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thrust response time, 189, 191
Naval Weapons Center, China Lake, 103, 104
Navy Bureau of Aeronautics, 27, 47
Neal, T. Peter, 149, 330, 331
needle, ball, and airspeed, 241
Neihouse, Anshal I., 124–126, 255
Nelson, D. C., 145
Nelson, Robert C., 17, 141, 161
Nerkin, Albert I., 65
Neumark, Stefan, 182, 188, 272, 353
neutral point, 54, 91 (definition), 202, 300
Newman, Brett, 302
Newsom, J. R., 321
New York, State University of, 14
New York University, 13
Newell, F. D., 272
Newton, Sir Isaac, 9, 276
Nguyen, Luat T., 142, 144, 161, 210, 353
Nickel, Paul, 112, 113
North American
A-26, 165
AT-6, SNJ Texan, 21, 47, 172, 313
B-25 Mitchell, 47–49
F-86 Sabre, 87, 172, 175–177, 219
F-100 Super Sabre, 78, 112–115, 175, 178–180,
189, 190, 209
FJ-1, FJ-3 Fury, 100, 189
P-51 Mustang, 67, 69, 73, 74, 82, 92, 146, 147,
167, 168
X-15, 35, 186
XB-70 Valkyrie, 180, 182, 185, 279
North Wales, University of, 13
Northrop Corporation
B-2 Stealth Bomber, 35, 37, 86, 255, 269, 283,
297, 300
F-5, 141
F-89, 288, 308
HL-10 lifting body, 229
Large Amplitude Simulator, 280
N9M, 81
P-61 Black Widow, 71
X-4, 178
XB-35, 81, 82
YB-49, 81, 82, 86, 313
YF-17, 141, 300
Northrop, John K., 30
Norton, Frederick H., 17–21
notch filtering, 300, 301
numerator time constant requirements, 150
oblique wings, 247–251
AD-1 flight tests, 251
inertial rolling and yawing moments, 247
Stanford University flying model, 251
trailing-edge controls, 248
untrimmed moments and side force, 250
wing torsional divergence, 248
offset centers of gravity and fins, 51, 52
O’Hara, J. C., 112
Oliveri, Frank, 339, 340
Olmstead, Stanley, 74
ONERA, France, 130, 142
Ormerod, Albert O., 267
Ormiston, Robert A., 199
Osder, Stephen, xix, 16, 83, 84, 88, 89, 319,
353
Oswald, W. Bailey, 30
Packard-Le Pere LUSAC-11, 20
Padfield, Gareth, xviii
Pai, S. I., 288, 293, 294
Pamadi, B., 18
PAN AIR program (Boeing), 97
Parke, Darrel, 115
Paris, A. C., 226
Parsons, Thomas, 115
Patton, James M., Jr., 126, 134
Patton, Phil, 257
Paulson, John W., 137, 138, 142
Pavelka, Jerry, 115
Pawsey, G. L., 267
pb/2V lateral control criterion, 27, 28, 65, 146
Pedriero, N., 161
P´enaud, Alphonse, 1, 9
Pengelly, C. Desmond, 79
Pepoon, Philip W., 124, 126
Perkins, Courtland D., xviii, 16, 17, 274, 353
on B-47 roll reversal, 290
P-47 dive difficulties, 166, 167
textbook, 17
Perrin, W. G., 4, 57
Pfafman, Edward, 306
phase stabilization, 300, 301
Phelan, D. J., 189
photo recorder, Wright Field, 21
Phillips, W. F., 260, 274
Phillips, W. Hewitt, xviii, 16, 133, 288, 295, 353
altitude response, 342
inertial coupling in rolls, 109–113, 115, 117,
101–106, 109, 111, 113
on automatic pilots, 304
on Bryan’s stability derivatives, 10
on canard stalls, 252
on electronic control systems, 34, 35
on Gilruth/Gates maneuverability criteria, 28
on Maxim’s machine, 2
on pilot-induced osillations, 325
on power effects, 42, 45, 52
on transonic flight problems, 178
on variable-stability airplanes, 38
on wing-flow method, 168, 169
spring tabs, 75
wing leveler, 237, 239
Piaggio, P.180 Avanti, 253
Pickett, Marlin D., 279
© 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 387
pilot-induced oscillations, 87, 148
categories, 328–330
C-17, 87
Vought/NASA F-8, 330
F-86, 87
F-111, 330
modern transport airplanes, 333
NT-33, 329
Rutan Voyager, 318
Space Shuttle Orbiter Enterprise, 324, 325
YF-12, 330
pilot-in-the-loop analysis methods, 87, 148
algorithmic model, 326, 327
bandwidth-phase delay criteria, 331, 332
compensatory operation, 326–328
crossover model, 327
Neal-Smith approach, 330, 331
simple gain models, 327, 332
Smith-Geddes criterion frequency, 331
structural model, 326
pilot ratings, 33, 34
pilot work load studies, 238–340
Pinsker, Werner J. G., 112, 118, 138, 142, 274, 354
Piper Aircraft
Arrow, PA-28R, 78, 133, 135
Cherokee, PA-28, 78
Cheyenne, PA-31T, 240
　
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