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Trouncer, J., 54
Tsien, H. S., 162
Tupolev Tu-54M, 173
turn coordinator, 241
Turner, L. I., Jr., 212, 213
Turner, W. N., 27, 28
Uddenberg, R. C., 112, 118
ultralight airplanes stability and control, 198–204
canard tilt, 200, 202, 203
longitudinal divergence, 202
opposite wing warp, 202, 203
scaling laws to conventional airplanes, 204
turning difficulties, 200, 202, 203
United Aircraft Research Department wind tunnel, 50
University of California, Los Angeles (UCLA), xix,
308
University of Southern California (USC), xix
University of Toronto, 159
Upson, Ralph G., 231, 233, 236
variable-sweep, 244–251
rotation and translation, 244
rotation only, 244, 245
variable-sweep airplanes
Bell X-5, 244
General Dynamics F-111 Aardvark, 245, 246
Grumman XF10F-1 Jaguar, 244
Grumman F-14 Tomcat, 246
Messerschmitt P.1101, 244
MiG-23 Flogger, 251
MiG-27, 251
Panavia Tornado, 251
Rockwell B-1, 246, 247
Sukhoi Su-17, 251
Sukhoi Su-24, 251
Tu-160 Blackjack, 251
Tu-22M Backfire, 251
variable-stability airplanes, 33–39
as trainers, 36
future of, 37–39
invention of, 35, 36
Learjet Model, 24, 36
NT-33, 37, 311
pilot cues in, 38
Princeton VRA, 36, 38
USAF/Calspan B-26, 36
USAF/Calspan TIFS, 36, 37
VISTA/F-16D, 39, 40
vector forms of the equations of motion, 274, 275
vee-tails, 217–219, 240
avoiding transonic pitchup, 218
design method, 219, 220
effect of stalling, 218, 219, 240
Vepa, R., 159
Verdin, James, 209
vertical wind tunnels (spin testing), 121–124
very large airplane problems, 341–344
control power requirements, reduced stability case,
343
delayed altitude response, 342
engine-out directional control, 341
phugoid and short-period frequencies, 342, 343
short tail lengths, folding wing designs, 341
time to bank requirements, 344
Vetter, Hans C., 55, 56, 102, 103
Vickers-Armstrong Aircraft, 251
Vietnam War, 1964–1973, 148
Vincenti, Walter C., xviii, 19, 24, 28
Virginia Polytechnic Institute, 267
Vogt, Richard, 247
Voison, Gabriel and Charles, 3
von K´arm´an, Theodore, 18, 30, 162
vortex bursting, 142
vortex encounters, 279
vortex generators, 49, 50
invention of, 50
transonic pitchup, 174, 177–179
vortex lattice methods, 95, 97
vortex ring state, 41, 55
Vought, 23, 24, 280
A-7 Corsair II, 140
F7U Cutlass, 178, 189
F8U Crusader, 83, 178, 189, 193, 249, 250,
316, 320
V/STOL flying qualities, 39–41, 54, 55
Vultee Vengeance, 75
w- and w’-planes, 309
Waco XCG-3 glider, 64, 65
Walker, Joe, 112
Wallace, Arthur R., 93
Wallis, Barnes N., 244–246, 250, 251
Wanner, Jean-Claude L., xviii, 14, 356
© Cambridge University Press www.cambridge.org
Cambridge University Press
0521021286 - Airplane Stability and Control: A History of the Technologies That Made Aviation
Possible, Second Edition
Malcolm J. Abzug and E. Eugene Larrabee
Index
More information
Index 391
Warner, Edward P., 19–22, 231
Washington, University of, 13
Washizu, Kyuichiro, 13, 356
Wasiko, Richard J., 192, 193
Webb, George J., Jr., 195, 196
Weick, Fred C., 16, 78, 134, 215, 216, 233–235, 356
Weick W-1A, 233, 234
Weil, Joseph, 51, 115, 178
Weiselsberger, C., 212
Weisshaar, Terrence A., xix, 288
Weissman, Robert, 137, 138, 142
Wendt, Harold O., 76
Wenzinger, Carl J., 134
West Virginia University, 226
Westbrook, Charles B., xviii, 31, 34, 115, 128, 356
Wetmore, J. W., 212, 213
whirling arm tests, 267
Whitaker, Arnold, 305
Whitbeck, Richard F., 309, 320
White, Maurice D., 27, 29, 93, 189
White, Roland J. (Jim), 16, 27, 93, 189, 356
eddy-current yaw damper, 101–103
frequency response method, 305
inertial coupling in rolls, 112
quasirigid model, Boeing B-47, 300
springy tabs, 77
White, William L., 133
Whittaker, Phillip, 309
Whitten, James B., 79, 237, 239
Wilkie, Lloyd, 115
Wilson, George C., 195
wing leading-edge extensions (LEXs), 158
wind shears, 277
wind-tunnel tests
free-to-roll tests, 141
free-spinning tests, 121–124
MIT tests, 1915–16, 19
model oscillation, 266
NACA Stability Wind Tunnel, 266, 267
NASA Ames 40- by 80-Foot Wind Tunnel, 209
NASA Free-Flight Wind Tunnel, 250
powered models, 45
transonic throats, 169, 339
　
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