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 70-73
viscosity of fiuid, 2-5, 12
Von Doenhoff, A. E., 177-178
von K5rman. Theodore, 7-11
vortex asymmetry, 705-709
vortex breakdown, 678-686
     control of, 686
     effects of, 708-710
vortex flap, 677, 679
vortex flow, 676-677
vortex generuors, 53
vortex Jift, 54-55, 676-677
Vought F8V aircraft, 60
W
wake vortices, 34
wash-out circuit, 604
wave drag, 39, 47, 54, 58-59, 67-68
wetted surface,  I I
wind
    axes system, 322
    body axes system and, 328-330,
336-337
    effect on gliding, 76-78
   effect on range, 110-111
    ground run and, 150
wind axes system, 322
w:indshear, 156-158
wing camber, 207-208
wing dihedral, 261-266, 293-297, 305
wing rock, 676, 695-710, 712-713
    active control of, 727-731
    forebody-induced, 714-725
INDEX
        suppression of, 725-73 I
wing sweep, 47-52, 298-299
wingtips, 52-53
wing unhedral, 265
wing vortex flow fields, 693-695
wing-lift carryover body, 192-193
winglets, 31-32
wings
   aerodynamic center, 173-174, 189-191
    aerodynamic characteristics of, 17-26
     aspect-ratio, 45, 46
    autoroWion of, 640-641
    configunUion of: 296
     dclta, 54-55, 676-686
      firute, 26-3 1, 39
     fuselage and, 1.70-171, 295-296
    high-litt devices, 23-26
   leading edge, 171-173
      litt-curvc slopeJ 73-183
    modifications to, 664-666, 667
    normal-force curve slope, 173-179
    oblique, 58-59
    pitching moment and, 186-193
   planform parameters, 16-17
    section geometry, 12-13
   section parameters, 12-15
     spin and, 65 1-652
    stability and, 173-193, 261-277. 295-297,
         299-301 .
    stall of, 22-23
    swept-forward, 55-58
     tnuling edge,  171- L73
   see also swept-back wing aircraft
X
X-29 aircrafL 674, 696, 697, 727-731
X-31 aurcmft, 139, 674
X-36 aircraft, 749
Y
yaw, 259-260
yaw damper. 604-607
yaw departure, 676, 732-733
yaw divergence, 628-630
yaw rate, 413-4 J 6, 571-572,  604-607,
663-664
yawing moments. 265, 268-269, 281-283,
             411-412, 630
     angle of attack and, 690-693
    balance of, 659-661
Z
zone of action, 36
zone of silence, 36
Texts Published in the AIAA Education Series
Performance, Stability, Dynamics, and
Control ofAirplanes
Bandu N. Painadi                            1998
Spacecraft Mission Design,
  Second Edition
Charles D. Brown .                                1998
Computational Fluid Dynamics
Malcolm J. Abzug                                    1998
Space Vehicle Dynamics and Control
Bong Wie                        1998
Introduction to Aircraft Flight
Dynamics
Louis V Schmidt                        1998
Aerothermodynamics of Gas Turbine
and Rocket Propulsion,
  Third Edition
Advanced Dynamics
Shuh-Jing fing               1997
Introduction to Aeronautics:
A Design Perspective
Steuen A. Brandt, Ran,dall J. Stiles,
John J. Bertm, and Ray Whitford        1997
Introductory Aerodynamics and
　
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