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direction cosines, 258–261
directional stability, 93–95, 215–217, 253, 254
displays, 238–240
dive recovery flaps, 165
Doetsch, Hans K., 128
Doetsch, Karl-H., 13, 15, 274, 348
Doolittle, James H., 231, 241
dorsal fins, 221, 224
Douglas Company
AD-1 Skyraider, 47
A2D-1 Skyshark, 189, 295
A3D-1 Skywarrior, 100–103, 172, 291, 295
A4D-1, A-4 Skyhawk, 43, 82, 100, 101, 172,
205–209, 219
A-20 Havoc, 47–49
A-26 Invader, 36, 47–49, 97–99
B-19, 74, 75
C-17, 86, 209
C-54 Skymaster, 63, 74
C-74, 67
C-124 Globemaster, 75
C-133, 75
D-558-II Skyrocket, 177, 178, 181
DC-2, 66, 67
DC-3, 41–43, 172, 221, 222, 234
DC-4, DC-4E, 20, 72, 74, 80, 164, 221
DC-6, 61, 75
DC-7, 61, 76
DC-8, 61, 76, 174, 291, 297
DC-9, 76, 174, 209, 291
DC-10, 82, 88, 174, 291
© 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 381
F4D-1 Skyray, 100, 101, 118, 119, 127, 175,
189, 190, 195
Mark 7 bomb, 112
SBD-1 Dauntless, 27, 61
X-3 research airplane, 112
downbursts, 277, 279
downsprings, 77, 78, 234, 240
downwash due to power, 51
Doyle, J. C., 321
Drake, Douglas E., 193
Draper, Charles S., 111
Drinkwater, Fred J. III, 189, 191
Dryden Flight Research Center, NASA, 39, 137,
225, 226, 250, 251, 269, 283, 316, 317, 225,
295, 296
Dryden, Hugh L., 30, 162
Duncan, William J., 13, 15, 17, 262, 287, 349
Dunn, Orville R., xix, 74–77, 349
Durand, Tulvio S., 192, 193, 333
Durand, W. F., 17, 22, 182
Durham, Wayne C., 140
Dusto, Arthur R., 297
dyadic forms of the equations of motion, 274,
276
dynamic directional stability, 137, 138, 140
dynamic fuel slosh
baffles, 205
Boeing KC-135A, 206
Cessna T-37A, 206
Douglas A4D-1 fuselage tank, 205, 206
in launch vehicles (Saturn V), 207
Lockheed P-80C tip tanks, 205
pendulum analogy, 206, 207
EF 2000 Eurofighter, 39, 86, 318
Efremov, A. V., 349
elevator angle–airspeed gradient, 19, 21, 23, 27, 43
Elgerd, Olle I., 310
Eller, Bob, 138
Enevoldson, Einar K., 142, 144, 210, 238
engine-out control, 47–50, 343
English Electric
Canberra, 75
Lightning, 78, 81, 82, 178
equations of airplane motion
alternate axes sets, 267–270
arbitrary origin of body axes, 284
near-orbital flight, 282, 283
numerical integration, 263, 264, 280
Eulerian integration, 280
perturbation forms, 10, 262, 263
Runge-Kutta integration methods, 280, 281
steady-state solutions, 281, 282
trajectory (point mass) forms, 284
see also modes of airplane motion
equivalent system models, 33, 148–152
ERCO Ercoupe, 233, 235, 255
Ericson, Albert L., 164, 165
Ericson, G. E., 142
Ericsson, Lars E., 141, 158
Esnault-Pelterie, Robert, 3
Etheridge, J. D., 192
Etkin, Bernard, xviii, 15, 17, 83, 159, 182, 349
aeroelastically corrected derivatives, 298
on aeroelastic methods, 286, 299
near-orbital equations of motion, 183, 283
textbook, 17, 39
turbulence model, 277, 278
Euler angles, 258–262
Euler equations, for moments, 10
Euler, Leonhard, 9, 258–262
Euler parameters, 260–262
Evans, Walter R., 308, 309
Experimental Aircraft Programme (EAP), 39, 316
fabric-covered control surface bulge, 67
Farley, Harold C., Jr., 336
Farman, Henri, 3
Federal Aviation Administration (U.S.), 44, 49, 235,
241
FAR Part 21, 243
FAR Part 23, 243, 255
FAR Part 25, 57
FAR Part 61, 241
FAR Part 91, 236
FAR Part 103, 199, 200, 243
feeler ailerons (used with spoilers), 107, 108
Feeney, T. A., 81
Feistel, T. W., 134
Ferber, Ferdinand, 11
Ferree, William M., 239, 240
Field, Edmund J., 153
Finn, E., 125
Fischenberg, D., 159, 226, 278
Flanders, James, 115, 118
flap-type control surfaces, invention of, 3
Flax, Alexander H., 290
Flettner, Anton, 4
FLEXSTAB program, 297, 299
flight director displays, 239, 240
floating main wings, 240
floating rudders, 47–49, 67
Florida University of, 14
fly-by-wire systems, 82, 86, 312
safety issues, 87–89
fly-by-light systems, 89
flying qualities, xvii, 19–44, 324–373
flying quality requirements, 22, 30, 41–43, 146–148
　
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