deformation I/Chapter 1:111I/Chapter 8 servo 111/5/15,16efficiency IV/6/8-17,20,21 spring 1/6/2,39: 111/1/7,8: 111/5/1,14-16:parmneters 111/4/24 V/3/29: V/6/53

Structural aspects of aeroelasticity Volume 11 types V/3/26Structures Tachometer IV/2h O

associated (SA) 1/4/2-S Tail surfacesdissipative 1/4/2,5-10 derivatives 11/11/60-63non-linear 1/4/18-20: 1/Chapter 6 main surface flutter V/6/1 1-28,58-60orthotropic: 111/7S/9 static aeroelastic phenomena 111/2/30:real (SR) 1/4/2,5-10 111/3/14representation of 111/5/12 Tailplanestypes of 1/2/2 all-moving 111/1/2: 111/5/7: IV/8/6-7:vibration 1/Chapter 2 V/4/15-21

Subsonic flow effect on body-freedom flutter V/2/42comparison with experiment Il/I 10/6-9,19-35S error in flutter calculations 111/4ý122three-dimensional theory 11/Chapter 3 flutter analysis 111/5/5-7two-dimensional theory 11/2/20-27 ground resonance tests 111/1/22

Superposition see also T-tailintegral 11/6/1 Tanksprinciple 11/ 1/6,8 liquid dynamics I/Chapter 8

Supersonic flow tip 11/11/63-6: 111/ 1/18-25: 111/2/4,55comparison with experiment 11/10/43-7 Taper, structural 1/1/9derivatives 11/11/30-32 Taper ratio effectgeneral considerations II/ I/ IS on derivatives 11/11/27-30,40

on flutter V/2/ 13-15: V/6/ 14-18,26,33,34

14

Weber number 1/8/70 WingsWedge profiles arrow-head 1115/14,36-8:11/10/25-8

comparison of theory with experiment comparison of theory with experiment11/10/16,18 1/2/14: Il/Chapter 10

hypersonic flow 11/9/46-9 cropped delta 11/7/24-5,58&61oscillating 11/9/23-7 deformation I/1/i10-18

Weight functions 11/3/19-24 deltaWeighting methods 111/2/33-6 comparison of theory with experimentWeissinger method 111/2/49 1/2/14Whirl flutter III/Chapter 9 indicial aerodynamics 11/6/31-3,41-3,52Wlelandt's method I11/4S/17-19,25: 111/6/19 influence coefficients 1/216Wind tunnel tests slender-wing theory 11/7/29

comparison with theory II/Chapter 10 three-dimensional sonic theory 11/4/74-8derivatives 11/111/27-30: IV/Chapter 5 derivatives fl/I 1/8-32: VIiTG/4-5,1 1-14,high-speed IV/6/9-20 26-41low-speed IV/6/20 flutter V/Chapter 2: V/S/6-26: V/6/10,1 1,media other than air IV/6/24-5 13-28,58-60techniques IV/Chapter 7: IV/Chapter 8 low-aspect-ratio 1/2/6-7: 11/4/69-78,see also Models 98-118:11!11/19-26: 1112/5,6,30,45-6:

Wind tunnels 111/3/14,16blow-down IV/7/6,20: IV/8/4,11 raked 11/10/43,44interference 11/10/1,10,40-41: IV/5/53-4: rectangular

IV/7/13: IV/8/ 11-12 comparison of theory with experimentoperation IV/8/3-4 UI/10/25,37,38,43,50resonance 11/10/10,11 indicial aerodynamics 11/6/30-31,34,43-5

Wind-induced vibrations V/5/25 slender-wing theory 11/7/23-4,29Wing theory Volume H three-dimensional sonic theory 11/4/36-68Wing tips slender 1/2/6:11/7/10-13,17-31,61-74: 11/9/9-20

effect of shape on flutter V/2/9-10 see also Wing theory, Wing-body combinationsWing-body combinations

sonic theory 11/4/78-98slender 11/7/14-16,48-61

15

AUTHOR INDEX

Abbott, F.T. Jr. 111/9/24 Barboni, R. 111/7S/85 Bohon, H.L.. 111/7S/71,73,76,Abramson, H.N. I/Chapter 8: Barling, W.H. 11/1 11/67 77,78,80,89

1/g/28,29,30,31,32,50: Bannby, J.G. IV/7/27: Bolas, H. I/lntro/48111/7S/64 V/2/9.44 Boley, B.A. I/Chapter 7:

Ackeret, J. 11/119: 11/9/20: Baron, M.L. 1/2/17 1/7/38,39,40,41111/7S/10,16,41,49 Barr, G. 111/7S/86,89,90 Bollay, W. IV/7/3,26: V/5/56

Acum, W.E.A. 11/3/2,37,40,41: Barrekette, E.S. 1/7/40 Bolotin, V.V. 111/7/47:11/4/119: 11/5/31,58: Barrett, S. IV/l/28 111/7S/59,62,63,64,65,67,7011/Chapter 10: 11/10/55,57: Basile, B. 1/3/2,37: Bosschaart. A.C.A. V/3/3611/ 11132,67: 111/7S/58,60,61: 1/4/12,20,82 Bratt. J.B. 11/9/1,54,60:IV/5/58 Bateman, H. 11/2/11,42 11/10/6,17,23,28,35,40,52,

Adams 11/6.)124 Bauer, H.F. 1/8/28,29,31 54,56,57,58: 111/10/22:Adams, J. V/5/41,59 Beam, B.H. 11/10/32,47,58: IV/Chapter 5: IV/5/54,55,Adams, M.C. 11/4/69,71,83,100, IV/5/55 56,57: V/5/I18,20,55,56,

120: 11/7/12,74: 11/9/33,57 Beatrix, C. I/Chapter 4(C): 57,6 1Aiken, W.S. Jr. 111/3/20: V/I/Il 1/4/49 Brebner, G.G. 11/ 11/68:Aitken, A.C. II1/4S/13,23,24,36 Belierby, P.J. IV/l0/28 V/6/56Alexander, AJ. 11/10/25,30 Belubekian, M. I1I/7S/84 Bremmer, H. 11/2/45:Alexander, H.R. 1/6/46,54 Benham, P.P. 1/7/39 11/5/56Alfrey, T. 1/7/39 Bennett, R.M. 111/9/7,10,11,13, Brewer, Griffith. 11/Intro/49Alksne, A.Y. 11/9/2,20,54,55 22,24,25 Bridgeman, K.B. 11/10/40Allen, D.1. 11/3/2,41 Benscoter, S.U. 1/2/8,16: Broadbent, E.G. 1/4/49:Allen, H.J. 11/1/19 IV/l1/27 IlI/Chapter 1: HII/Chapter 4:Ambartaumyan, S.A. 111/7S/68, Benun, D. 1/Chapter 5: V/ I/ 12 111/4/36,37: IV/10/8,27:

69,77 Bergh, H. 11/10/6,52: 11/11/8, V/2/14,19,21,45: V/3/23,35:Anderson, M.S. 111/7S/80,83 34,35,48,52,56,66,67,68: V/4/20,21: V/6/25,55,56Anderson , R.A. 1/2/15 111/9/19,25: V/5/57: Brock, J.E. 1/6/25,54Anderson, W.J. 11/9/42,45,59: VI/Tables; and Graphs Broglio, L. 1/7/40: IV! 1/28

111/7S/ 10, 11, 12,44,67,70,73, Berlot, R.R. 1/8/30 Brooke Benjamin, T.74,80,81,86,89 Berman, i.H. 11!2/35,44: 111/7S/1 1,94

Andreopoulos, T.C. 11/10/53: 11/5/57,58: 11/10/53,59: Brooks, G.W. 111/9/25:11/ 11/34,67: IV/8/13: 111/2/57: V13/34: V/5/43, 111/10/22V/3/25,36 58,60: VI/TG/5,8 Brown, A.N. I11/7S/76

Andrew, L.V. 11/9/33,57 Berry, .J.G. 1/2/17: 1/8/18,31 Brown, C.D. IV/7/3,26:Andrews, R.E. 1/6/55 Betts, D.B. 11/ 10/33: 11/11/45 V/5/56IAndronow, A.A. I/b/55 Betz, A. 11,14/72,82,120 Brown, C.E. 11/1/19:Argyris, .J.H. 111/1/6 Bielawa, R.L. 111/10/21 11/7/61,75Arnistead, A.L. 1/8/29,50 Billing, H. 11/8/43 Brown, R.A. 111/75/ 10,74,77Arnold, F.R. 1/6/54 Biot, M.A. 1/3/37,38: 1/7/41: Browne, K.A. 111/9/1,24Arnold, L. 11/1/25: 11/5/15,57: 11/5/15,57: 11/6/49,58: Bruhn, G. 11/9/27,56

IV! 5/57 11/10/20: 111/2/55: Brusilovskii, A. 111/7S/82Arnold, R.N. 1/2/17 V/I/10: V/3/35 Bryan, G.H. 11/1/1,4,5Asher, G.W. 111/7S/76: IV/2/21 Birchall, P.C. 11/3/37,42 Bublik, B.M. 111/75/75Ashley, H. I/lntro/48: 11/ 1/ 15: Birnbaum, W. I/Intro/49: Buchan, A.L. 11/10/56

11/2/1,45: 11/Chapter 9: 11/1/5,18: IV/7/3 Budiansky, B. 1/2/17:f11/9/28,31,54,57,58: Bisplinghoff, R.L. I/Intro/48,49ý 1/8/29,50: 111/2/55:11/10/20,25,56: 111/1/26: 112/15: 1/7/40,41: 11/1/25: 111/7/10,35,36111/4/36: 111/7/8,41: 11/5/56: 11/9/28: 111/1/26,56: Buivol, V.N. 111175/86111/7S/60,70 111/4/25,36: 111/6/33: Bullen, N.I. I11/4/fl7

Atkinson, C.P. 1/6/37,54 111/75/58,62,70: 111/10/21: Buwgers, J.M. 11/1/6IV/l/28: IV/7/27: V/1/10,12 Buigess, M.F. IVf 1/29

Bagdasaryan, Z.E. 111/75/68,69, Black, S.D. 11/10/16,55 Burow, H. IV/10/2770,77,78,84 Bland, S.R. 111/75/86: 111/9/7, Bursnall, W.J. V/2/16,44

Bailie, J. 111/75/88 10,11,24,25 Burton, G.E. IV/l0/28Bairs'tow, L. 1/Intro/46: 11/1/4 Blasius, H. 1/Intro/49 Busemann, A. 11/ 1/ 18:Baker, B.B. 11/'6/57 Bleich, H.H. 1/2/17: 1/8/31 11/9/11,21Baker, i.E. 111/7/12,37,446: Blenk, H. 1/Intro/SO Buxton, G.H.L. 11I/7S/57:

I11/7S/57: 111/9/9,24: Block, D. 111/7S/94 V/3/28,36111/10/22: V/5/14,56 Boersma. J. 11/2/40,45:

Baldock, J.C.A. 111/4/37: VI/TG/4,811I/Chapter 5: V/3/35: Bogliubov, N. 1/6/55:V/4/20,21 111/7S5/

16

Calligeros, J. 111/7S/75 Cunningham, H.J. 11/5114,56,59: Dugundji, J. 1/7/40: 11/5/57:

Carlson. W.C.A 11/10/58 11/7/8,11.12,44: 111/7S/ 10, 111/2/57: 111/7S/62,70,75,81:

Carslaw, H.S. 1/7/39 58,73,85: V/2/9: V/5/56 V/l/12

Carter, L. 111/7S/83,84,86 Curran, J.K. 11/10/20,56: Duncan, W.. J /IntroductoryCarts, F. 111/110/22 IV/5/56 Survey: 1I/ntro/48 ,4 9 ,50:

Chaikin, C.E. 1/6/55 Czuba,T.W. 11/10/16,55 1/2/5: 11/1/4,6,24: 111/3/20:

Chang, C.C. 1/6/56 111/4/20,36: 111/6/18:

Chapple, E.W. 11/ 11/29,67: D'Aiutolo, C.T. 11/10/40,59 IV/5/54: IV/6/1

V/2/6,10,13,15,44 Dalzell, J.F. 1/8/24 Dunn, D.W. 11/9/50,60

Chastenet de Gary, J. 11/8/4,43 Danghaday, H. 111/10/21 Dunadon, D.V. 11/11/35

Chawla, J.P. :1/9/19,55 Dat, R. 1/Chapter 4(E): Durand, W.F. 11/8/43:

Cheilek, H.A. 11/11/34:V/3/25 1/4/41,87: 11/10/54,58: 11/7/75

Chen, C.F. 11/9/2,55 111/7S/14,83,88: Durling, B.J. V/3/34:

Chen, M.M. IV/!/28,30 IV/5/55 V/5/58: VI/TG/5,9

Chinneck, A. 11/9/1,54: Davenport, W.W. 1/2/17 Durvasula, S. II1/7S/41,83,88

II/1 0/ 16,33,54: 11/11/45: Davies, D.E. 11/Chapter 4: Dzygadlo, Z. II1/7S/66,70,75,

IV/5/54: V/5/18 111/7S/10,61,89: IV/9/14 78,79,80,81,83,85,88

Chu, W.H. 1/8/28,29,31,50: Davies, R.J. 111/7S/66

111/7S/64 Davis, C.i. 11/10/56: IV/5/54 Eagleson, P.S. 111/7S/74

Chuan, R.L. 11/9/53,60 Davis, E.L. Jr. IV/5/57 Eastep, F. ili/7S/91

Chubb, R.S. 111/2/56 De Garcia, HJ. 111/10/21 Eckhaus, W. V/5/41,59

Cicala, P. I/Intro/48 ,5 0: de Jager, E.M. 11/10/52: Eggers, A.J. Jr. 11/9/56

1/2/16: 11/1/8,20: V/6/56: VI/TG/4,8 Eisley, J.G. 111/7/11,16,21,37,

11/3/1,40: 11/6/15: Dengler, M.A. III/6/31,33: 41: 111/7S/58,60,71

IV/7/3 V/3/25,36 Ellen, C.H. 111/7S/5,80,90

Clarke, I.F. IV/5/56 den Hartog, J.P. 1/6/22,53: Ellis, C.W. 111/10/21

Clauser, F.H. 1/6/55 V/5/57,58 Emerson, H.F. 11/10/38,59

Clerc, D. 111/6/5,33 Derbentsev, D. 111/7S/86 Epperson, T.B. 1/8/32

Clevenson, S.A. 11/10/32, Destuynder, R. 1/4/20,87: Epstein, A. V/I/11

54,58: 11/11/65,66,69: i1/!0/58 Erickson, A.L. 111/7S/83,84:

IV/5/55: V/3/35: de Veubeke, B.M.F. V/3/34: V/5/41,58,59

V/5/59,60 I/Chapter 3: 1/3/37,38: Etkin, B. 11/1/25

Clymer, A.B. IV/1/29 1/4/12,21: 1/7/39: Evans, E.W. III/7S/62

Coales, i.D. V/1/23,58 IV/3/30 Evenson, D.A. III/7S/87,89

Cohen, H. 1/8/32 de Vries, G. 1/4/2v,21,87: Evvard, J.C. 11/t/22,45:

Cole, J.D. 11/9/56 1V/3/24,30: V/3/37 11/6/16,55: 11/10/43,60

Coleman, R.P. 111/9/17,25 De Young. J. It/I 1/ 19,21,

Coles, W.A. V/2/28,37,46 22,27,28,67:111/9/25 Fage, A. I/Intro/46

Collar, A.R. I/Intro/47,4 8 , Diederich, F.W. 11/1/20: Falkner, V.M. 11/1/21: 11/3/1:

49,50: 1/6/53,55: 11/1/6: I11/Chapter 2: 111/2/55,56, 11/5/33,58: 11/11/19: 111/2/58

111/2/55: 111/3/20: 57,58: III/Chapter 3: Farkas, EF. III/7S/78

111/4/36: 111/6/1,18,33: 111/3/20: V/1/10,1 1,12 Farren, W.S. V/5/56

IV/9/14,15: V/I/I/I: Diethelm, M. 11/9/27,56 Faure, G. 11I/7S/70,87

V/2/14,21,45: V/3/27,36: Dietze, F. 11/2/25,43: Feingold, A.M. 111/9/25

V16/25,55 11/6/56 Felgar, R.P. 1/2/15

Collatz. L. 11/3/33,41 Dixon, S.C. l1/7S/69,73,76, Feshbach, H. 11/3/3,8,41

Congelliere, J. 1/8/32 77,84,87 Fettis, H.E. 11/2/26,44

Conlin, L.T. 11/10/47,60 Djojodihardio, R.H. Filippov, A. 11I/7S/84

Connor, R.W. V/3/36 11/9/30,56 Fischel, 3. 111/7S/75

Constant. 111/7/8 Dobson, A.M. IV/10/27 Fisher, R.A. V/I / I1

Cooper, R.M. 1/8/28 Dodge, F.T. 1/8/32 Fiszdon, W. 111/7S/72:

Copson, E.T. 11/6/57 Donnell, L.H. I11/7/26,28,29, V/5/41,59

Couchet, G. 11/8/3,42 30,41: !11/7S/5,14,4S,47 Flax, A.H. !1/1/25: 11/6/46,57:

Coupry, G. 1/Chapter 4(B): Donovan, A.F. 11/6/55: 11112157: 111/7S/66

1/4/41: I1117S/90: lV/3/30: 1I/ 1/34: V/3/25 FIUIe, W. 111/7126,28,42

'V/5/42,59 Dorozhkin, N.Ya. 1/8/30 Forlifer, W.R. IV/2/21

Courant, R. 11/2/28,44: Dblrr, J. 11/8/3,42 Forsberg, R.H. IV/l/30

111/7/46 Dow, N.F. 111/7S/94 Forshaw, J.R. IV/5/57

Covert, E.E. 11/9/31,57 Dowell, E.H. 111/7S/6,32,41 Foss, K.A. 111/2/56,58:

Cowley, W.L. V/5/23,58 67,74,75,77,78,79,80,81,82, 111/3/20: V/Chapter 1:

Cox, R.N. 11/1/19 83,85 87,88,89,90 V/1/10,11,12

Crisp, J.D.C. 11117/41: Drake, D.G. 1V/5/58 Fox, L. 1/6154

!11/7S/62 Drescher, H. 11!8/40: Fr/lich, 1.W. 1/2/17:

Cummings, B.E. i11/7/41: 11/10/52 111/7S/51,52,74,89

111/7S/61 Drischler, J.A. 11/6/32,56

*1

17

Frazer, R.A. 1/Intro/8,46,48, Giltner, T.A 111/7S/61,62 Hall, W.E. Jr. 111/9/13,2549,50: 1/6/53,55- 11/1/4, Glauert, H. I/Intro/47,48,50: Ham, N.D. 11/9/53,60:24,25: 11/ 2/25,43: 11/6/56: 1I/1!5,6,9,18,20: 11/3/31I: III/Chapter 10: 111/10/22111/2/57: 111/4/36: 111/6/18, 111/2/49: IV/7/3: V/2/13,44: Hanim, M. 111/7S/8833: IV/5/54: P1/6/I: V/5/6,55,58 H armon, S.M. V/ I/IlIIV/ 10/27: V/3/28,36,37 Glazebrook, R.T. 11/ 1/4 Harper, C.W. 11/I11/67

Freelin, J.R. IV/ 1/27 Goland, M. 111/6/31: 111/7/8, Harris, G.J. II1/7S/82Freudenthal, A.M. 1/7/38 42: III/7S/57: I1/1/27: Harris, R.C. V/5/55[Frick, C.W. 111/2/56 V/3/25,36 Hartley, D.E. 11/I 11/63,66,69Friedman, E. 1/7/41 Golden, C.T. III/7S/79 Hartley, E.V. IV/1O/27:Friedmann, P. 111/7S/88 Goldenveiser, A.L. 111/7/28,29, V/4/21Frueh, F.J. 111/7S/64 32,42: 111/7S/8,94 Hartree, D.R. IV/1/29Fung, Y.C. I/Intro/48,50: Goldman, R.L. 111/7/36: Haskind, M.D. 11/2/43

1/2/17: 11/1/25: 11/9/42, 111/7S/61: IV/8/13: V/3/35 Hayes, W.D. I/1/1/I: 11/9/18,59: 111/1/6,26,56: Goldstein, S. V/5/57 25,26,28,40,55,56: 111/7/17,111/4/36: I11/Chapter 7: Gallnitz, H. 11I/4S/10,13,35 37,42: 111/7S/57 I111/7/9,10,11,12,17,37,39, Gontkevich, V. 111/7S/82 Head, A.L. 111/9/21,25:40,42: 111/7S/6,7, 10,11, Gonzales, R. 1/8/31 IV/7/27: IV/8/14: V/3/8,3414,44,45,59,60,61,65,68, Goodier, J.N. IV/1/29 Heard, W.L. 111/7S/79,8171,73,74,88,91,93: Goodman, L.E. 111/7/21,45,47: Heaslet, M.A. 11/1/26: 11/2/28:IV/ 1/28: V/I/I10 111/7S/65,66 11/6/46,47,56,57: 11/7/75:

Goodman, T.R. 11/6/58 111/2/56,58Gainer, T.G. V/5/60 Gossard, M.L. 1/2/8,16: Heath, B.O. 111/4/36Gaji, B. III/7S/85 1/7/40: IV/1/27 Hedgepeth, J.M. 1/Chapter 2:Gallagher, R.H. 111/7S/5,93: Gothert, B. 11/1/18,20 1/2/16: 111/3/20: 111/7/8,10,

IV/ 1/30 Gourbil, L. 11/10/38,59: 14,15,17,19,24,25,26,27,28,Gardner, C. 11/6/43,57 IV/ 10/28 29,32,35,36,42,43: I11/75/6,Garner, H.C. 11/1/21: Grame, W. 11/6/56 16,17,18,32,.35,57,59,60,61:

11/3/2,37,40: 11/5/34,59: Grahamn, E.W. 1/8/30 IV/l/29: V/1/1211/10/53,55,57: 11/11/68 Gray, A. 11/1/6 Hedman, S. 11/9/30,56

Garrick, I.E. 11/Chapter 1: Greenberg, J.M. 111/10/22 Helmholtz, H.L.F. (von)II/1/8,9,I9,22,26,28,41,4.4- Greene, P~. 111/7S/87 11/1/14: 11/2/9: 11/8/4,1211/3/2,41: 11/5/12,56: Greenspon, i.E. 111/7/36: Hemp, W.S. 1/Chapter 1:

116/,I,3,511/9/8,55: I11/ 7S/61 1/1/2011/ 11/68: 111/4/36: Greidanus, 3MH. 11/1I1i18: Henderson, A. 11/10/47,60111/7/12,42: 11I/7S/60,73: 112/26: 11/10/6,52: Henning, A.B. V/5/60IV/7/3,5,26,27: P1/8/8: 11/11/8: P1/5/55: V/01l0 Herr, R.W. IV/7/25: V,;5/60V/2/9,19,21,45: V/3/1,18,34: Grigoliuk, E.I. 111/7/42: Herrera, R. 11/10/54V/5/58: V/6/55: VI/TG/5,9 III/7S/77,79,80 Herrminn, G. 111/7/43

Gamz, L.R. 1/8/29,32,50 Grinsted, F. 111/3/20 Hertrich, H. 111/4S/10,35Gaspers, P.A. 111/7S/84 Gwoen, M. 111/7S/64 Hess, J.L. 11/9/33,56Gates, S.D. 1/Intro/46,48: Grote, H. 111/4S/13,35 Hess, R.W. 11/10/55:

111/7S/92 Guy, L.D. 111/7S/67,71,76 II1/7S/47,64,73Gaugh, W.J. 111/2/57 Guyett, P.R. 11/10/20.56: Hicks, W.D.T. 1/6/54:Gaukroger, D.R. PV1/9/IS: 11/Chapter 11: IV/5/54,S6: IV/5/57

V/Chapter 2: V/2/21,28,40, P1/9/IS Hilbert, D. 11/2/28,4444,45,46: V/6156,57 Guz, A.N. 111/7S/86 Hildebrande, F.B. 1/6/53

Gauzy, H. 1/3/38: 1/Chapter Hill, G.T.R. V/I/104(A): 1/4/21,41: IV/Chapter 3: Hawck, W. 11/9/27,56 Hlraokn. K. 111/7S/76IV/3/30 Hama J. P1/ 1/29 Hitch, H. IV/l10/27

Gayman, W.H. P1`/8/ 13 Habip, L.M. 1/8/32 Hjelte. F. 11/9/19,55Geissler, E.D. 1/8/30 Halines F.D. 111/7S/62 Hodge, P. 1/7/39George, W.D.T. II/1/ 15,S Haley, S.M. V/j/16,2S Hodson, C.H. 111/7S/78

1119/51.60 Halfn'an, R.L. l/Intro/48: Hoff, N.J. 1/7/39Gerber, EMH. 11/1/20: 11/6/57: 11/9/S2,60: 11/10/52.56: Hofsormznqr, DiJ. VIITG/5,8

It/ 10/23,30,32,56: 11/11/ 10. 11/ 11/8,66. 111/10/22: Hohenemser, KMH. 111/10/22I I, 12,18,21,26,27,39,66: P1/1/30: P1/5/56: Holder, D.W. V/5/44,60V/6/56 IV/7027: IV/8/4.5,13: Holliday, P.T. V/3/36

Gore, iN. 1/7/40 V/S/'16.25.56 Holt, M. 11/9/33,57: 111/7/28,Gert, T.Ya. 111/75/69 Hall, H. 11/11/29,30,67: 29,30,32,43,45: 111/7S/10,Glavotto, V. 111/7S/8I V/2/S,6,10, 13.14,15,28, 44,61,62,63,74,77Gibson, F.W. 111/7S/73 37,44,46 Houbolt, i.C. 1/2/I5: 111/7/ 10,Glesng. 3.?. 11/9/2,28,30,54 Hall, J.C. 111/4/37: 43: 111/7S/6,16,62,89:Gilnian, J. 11/7S/69 IV/Chapter 4 111/9/10,24: IV/ 1/29:

V/2/43,44,46: V/3/ 13

18

Houghton, D.S. 111/7S/68 Kacprzynski, J.J. 11/9/31,32,33,35, Lall, T.R. !11/7S/81

flovanessian. S.A. 116!54 37,57.58 Lamb, H. 1/8/29: I!/1/4:

Hoyle, R. 117139 Kaliski, S. 11/7S/66,71,78,80, 11/5/32,58

Hsu. C.C. 1/6!53 82,88 Lamboume,N.C. 1I/!/17:

Hsu, K.H. 111/75/89 Kalnins, A. 1/8/31 11/10/33,58: 11/11/45,68:

Hsu, P.T. 11/3/2,34,37.41- Kana. D.D. 1/8/31,32 IV/Chapter 6: IV/7/12:

11/5/34,59: 11/9/33,57 Kantorovich, LV. 111/7S/6,35,93 V 2/28,34,35,38.45:

liuang, T.C. 11618,55 Kaplan, S. 11/9/54 V/Chapter 5: V/5/57,58,59

Huckel, V. 11/2/33A44: Kappus, R. 111/6/5,33 Lamp~r, R.E. 111/7S/65,74

11/5/56: V/311,18,20, Karamcheti, K. 111/7S/86 Lanchester, F.W. l/Intro/45,

34,35: V/5/58: Kariappa. 111/7S/90 49: 11/1/4

VI/TG/5.9 Kell, C. IV/9/15 Lanczos, C. 111/2/57

Hudson, M.L. 111/75/87 Kell, R.J. 111/3/20: V/1/12 Land, N.S. 1I1/7S/89

Hunsaker, J.C. 11/1/4 Kelsey, S. 11112/26 Landahl, M. 1|/1/15,19:

Hutton, R.E. 1/8/30 Kelvin, Lord. 1i/1/4,5,6,14: 11/2/0,42: 1114/2,7,49,52,11/8/4: 111/7/34 61,119,120: 11/7/75:

lift, I. 11/lli8,53,56,66,69: Kennedy, C.C. I/3/20,35,38: 11/Chapter 9: 11/9/13,20,

111/6/31,33: VI/TG/5,8 IV/7/25: IV/8/3: IV/10/8,27 22,'1,54,55,57,58:

Isaacs, R.P. 111/7/17,37,43: Kennett, H. 111/75/65 IU/ 10136,37,36,39,42,53:

I!1/7S/57 Ketter, D.J. 11117S/76,85 U1/75/14,94: V(5(43:

Ishii, T. i1117S/68,81,87 Keune, F. 1f/1/13 V/5/60

lzmailov, A. 111/75/91 Kind, R.J. 11/9/49,59 Langley, R. 111/7S/78

Kinnaman, E.B. IV/7/27: Laschka, B. 111/4S/10,35

Jaeckel. K. 11/3/33 IV/8/13 Lauten, W.T. IV/Chapter 1:

Jaeger, J.C. 117/39 Kirkby, W.T. 1/4/49: IVIl/29: IV/9/15

Jan. H.A. 11/2/28,44 IV/Chapter 10: IV/10/27 Lawrence. 14.R. 11/1/20:

Jeffreys, H. 1/3/37: !/7/75 Kliauz, L. 111/75/85 -1/6/55,57: 11/10/23,30,32,

Jeffreys.Lady. 11/7/75 Klotter, K. 1/6/53 56: 11/I 1/10,11,12,18,21,

Johns, D.J. 111/7/13,20,21,43,46: Knechtel, E.D. V/5/61 26,27,39,66: V/6/56

Ill/Chapter 75: 111/75/8,62,65, Kobayashi, S. 11/7S/45,72,75, Lazennec, H. III/Chapter 8

66,68,70,74,75,76,77,79,81,83. 76,79 Leadbetter. S.A. 11/10/32,58:

92,93 Kobett, D.R. 111/7S/10,73,76, 11/11/65,66,69: V/3/35

Johnson, H.C. 11/9/60: 11/10/35: 77,83,84 Leclerc, J. 1/Chapter 4(D)

V/5/16,25 Konditsina, E. 111/7S/87 Lee, E.H. 1/7/39

Johnson, W.H. IV/10/27: Koning, C. 1/Intro/46, 49 Lee, F.A. 111/7S/72

V/5/57 Kopzon, G.I. 111/7/28,29,43: Lees, L. 11/9/28,56

Jones, C.H. 111/10/21 111/75/59 Lehrian, D.E. 11/3/1,40:

Jones. J.P. l/lntro/26,4 8 : Korbut, B. 11117S/87 11/5/33,59: 11/10/57,60:

1/6155: 11/9/52,60. Kordes, E.E. 1/2/17: 111/75/62, 1/I I/18,27,45,67,68:

111/10/22 66,70: IV/1/30 V/6/56

Jones. R.T. i1/1/19: 11/6/6, Komecki, A. 111/7S577 Leissler, L.A. 111/7S/58

11,27.30,55 111/2/49 Kotyukov, V.G. 111/75/78 Lemaire, D.A. 11/11/68:

Jones. W.P. Editor of Manual: Krumhaar, H. 111/7S/6,10, V/6/56

li/i / 14,21: 11/2/24,26,43: 44,69,72,75 Lemley, C.E. 111/7S/87,91

11/3/1,2.40: 11/5/31,33,58: Kruszewski, E.T. 1/2/16,17: Leonard, H.W. 1/8/30

11/6/I1,32,',0,55,56: 111/7S/72 Leonard, R.W. 111/7/10,24,25,

11/8/4,43: 11/9/1,54: Kryloff, N. 1/61/55 26,27,28,35,36.43: 11117S/

11/10/52,53,56,59: Krylov, V.I. I1d/7S/51,93 59,60

11/! !/9,10,11,12.17,21,22, Kuhn, P. 111/2/57: IV/1/29 Leroy, lean. 1/8/31

26,27,30,44,67,68: KUssner, H.G. I/Intro/4 8,50: Lessing, H.C. 1Il10/23,25,57

111/4/36" 111612,33: 1/6/22,46,53: 11/1/6,8,9, Levy, L.L. V/5/61

IV/5/58: IV/10/27; V13/28, 13,20: 11/2/6,16,42: 11/3/1, Levy, S. 1/2/14,16: IV/1/27

36: V15/6,7,55: VI/TG/4,8 16,40,41: 11/6/47,58: Lewis, F.M. IV/10/28

Jordan, G.B. I!!/75/70 11/Chapter 8: 11/8/3,14,30, Lewis, R.C. 1/3/2,36.

Jordan, P.F. 11/1/1 5: 11/2/44: 42,43: 11/9/2,28: 11/10/6, 1/4/16,21: IV/Chapter 2:

11/5/34,5 9 : 11/10/14,54: 20,52: 11/11/68: I/1/13,15, IV/2/21: IV/7/25

11110/48.51,60,68,69: 111/411,31,32: Ill/Chapter 45: Li, T. 11/5/57: V/6156

111/7/34,36,43: 111/75/57,59: 111/45/10,35: 111/7S/58: Li, T.M. !I1/75/87

1V/5/59: IV/7/27: IV/8/13: IV/7/3: VI/TG/5,8 Li, Yr. IV/5/57

V/2/8,44: V/5/7,55: V/6/56: Lihjn, E. 11/5,57

VI/TG!4.5.8 Lagerstrom, P.A. 11/9/54 Librescu, L. 111/75/69,72,74,

Joyner, U.T. 11/10/53 Laidlaw, W.R. 1I/10/23,30,56, 80,83,86,87,90

Julia, G. 1/4/72 57: 11117S/73 Liebers, F. 1/Intro/50Liepmann, H.W. 11/1/26

19

Lighthiil, MJ. 11/1/11,15,26: Mahortikh, ZILK. 111/7/17,47: Minhinick, 1.T. 1/2/15:11/2/2'3: 11/7/ 75: 11/9/1,8,19, 111/7S/63,65 11/10/53,54: 11/1 1/19,21,31,25,34,35,37,39,54,55,58,59: Malain, E. 111/7S/90 32: V/6/56: VI/TG/4,5,8,911/10/54: 111/2/58 Mangler, K.W. 11/3/34,42: Mirowitz, L.I. 111/7S/72

Lin, C.C. 1I/l/18: 11/2/1,42: 11/4/27,119: 11/5/42: Mirsky, 1. 111/7/4311/4/119: 1119150,60 11/10/36,39,59 Mitchell, C.G.B. 111/4/37

Lin, H. V/1/Il Mannes, R.L. V/5/58 Mitchell, D.H. 111/7/37,44:Lindholm, V.S. 1/8/31: Mansfield, E.H. 111/4/26,36 I11/7S/61

111/7S/94 Manson, P.W. 1/4/86 Mitchell, R.R. 111/7S/91Linebarger, 1. 11/9/50,59 Marchenko, G. 111/7S/84 Moiseev, N.N. 1/8/28,31Lisunov, A.D. 111/7S/66 Marguerre, K. 1/7/27,40: Mollo-Christensen, E. I1/ 1/ 18:Livanov, KiJ. I11/7S/64,78 111/7/23. 11/2/1: 11/4/119: IV/l/5,29:Lock, M.H. 111/7/12,44: Markorov, B.P. 111/7S/67,68 V/5/41,59

111/7S/ 10,62,63,68,71,72, Marshall, P.L. V/5/61I Molyneux, W.G. 11/10/23,33,78,79 Martin, D.J. 11/10/54: 56,58: 11/11/29,30,67:

Loewy, R.G. 111,/9/11,24,25: IV/Chapttr 1: IV/l/29: IV/5/54,55,56,57: IV/6/"!5:111/10d/21 V/6/55 IV/Chapter 9: IV/9/15:

Lofts, M. 11/ 11/68 Martucelli, J.R. 11/10/16,55 V/2/5,10,13,14,23,28,40,43,Lohmann, K. I1I/4S/l0,35 Martz, C.W. 11/10/58: 44,46: V/Chapter 6: V/6/25,Loiseau, H. 1/4/20,41,87: V/5/32,58,60 55,56,57

V/5/50,59,60 Mathews, C.W. I11/7S/92 Monfort, i.C. 11/10/53Lomax, H. 11/ 1/26: 11/2/28, Mathews, G.B. 11/1/6 Moore, F.K. 11/9/39,41,53,59,

44:11I/Chapter 6: 11/6/55, Matsensaki, Y. lI1/7S/79 6056,57,58: 11/7/75: 111/2/58 Mayo, A.P. IV/ 1/30: V/ I/IlI Moore, i.A. 11/10/46,47,60

Love, A.E.H. 1/1/20: Mazelsky, B. 11/ 1/ 19: Moore, M.T. I1I/7S/74II1/7S/7,93: IV/l/28 11/6/55,56 Morgan, H. 11I/7S/61

Lowson, M.V. 11/7/75 Mazet, R. Editor of Manual: Morins, L. 111/75/84Luce, R.G. 1II/7S/75 1/4/12,21,71: 11/8/3,42: Morse, P.M. 11/3/3,8,41Luessen, G. 111/7S/71 IV/5/54: IV,'10/17,19,28 Moseley, W.C. 11/10/59:Luke, Y.L. 111/6/31: 111/7/8, Meekishef, G.N. 111/7/47: V/5/60

16,18,42,44,46: II/7S/57, 111/7S/63 Moss, G.F. 11/10/30,57:58,59,61: IV/1/27 Melan, E. 1/7/38 IV/5/57

Luscombe, P.D.R. IV/l10/27 Mendelson, A. V/5/14,56 Movchan, A.A. 111/7/10,17,29,Lyon, H.M. 111/2/56: Menees, G.P. 11/10/23 44: 111/7S/6,16,20,59,60,

111/3/20: III/7S/92 Menkes, E. I1I/7S/89 65,72Lyons, D.J. 111/7S/92 Merbt, H. 11/1/19 Movchan, A.1. 111/7S/72

Mercer, A.G. 111/7S/I11,94 Movsisyan, L.A. 111/7S/87McCann, G.D. IV/7/26 Meyer, E. 11/1/9 Muhlstein, L. 111/7S/84,89McCarthy, JRF Jr. IV/1/30: Miakushev, A. 111/75/85 M~iller, P. 111/7S/91

IV/7/27: IV/8/4,5,13 Michael, W.H. 11/1/19: Mul1ler, W. 111/4/18McCarthy, J.L. 1/8/29,30,50 11/7/61,75 Multhopp, HI. 11/ 1/21: 11/3/ 1,McClure, J.D. 11/9/45,50,51, Migotsky, E. 11/6/56 2,28,30-33,37,40: 11/4/119:

52,59: 111/7S/29,71,94 Mikhaylov, A.P. 11I/7S/80 1./5/33,42,58: 111/2/58:McElman, J.A. II/7S/37,53, Mikishev, G.N. 1/8/30 V/6/56

77,79,80,89 Miles, C.JW. 11/10/35,40,57: Munk, M. 11/1/5,19McFeeley, i.E. 111/7S/88 V/5/20 Mykytow, W.i. IV/Chapter 7:Macgeorge, W.D. IV/ 1/ 18,29 Miles, i.W. 1/6/55: 1/8/5,15, IV/Chapter 8McIntosh, S.C. 11/9/23,24,37, 29,31,44,45: 11/ 1/ 13,18,

56: 111/7S/84 19,26: 11/2/1,28,41,42: Nacht, M. II/7S/87McKillop. 111/9/16 11/4/119,120: 11/5/14,15, Nagholi, P.M. 1/2/17McKinney, R.L. III/7S/74 31,56,58: 11/6/43,47,56, Nakamura, Y. V/5/44,55McKinnon-Wood, R. 57,58: 11/7/10,13,74,75: Nayler, J.H.F. 111/75/68

1/Intro/47,50 11/9/21,33,45,50,54,55,59: Naylor, H.F.W. 111/9/13,14,15,McLachlan, N.W. 1/6/54: 11/ 10/37,38,43,55: 111/6/33: 16,25

11/2/42: 11/7/75 111/7/10,11,17,24,25,26,29, Neal, B.G. 1/7/39McMillan, G.A. 1/1'itro/47, 30,34,35,36,44: 111/7S/Il1, Neilsen, 11/10/20,25

50: 111/3/20 20,57,58,59,60,61,63,66, Nelson, H.C. 11/2/35,44:Macneal, R.H. IV/7/26 69,94 11/5/14,56,58: 11/10/53,59:MacRobert, T.M. 11/1/6 Miller, R.li. 111/10/21 111/7/8,11,12,44: 111/7S/58:McRuer, D.T. 1/5/46 Milne 1/6/24 IV/9/15: V/2/45: V/3/34:Macder, P.F. 11/1/13 Milne, R.D. H1/ 11/66,69 V/5/58: VI/TG/5,8Magnus, R.J. 11/9/53,60 Mmn-Dc, D. 111/7/8,46: Neubert, H.K.P. 111/4/37Magnus, W. 11/2/44 111/7S/61,82 Neumark, S. IV!3/30Mahaffey, P.T. IV/7/27: Mineur, H. 11/3/16,41 Newmark, N.M. 1/2/13,16

IV/8/14: V/3/34

20

Niblett, LIT. III/Chapter 5 Presneil, J.C. 111/7S/68,74 Rich, R.L. l11/7S/79Niesytto, J. 111/7S/68 Press, H. 111/4/37 RcadaI/02NixnD. /246Preston, ill. 11/ 1/ 14 Richardson, J.R. If/ 1/21:Noll, R.B. 11l/7Sj70 Price, G.W. V/5/60 11/3/2,3,10,37,41: 11/4/119:Novichkov, lu.m. 111/7S/67,71 Pride, R.A. 111/7S/77 11/5/34,58: 11/10/55:Novozhiloy, V.v. 111/7S/8,93 Pritchard, AJ. 111/7S/20,89, 111/7S/92: 111/9/13,14,16,2SNowacki, W. 1/7/39 90,94 Richey, G. 1/6/46,54O'rin.T.. 117S65Probstein, R.F. 11/9/28,40,56 Riley, 1/8/00O'reTF.117/5Pugh, P.G. 11/10/18,55: Ripley, J. 111/2/S6: 1113/20:-1)berhettinger, F. 11/2/44 V/5/55 II1/7S/92Odqvist, F.K.G. 1/7/39 Pugaley, A.G. 1/Intro/47,SO: Roberson. R.E. 1/6/25,54a')gbalov, P. 111/7S/82 111/2/56: 111/3/20 Robinson, R.C. 11/10/38,59:Oglesby, T.H. IV/1/30 Puttick, E.B. V/2/14,21: V/5/59Olson, JJ. 11I/7S/6,10,45,76 V/6/2S Rodden, W.P. 111/7/9,16,17,18Olson, M.D. 11/9/50,59:I

353445471I//511175/0,8,8,8889, 1 Quinn, J.F. IV/ 1/30 7,41,61,63,70,78,93:Ol88on, C.O. 11/ 10/39,59: Quozzo, G. 1l1/7S/76,77,91 I1/1/28I1/5/54 Rodriguez, A.M. 1/8/30OrliK-RUckemann, K. 11/9/41, Ruab, A. 1/Intro/49 Rogers, M. 1/8/3 2j42,46,48,49,59: 11/10/39,47, Rabinovich, B.I. 111/7S/63 Roos, H. IV/IO/2748,59,60: IV/S/54,57 Rabinovich, F.I. 1/8/15,31 Rose, R. 11/10/40,59Osgood, W.R. 1/7/39 Rabinowitz, S. 11/2/26,44: Rosenbaum, R. 11/1/26:Ostrach, S. 11/9/41,59 VI/TG/4,8 I1/1/28Oswatitsch, K. 11/1/13 Rainey, A.G. 11/9/52,60: Rosenberg, R.M. 1/6/54,55Otto, E.W. 1/8/32 11/10/54: 111/ 10/22: Rosencrans, M. 111/75/64Owen, T.B. IV/5/57 IV/5/55: V/3/34: R~ho .1/16 //35

Pai, S.I. 111/2/56 Rab/14,2W.6/7/3 Rost, J. IV/3/21,30Rambrg, . 1//39Rott, N. 11/1/15,18: 11/2/36,Paidouinsis, M.P. 111/78/85 Randall, D.G. ;1/7/75: 37,44: 11/9/51,60Pancu, C.D.P. 1/3/20,3S,38: 11/9/38,58 Row, P.V. 111/7S/75IV/7/25: IV/8/3: IV/l0/8,27 Randals, W.C. III/7S/58 Routhi, E.J. I/Intro/15-16Parks, P.C. 111/7/46:111I/7S/l7, Ransleben, G.E. Jr. 1/8/3 2 Roxbee Cox, H. I/lntro/38,47,66,80,87,88,89,90,94 Rattayya, J.V. 1/8/30: 49,50: 111/3/20: V/ I/ I IParkus, H. 1/7/38 111/7/21,22,45,46,47: Rubbert, P.E. 11/9/20,22,23,Pearson, H. V/5/57 1,117S/65,66 30,55,57Pearson, H.A. 111/3/20 Rattinger, 1. IV/l/29,30 Rbn .183Pengelley, C.D . IV /8/13: R sc e , M 1 2 8 12 6:R ubin o, S .. 1 1/1/3 2 2: 1 / / 8

V/1/2: /3/5 P/1/28: P1/7/3: IV/8/13: 44: 11/5/56: 11/9/55: 111/7/12,Pedisho, C.H. 111/10/21 V/5/56 42: V/5/58: VI/TG/5,9Perlmutter, A.A. 111/7S/73 Ravera, RiJ. 111/9/11,24 Ruddlesden, F. 11/I10,'23,56,58:Petrone, DA. 1'/8/32 Rayleigh, Lord. 1/3/2,35,36, P1/5/56,57: V/6/25,56PetrshD.A 1//3237: 1/4/12,21 Runyan, H.L. 11/1/21,42,43:Petrov, A.A. 1/8/28 Raymer, W.G. 11/ 11/35: 1//1:153,9PV/5/4p ,59H. 14/9 V/5/20 11/10/53,59: I11/7S/61:V/54159Raymond, J.L. 11/1/16 P1/5/59: V/2/45: V/3/35:Plan, T.H.H. 1/7/41: V/I/IlI Redd, B. 1II/7S/84 V/5/6,55,58: V/6/55

Piercel, G. 11/9/ ,56 Reed, E.G. 11/10/53Pirc, .119/6Reed, W.H. 1I1/Chapter 9: Sabatuik, A. V/5/57Pines, S. 11/1/22: 11/5/19,57: 111/9/10,13,22,24: St. John, A.D. 111/7/8,16,18,11/6/57: 111/2/57: 111/7/45: P1/9/13,15 4:11756IV/8/7,l 1,14: V/3/16,35 Reese, D.E. 11/10/32,47, Saito, H. V/5/59Pinkerton, R.M. 11/1/14 48,58 Sanders, J.L. 1/2/13,14,16,17:Pironneau, Y. 1/3/38: 1/4/21 Regier, A.A. IV/7/26: 111/2/57. P1/1/28FPlatzer, M. 111/7S/81,85 V/Chapter 3 Sandorff, P.E. 1/8/24,32Plaut, R.H. 111/7S/87,89 Rein, J.A. V/2/22,45 Sankaranarayanan, R.Ponomarenko, V. 111/7S/82 Reismner, E. 1/2/17: 1/8/ 18, 11/9/31,57Posaio, C. 1/Intro/48,SO: 31: 11/1/18,19,20: 11/2/I, Santini, P. 1/7/40:11/ 1/9,18,20,21,22: 11/2/25, 43: 11/3/1,40:11/6/57: 111/7S/77,8526,43: 11/10/10 11/ 11/9,10,21,27,66: Sarkisyan, V.S. 111/7S/92Poulter, D.E.G. 11/10/20,5 16: IV/5/58 SudrH I/SIVIS/56 Reissner, H. 11/1/20: Saunersei, H. 11/9S/27,3,5Prager, W. 1/7/39 111/2/55 Scanlan, R.H. 11/1/26:Prandtl, L. 11/1/8,9,13,18,20: Revell, J.D. 11/9/33,34.35, IV/ 1/2811/6/30: 11/8/39: 111/2/49: 57,58: 111/7S/5,70 Schade, Th. 11/2/25,26,43:111/4S/10 Ribner, H.S. 111/9/10,24 11/6/56

21

Scbaffr, H.G. lih7S/79,81 Sobey, AJ. I71//83 Testa, R.B. 117/41Schindler. A. 112/45: V/6/56 Sidbngn, H. W12/16,42: Theodorsen, Th. l/Intbro/47,50:Schmiedua, C. 1/6/37,41,S3 116/55: 111/2/58 11/ 1/6,8: 11/2/10,42: 11/6/14,Schnittpr, J.R. 111/10/22: Sokolnlkoff, E.S. IV/1/30 21: 11/8/20: 11/10/6:VS/S/6 Sokolnikoff, 1.S. I1/1/28,30 11/I 11/68: 111/9/11: IV/7/3,Schuchardt, H. 1/6/54 Solarz, L. 111/7S/71,78,83,85 26: V/3/1 8,34: V/6/55:Schuerch, H.U. 1/2/16: Somashekar, D.R. 111/7S/90 V1/TG/ 1.2,3

1112/57: P1/1/27 Sommerville, D. 111/7S/83 Thielemann, W. 1/6/46,S5Schult, E.D. V/1/11 Sorensen, R.M. 11/10/14,54: Thomas, H.H.B.M. 11/ 11/68Schwartz, I. 11/ 11/68 V!S/48,59 Thomas, M. 111/7S/68Schwartz, L. 11/2/16,42: Souriau, J-M. 11/8/4,43 Thompson, R.F. 11/10/59:

11//3,4,42,43: VI/T/5,8 Southweil, R.V. 1/1/20 V/5/60,61Schwarz, M.D. 1/4/40 Spencer, B.R.F. 11/3/34,42: Thomson, R.G. 111/75/72Schwarzchld, K. 11/4/38, i20 11/4/27,119 Thomson, W.T. 111/3/20Scruton, C. 11/10/16,25,30,52, Spreiter, J.R. 11/6/46,47,57: Tijdeman, H. VI/Tables and

55,57,58,60: 11/11/35,68: 11/9/2,20,54,55: 111/2/56 GraphsP1/5/55,56: P1/Chapter 6: Spriggs, J. 111/7S/90 Timman, R. 11/1/ 18: 11/2/26,P1/7/12,27: V/5/23,S5,57,58 Squire, H.D. 11/1I/ 14 43: 11/3/16,41: 111/9/11,24:

Sears, W.R. 11/ 1/8,9: 11/4/69, Stahle, C.V. P1/2/21: V/3/35 111/10/22: IV/5/5871,80,100,120: 11/6/47,55, Stark, V. 111/7S/94 Timoshenko, S. 1/7/40:57: 11/7/12,74: 11/9/33,57: Stearinan, R.D. 111/7/36,37, 111/7S/8,93: IV/1/29111/2/56 38,45: 111/75/10,63,71,73, Tobak, M. 11/6/58: 11/9/38,58:

Sep, Z. II1/7S/68 76,79,84,86,89,90 11/ 10/32,33,46,47,58,60:Sethum P.R. 1/6/8,54 Stein, M. 1/2/13,14,16: V/5/10,55Sewall, .J.L. P1/1/28: V/2/45: 111/2/57: P1/1/28 Tolins, I.S. 1/7/39

V/3/1 Stenton, T.E. 11/9/33,57 Tommassoni, L.E. V/2/45Shal'da, L.M. II1/7S/81 Stepanov, R.D. 111/7/25,26,28, Toulson, K.W. 111/9/9Shandarov, L.G. III/7S/74,89 29,32,45: 111/7S/60,64,65,67 TiaiII-Nash, R.W. 1/3/35,38:Shurpe, G.D. V/3/27,28,36: Stephens, D.G. 1/8/29,30,50 P1/2/21

V/6/55 Stephenson, i.D. V/5/41,.58 Trembath. 1/8/50Shen, S.F. 1/6/22,53: 1117/10, Stepniewski, W.Z. 111110/21 Trilling, L. 11/1/17: V/5/41,59

11,36,37,40,45:I111/7S/57, Steme, L.H.G. IV/5/5'6 Troutman, J.L. 11/10/2359,63 Steuding, H. 11/8/43 Trubert, M. 11/ 10/54. P1/5/55

Shenhman, A.M. 111/9/25 Stevens, i.E. 11/6/57: 11/ 11/9, Tsein, H.S. I1/ 1/ 18: 11/2/ 1Shideler, J. III/7S/84,94 10,19,21,22,27,66 Tukey, J.W. 111/4/37Shirk, M.H. III/7S/76 Stewartson, K. 11/4/99,120: Tuovila, WJ. 1/4/86: 11/ 10/55:Shore, C.P. III/7S/76,90 11/5/31,58: 11/6/57: 111/75/47,64,68,89Shulman, Y. 111/7/28,29,30, 11/10/43,60 Turner, M.J. 11/2/26,44:

33,45: III/7S/42,64 Stocker, J.E. II/7S/69 IV/ 1/28: VI/TG/4,8Shveiko, Y.Y. 11l/7S/45,66, Stofan, AJ. 1/8/29,50

68,78 Stoker, J.J. 1/6/54: 1/8/28 Unterberg, W. 1/8/32Sibley, i.D. 111/10/21 Strack, S.L. 111/7/28,29,30,Silveira, M.A. 1/8/29: V/3/37 32,45: II1/7S/63 Valensi, J. IV/5/58Silverstein, A. 11/10/53 Strang, W.J. 11/6/57 van der Neut, A. 1/7/40Sims, J.L. 11/9/37,58 Strass, H.K. Vi/1/ 12 van der Pal, B. 11/2/45:Singer, J. 1II/7S/5,93 Stroud, W.J. II1/S/94 11/5/56Sinnott, C.S. 11/10/53: StUder, H.L. I/Intro/48: van der Vooren, A.1. 11/ 1/ 18,11/ 11/44,68 11/9/60: IV/7/3: V/5/12,56 26: lI/Chapter 2: 111/2/26,Sisto, F. V/5/57 Sumner, I.E. 1/8/29,30 40,41,42,43,45:1[1/3/16,41:Skalak, R. 1/8/32 Sundararajan, V. 1II/7S/91 11/10/6,8,52,53: 11/ 11/8,53,Skan, S.W. 11/6/56 Sykes, D.R. II1/7S/92 56,69: 111/4/12: I11/4S/35:Skurlatov, E. III/7S/86 Sylvester, M.A. 111/7/12,37,46: I11/Chapter 6: 111/6/5,19,33,Slap, i.K. 111/2/57 I1I/7S/57,58,59 34: 111/9/11,24: 111/10/22:Smilg, B. IV/7/26: V/5/6,41, Symonds, P.S. 1/7/139 V/5/57: VI/Tables and

55,59 Graphs: VI/TG/4,5 ,8Smirnov, A. III/7S/86,90,91 Targoff, W.P. IV/7/25,27: van Darn, N.H. 11/11/ 19Smith, A.M.O. 11/9/29,33,56 P1/8/4,13 van Dyke, M.D. 11/ 1/ 15:Smith, A.D.N. V/Chapter 4: Taylor, E.S. 111/9/1,24 11/7/12,75: 11/9/8,11,13,14,V/4/21 Taylor, H. IV/S/57 18,54,55,58: 11/10/16,17,Smith, F. 1/6/54 Temple, G. 11/2/28,41,44: 18,34,43,45,49,54: V/5/9,55Smith, G.E. 1II/7S/67 11/3/2,41: 11/5/56 Veletsos, A.S. 1/2/16Smith, N.H. V/3/34,36 Templeton, H. 1/lntro/48,5 1: Ventres, C. 111/7S/89,90Smith, R. 111/9/9 IV/1/28: IV/7/3,5,27: Victory, M. 11,9/60:Smith, W.D. 111/9/21,25 IV/ 10/27: V/3/25 ,28,34,36: V/5/I14,56

V/5/55,56 Villaggia, P. 111/7S/75

22

Vincente. W. 11/10/53 Webb, G.R. 111/7S/88 Woodgate. L 11/ 10/118.25.30.Viasov, B.F. 111/7S/62 Weber, R. VI! rG/S,9 55,60: V/5/55Viasoy. V.S. 111/7/46 Weeks, G. 111/7S/94 Woods, L.C. 11/814,43Voight, H. IV/7/3: V/3/25, Weidman, D.J. 111/7S/82: Woolston, DS. 1/6/43.46,54,

28,36 IV/l1/30 55:- 1H/1/21,42,43: 11/4/119:Volkof, A.N. 111/7S/62.91 Weiner, i.H. 1/7/38 11/5/33.59: 11/10/23,S6,59:Volterra, E.. 1/3/14,37 Weasnger, J. 111/2/49,58 IV/l1/29: IV/5/56,59:von Baumhauer, A.G. I/Intro/46 Weston, D. V/2/45 V/2/45: W/3/19,20,35,37:

-Ivon Dorbely, S. 11/2/28,44 White, E.C. IV/10/28 V/6/55von Gonap, G. 11/g/3,42,43 White, R.B. 11/9/37,58 Woroozyl, S. 111/7S/82,85,88von Kinnan, Th. 1/7/27.40: White, R.P. IV/7/25,27: Wrisley, D.L. 1/3/2,37:

11/1/8,15: 11/6/47,55: IV/8/4,13 1/4/16,21,40: P1/Chapter 2:111/7S/49: V/3/35 Whitanarsh, G.E. 11/10/57 P1/2/21: IV/7/25

von Mises, R. 11/8/19,21,37,38: Widmayer, E. 11/10/54,57: Wykes, J.H. 111/7S/73IU/4S/ 13,17,19,20,21,25 P1/5/S S Wys, J.A. 11/10/ 14,53,54:

von Schlippe, B. IV/ 10/2,27 Widnall, S. 11/7S/82 V/5/48,59Voss, H.M. 11/ 1/2 1: 11/5/15: Wieghardt, K. 11/6/21,55

111/7/28,32,33,46: Wielandt, H. 111/4S/13,17,19,20, Yanagzawa, M. 111/7S/68111/7S/8,42,44,65,67, 21,22,23,25,36: 111/6/19,20, Yarymovych, M. 1/8/3274,75,76,77 33 1//6Yates, i.E. 1117/23,24,47:

Wieat, K.C. 11/9/60: 11/10/6, 11117S/64Wagner, H. 1/Intro/47,50: 8,28,52,53,S6,57: 11/11/33, Yff, J. see Ujff

11/1/5,8: 11/612,5,10,11,55: 44,67:111/10/22: I1/5/56,57: Yntema, R.T. !11/9/25ii11/8/13,43: 111/4/31,32: V/5/18,48,57 Young, A.D. 11/1/14111/6/31: P1/7/3 Wilkinson, .J.H. 111/4/37: Young, D. 1/2/15

Walker, P.B. V/6/55 111/4S/27,36: 111/6/19,34 Young, J.P. 111/'S/61,62Walker, R.W. 111/75/80 Wille, R. 111/4S/13 Young, M.1. 111/10(21,22Walsh, J. B1/5/15,57 Williams, D. 1/2/ 16: 111/7S/94:Walshe, DE.EJ. V/5/23,58 P1/1/27,28: V/1/12: V/3/37: Zartarian, G. 11/2/45:Walter, F. V/3/25,29,36 V/4/16 11/5/10,15,57: 11/9/37,Walters, R.E. V/ I/IlI Williams, D.E. Il/Chapter 3: 54,56,57: 11/10/20,25:Walton, W.C. Jr. 1/8/30: 11/3/16,37,41,42: 11/7/75 111/7/8,41: 111/7S/60

P1/1/29 Williams, J. 11/1/126: V/3/35 Zeydel, E.F.E. 111/7/23,24,47:Waner, P.G. 1/2/16 WfiliamsW.C. V/I/Il 111/7S/ 10,64,69,73,76,77,8 1,Wang, C.Y. 11/9/53,66 Wilson, E.B. 11/1/4 84,85Wang, P.K. 11117S/82,94 Windsor, E.P.L. P1/7/27: Zimmermann, N.Hi.Warburton, G.B. 1/2/17 P1/8/13 111/7S/64,79Ward, G.N. 11/4/82,86,120: Winson, J. 1/4/49: V/4/21I Zisfemn, M.B. 1II/7S/64

11/7/12,74 Wirtz, R.A. 11/9/2,55 Zlotnick, M. 111/2/57,58Ward, J.F. IV/ 1/30: V/I /IlI Wittmeyer, H. V/3/28,36: Zrzywoblocki, M.Z. V/5/57Wasserman, L.S. 11/ 10/20: V/5/55 Zvara, J. 111/10/21

P1/Chapter 7: IV/7/26: Wolfe, M.O.W. P1/Chapter 10: Zwaan, R.J. 111/9/19,25:IV/Chapter 8: V/3/36 IV/ 10/28 VI/Tables and Graphs

Watkins, C.E. 11/1/21,22.,42, Woodcock, D.L. 1/Chapter 6:43: 11/4/119:11I/Chapter 5: 1/6/51,55: lI/Chapter 7:11/5/57,58,59: 11/10/53,55, 11/9/3,33,38: 11/10/54:59: 111/2/57: IV/1/29.: IT/I1/ 19,67: VI/TG/5,9

V/5/55

41

23

MANUAL ON AEROELASTlCrYF

VOLUME I INTODUCTORY SURVEY

PART ISTRUCTURAL ASPECTS

VOLUME H PAR1 UAERtODYNAMIC ASPECTS

VOLUME III PART IllPREICMlN OF AEROELASTIC PHENOMENA

VOLUME IV PART IVEXERI*EENTAL METlIODS

VOLUME V PART VFACTUAL INFORMATION ON FLUrFER CHARACTERISTCS

VOLUME VI PART VICDLLEjCTED TABLES AND GRAPHS

General EditorRjdazet

CONTENTS OF VOLUME I

W.J.Dunican Introductory Survy Aug. 1959*

PART I - STRUCTURAL ASPECTS

QHAP`TET I W.S.Hemp, Analytical Representation of the Aug.1959Deformation of Structures

CHAFFE 2 J.M.Hedgepeth Vibration Analysis of Aircraft Aug. 1959Structures

CHAFF7ER 3 B.M.FraeUs de, Influence of Internal Damping on Nov. 1959Veubeke Aircraft Resonance

CHAFFER 4 ONERA Staff Theory of Ground Vibration Tesftig May 1960

CHAPTER S D.Benun The Influence of Powered Controls Aug.1959

CHAFFER 6 D.L-Woodcock Structural Non-Linearities Apr. 1960

CHAPTER 7 B.A.Bokey Thennoelasticity Feb. 1968(A reytron of the orignal chapter by R. L.Bw5plinghoff, Aug. 1959)

CHAMFR 8 H.N.Abramnson Liquid Propellant Dynamics Dec. 1967

CONTENTS OF VOLUME B

PART 11I- AERODYNAMIC ASPECTS

CHAFFER I I.E.Garrick General Introduction Sune 1960

CHAPTER 2 A.I. van der Vooren Two-Dimensional Linearized Theory July 1960

*The dates given relate to the acceptance of the manuscript by AGARD

24

CHIAPER 3 D.E.Williams " "ym l Sohmemic Theory Jan.1961

CHAPTER 4 D.E.Davies "r "tAh mi Sonic Theory Nov.1960

CHAFFER 5 C.E.Watkins "mr. "Dimensinl Supermonic Theory Nov.1960

CHAPTER 6 H.Lomax Indicial Aerodynami Nov.1960

CHAPTER 7 D.L.Woodcock Sleader-Body Theory Apr.1962Revision Nov.1967

CHAPTER 8 H.G.Kwssner Non-Stationay Theory of Airfoils of FiniteThickness in Inoompeseule Flow Dec.1960

CHAPTER 9 M.T.Landahl and Thickness and BoundaryLayer Effects Mar.1%9H.Ashley

(A revision of the original chapter by H.Ashley and G.Zartawin, Nov.1960)

CHAPTER 10 W.E.A.Acum The Comparion of Theory and Experiment May 1962for Oscilating Wmins

CHAFFER I I P.R.Guyett Empirical Values of Derivatives Mar.1961

CONTENTS OF VOLUME [H

PART ll - PREDICTION OF AEROELASTIC PHENOMENA

CHAPTER I E.G.Broadbent An Introduction to the Prediction ofAeroelastic Phenomena Feb.1963Revision Sep. 1967

CHAPTER 2 F.W.Diederich Divergence and Related Static Nov.1963Aeroelastic Phenomena

CHAFFER 3 F.W.Diederich Low of Control Aug.1964

CHAPTER 4 E.G.Broadbent Flutter and Response Calculations inPractice Apr.1963Revision Sep. 1967

Supplemet H.G.Kfissner Flutter Calculations as Automaticto CHAPTER 4 Processes Nov.1967

CHAPTER 5 J.C.A.Baldock and Diagnosis and Cure of Flutter Troubles Apr.1962LT.Niblett

CHAFFER 6 A.I. van der Vooren General Dynamic Stability of Systems Nov. 1961with Many Degrees of Freedom

CHAPTER 7 Y.C.B.Fung A Summary of the Theories andExperiments on Panel Flutter Feb. 1961

Supplement D.J.Johns A Panel Flutter Review May 1969to CHAPTER 7

CHAPTER 8 H.Lazennec The Effect of Structural Deformation onthe Behaviour in Flight of a Servo-Controlin Association with an Automatic Pilot July 1968

CHAPTER 9 W.H.Reed Propeller-Rotor Whirl Flutter Sep.1967

CHAPTER 10 N.D.Ham Helicopter Blade Flutter Sep.1967

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25

PART IV - EXPURIMEPITAL, METBODS

CHAPTER I DJ.Martin and Measuremet Of Structural Inf1uenceT.Lauten Caefficieuts Oct. 196

CHAPTER 2 R.C.Lewis and Ground Resonace TestingD.L.Wrisley Dec.1961

CHAPTER 3 H.Gauzy Measurwement of Inertia and Structural Feb.1961Dampin#

WHAPTER 4 J.C.Hall Experimental Technique. for theMeuuement, of Power CountrolImpedance June 1964

WHAPTER S J.B.Bratt Wind Tunnel Techn*u= for theMeasuremuent of Oscillatory Derivaties Jan.I196

WHAITER6 C.Scruton and Skmilarty Requirements for FlutterN.C.Lambourne Model Testing Nov. 1960

WHAPTER 7 L.S.Wasserman and Model ConshmictionWJ.Mykytow Jan.1961

CHAPTER 8 L-S.Wassernan and Wind Tunnel Flutter TintsWJ.Mykytow Jan. 1961

CHAI'TER 9 W.G.Molyneux Rocket Sled, Ground-Launched Rocket andFree-Falling Bomb Facilities Jan. 1961

CHAITR 10 M.O.W.Wolfe and Flight Flutter TestsW.T.Kkkby Dec. 196

CONTENTS OF VOLUME V

PART v - FACTUAL INFORMATION ON FLUTTER cWARAcrERISTICS

CHAPTER 1 K.A.Fous Divergence and Reversal of Control Feb.1960

HAFIER 2 D.R.Gaukroger Whig Flutter Feb.1960

CHAPTER 3 A.A.Regier Flutter of Control Surfaces and Tabs Feb. 1960

CHIAPTER 4 A.D.N.Smith Flutter of Powered Controls and ofAll-Mowing Tailplanes Apr. 1960

WHAFTER S N.C.Lambourne Flutter in One Degre of Freedom Aug. 1960Revision Feb.1968

CHAFFTER 6 W.G.Molyneux Approximate Formulae for FlutterPrediction Apr.1960

CONTENTS OF VOLUME VI

PART VI - COLLECTED TABLES AND GRAPHS

A.L. van der Vooren The Theodorsen Circulation Function.Aerodynamic Coefficients Jan.1964