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Schmidt, L. V., 18
Schmidt, Stanley F., 115, 118
Schmitt, V. R., 83
Schmued, Edgar, 30
Schroeder, R. W., 20, 231
Schuler, John M., 112
Schy, Albert A., 120, 207
Scudder, N. A., 121
Seanor, B. A., 226
Sears, Richard I, 58, 59
Sears, William R., 81, 288, 292, 294
Seckel, Edward, 17, 112, 193
Seidman, Oscar, 124
separation of linearized equations, 262, 263
Shafer, Mary F., 39, 226
Shanks, G. T., 41
Shaw, David E., 355
Shevell, Richard S., 174
Shields, E. R., 189
Shortal, Joseph A., 169, 171
side stick controls, 34, 57
sideslip and angle of attack conventions, 270
sideslip excursions in rolls, 155
sidewash, 94
Sikorsky, Igor, 5
Silver, Brent W., 257
Silverstein, Abe, 59, 61, 94
SIM2 computer program, NASA, 269, 270
single engine failure, 47–50
single pilot IFR operations, 242, 243
Sisk, T. R., 234, 236
Sitz, D. M., 145
Skoog, Richard B., 291, 292, 294
Skow, Andrew M., 142
Sleeman, William C., Jr., 51
slipstream effects, 45, 50–52
Sliwa, Steven M., 126, 134
Smelt, Ronald, 50
Smetana, Frederick O., 17, 243
Smith Aviation Trainer, 136
Smith, John W., 185
Smith, Rogers E., 330, 331
Smith, Terry D., 355
Society of Automotive Engineers (SAE), 18
Soderman, Paul T., 209, 211
Sohn, Ronald F., 128
Sopwith Camel, 7
Soreau, M. M., 11
Sorenson, Emil L., 167
Soul´e, Hartley A., 22–25, 30, 121, 355
SPAD (Societ´e Pour Avions D´eperdussin), 5
special airspeeds, multi engine, 49, 50
Sperry Company
A-12 autopilot, 82, 103, 313
“Stabilizer”, 304
Sperry, Elmer, Jr., 241
splitter-plate (tadpole) rudders, 219
spin recovery
NACA design rules for, 124–126, 133,
134, 346
piloting techniques, 101, 126–128
RAE design rules for, 125
spin research
computed motions, 123, 128–131
coning rotary balances, 129, 130
drop models, 121, 123, 136
equilibrium spin analysis, 129, 130
factors other than tail design, 126–128,
134–136, 346
forebody geometry, 140
free-spinning wind tunnels, 121–124, 133
nonlinear effects, 140
oscillatory rotary balances, 130, 131
pilot-in-the-loop considerations, 140
radio-controlled models, 136
remotely piloted models, 137
satisfactory recovery criterion, 123
systematic configuration variations, 124
spins, 131–137
characteristically incapable of spinning, 233
departure motions, 127–141
flat and steep, 121, 131–133
inadvertant, 49, 101, 235
oscillatory, post-stall gyrations, 127, 144
spin resistant, 233, 247
rotary derivatives, 128
spiral divergence, 9, 235–237, 272
spoiler ailerons, 43, 69–72, 107, 108, 233, 291
Spreeman, Kenneth P., 178
spring tabs, 4, 75–77, 107, 146
springy tabs, 77, 78
Squire, H. B., 54
Sri-Jayantha, M., 227
© 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 389
stability and control
at the design stage, 90–99
power effects, 46–56
teachers, 13, 14, 17
texts, 17, 18
stability and control estimation, drawings
bodies, 93
computer-aided design, 243
downwash and sidewash, 93–95
finite-element methods, 95, 97, 98, 297, 298
RAeS data sheets, 95
wings and tails, 91–93
wing–body interference, 93
USAF DATCOM, 95
stability and control estimation, wind-tunnel data, 97
stability and control myths, 44
stability augmentation, xvii, 66, 181, 303–323
adaptive systems, 320, 321
command augmentation systems, 33, 310–312
decoupled controls, 321
degree of authority, 310, 311
digital augmentation, 316
effect of valve friction, 303, 307
inappropriate applications, 240
kinematic coupling minimization, 120
Mach hold systems, 185
Mach trim compensators, 175, 176
mechanical devices, 101–103, 234
nonsynchronous sampling rates, 316
optimal designs, failed applications of, 319
rate-limited commands, 310
robust controllers, 320, 321
roll ratcheting, 311, 312
superaugmentation, 33, 312, 314
use required, 100, 181, 306, 336, 338, 340
wing levelers, 235–237
stability augmentation design methods, 270, 304, 305,
308–310, 316, 318
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