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Comanche PA-24, 78
Navajo, PA-31, 52, 240
Twin Stinson (later Apache) PA-23, 49
Planeaux, J. B., 142
Platz, Reinhold, 7
Plum Tree test site, NASA, 136
Polhamus, Edward C., 142, 244–246
Poisson-Quinton, Phillipe, 354
Poisson’s equations, 260
Potts, David W., 319
Powers, Bruce G., 283, 284, 341
Prandtl-Glauert rule, 93, 97, 162
Prandtl, Ludwig, 92
Pratt, R. W., 18
Princeton University, 31, 36, 38, 193, 227, 242
principal axis inclination instability, 181
propeller tilt, 46, 47
propulsion-controlled aircraft (PCA), 314, 316
propeller forces in yaw, 52, 53
Pugatchov, Viktor, 157
Pugsley, Sir Alfred G., 290
Purser, Paul E., 219, 220
q-springs (artificial feel), 82
QUADPAN program, 97
quaternions, 258–262
Questar Venture, 136
Rae, William J., 14
Rahn, Robert O., xix, 101, 175
rapid rolls to steep turns, 155–157
Rayleigh, Lord, 162
recording instruments, NACA, 20, 21
Rediess, Herman A., 279
redundant hydraulic controls, 83–89
redundancy, analytic and physical, 88, 89
Reed, R. Dale, 223
Reeder, John P., 55
reference axes
body axes, 267–270
hybrid axes, 269, 270
principal axes, 269
stability axes, 269
wind axes, 268, 269
wind-tunnel stability axes, 269, 270
Regan, Frank J., 183, 184, 273
Regis, Edward, 240
Reid, Henry, J. E., 20
Reid, Lloyd D., 16, 17, 354
Reissner, Hans, 11
Relf, E. F., 13, 16, 53, 129, 354
Renier, O., 130
Republic Aircraft
P-47 Thunderbolt, 165–167, 289
F-84F Thunderstreak, 178, 189, 288
XF-12, 74, 75
Research and Technology Organization (RTO), 18
restructurable controls, 321
reverse dihedral due to slipstreams, 52
reverse rigging, 79
Rhoads, Donald W., 112
Rhode, Richard V., 166
Ribner, Herbert S., 53, 354
atmospheric turbulence models, 278
propeller side force theory, 52, 53
jet air intake forces, 53
Ringland, Robert F., 187, 191, 192
Ritchie, Perry, 166, 167
Robbins, Robert, 306
Robinson, A. C., 260
Rockwell Corporation,
Aero Commander, 49, 127
B-1, 37, 38, 310
HIMAT, 281
Space Shuttle Orbiter, 36, 37, 86, 154, 155, 229,
269, 283, 324, 325, 341
X-15, 37
Rockwell/MBB X-31, 145, 160, 317, 321
Rodden, William P., xix, 354
arbitrary origin of body axes, 284
dihedral effect on flexible wing, 295–297
mean and structural axes, 299
MSC/NASTRAN, 298
unsteady aerodynamics, 159
Rodrick, W. E. B., 200
Rogallo, Frank, 199
Rogers, Kenneth, 159
Rolf, J. M., 17
rolling pullouts, 112
roll rate capability, 27–29, 146–148
roll rate requirements, missile-armed fighters, 148
roll-to-yaw ratio, 37
Root, L. Eugene, 66, 67, 77, 92, 354
root locus (Evans) method, 270, 308–310
Roskam, Jan, xviii, xix, 16, 17, 253, 354
Ross, A. Jean, xviii, 16, 141, 354
Rossito, K. F., 153
rotary derivatives, 10, 266, 267
Routh’s criterion for stability, 118, 137, 267
Royal Aeronautical Society, 18
Royal Aircraft Establishment (RAE) (now DERA),
36, 41, 125, 141, 142, 190
Royal Aircraft Factory S.E.-5, 7, 8, 264
© 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
388 Index
Rubbert, P. E., 95, 297
rudder deflection to coordinate maneuvers, 155–157
rudder lock, 220, 224
Boeing KC-135, 222
Boeing Model, 307, 221
Boeing Model, 707, 222
Douglas DC-3, 221, 222
explained, 221
Waco CG-4A, 224
Waco CG-13, 224
rudder pedal forces, engine dead, 47–49
rudder snaking oscillation, 66, 67
Rudlicki, Georges, 217
Russell, John M., 18
Rutan, Dick, 257
Rutan, Elbert L. (Burt), 91, 252, 257
Rutowski, Edward S., xix
Ryan FR-1 Fireball, 35
Saab, JA-39, 86, 87
Sachs, Gottfried, 182
Saegesser, Lee D., xix
safe maneuver limits, 119
safe personal aircraft, 231–243
Schaefer, W. S., 88
Schaeffer, Harry, 289
Schairer, George S., xix, 30, 61, 67, 221, 355
Schaufele, Roger D., xix, 74
Schelhorn, Arno E., xix
Scher, Stanley H., 124–126
Scheubel, F. N., 182, 183
Schiff, Barry, 49
Schiff, L. B., 130, 142, 161, 283, 284
Schilling, Lawrence J., xix, 279
Schlaff, Bernard A., 189
Schmid, L., 81
Schmidt, David K., 300, 328
　
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