曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
constant altitude and, 108, 110
constant velocity and, 108-109
jet aircraft, 107-109
overview} 106-107
propeller aircraft, l09-110
wind effect on, 110-111
reconnaissance aircraft, 106-107
reduced-state observer, 522
relaxed static stability (RSS), 205-206
rxsponse. see airplane response
Reynolds number
definition, 1
forebodies and, 692
transition, 7 I 9-723
vortex breakdown and, 685
roll angle, 695-696
roll attractor, 710-7 l3
roll coupling. see inertia coupling
roll damping, 727-731
rolI rate, 571-572, 590, 636-637, 73 I
roIJ reversal, 676, 732, 734
roll subsidence, 572-573, 576, 586-588
rolling moments. 304-309, 413-416, 657-659,
705, 712
root-locus method, 467-470, 487-488
roranng circular cylinder, 7 t 7-721
Routh's stability criterion, 463-465, 543, 552,
634-636
Royal Aircraft Establishment, U.K., 12, 157
RSS. see rclaxed static stability (RSS)
rudder, directional control, 279-285
rudder lock, 286-287
rudder-fixed directional stability, 279
rudder-free direaional stability, 283-285
Russian Su-35 aircraft, 689
S
SAAB 37 aircraft, 734-735
sailplanes, 76-78
SAS. see stability augmentation sysrem (SAS)
scale effects, 19
second-order systems, 447-452, 484-486
secondary vortex, 676
semifree flight, 389
service ceiling. 99-100
set-back hinge balance, 219
sharpest sustauned tum, 132, 146
shear stresses, ll-l2
shock waves, 37-39, 42, 44-47, 59
shock-boundary layer interaction, 42
short-period mode, 593-594
side force, 404, 413
sideslip, 137, 4 L7, 570, 572, 590
angle of attack and, 695-696
effect on delta wings, 710
full-state feedback control, 607-611
LEX and, 690
roll attractor and, 7 L2, 713
spin and, 651-653
stability and, 258-260, 294-296
turning tlight and, 125
vortex breakdown and, 682-684
sink nUe, 76-77
sinusoidal response, 456-457
skin firiction, 11, 47, 67-68, 196-197
slot btowing, 746, 747
Space Shuttle orbiter, 73
specific excess power, 100-103
speed, level flight, 86-90
spin, 636-637. 646-649, 673
balance of forces in, 654-655
balance of moments, 655-663
departure criteria application, 733-735
resisrance improvement, 664-668
sideslip in, 65 1-653 .
steady-state, 649-654
steep, 648-649
spin recovery, 281-283, 663-664, 665
INDEX
spin-chute, 663
spiral mode, 575-576. 587-588, 595, 646-647
spoilers, 307, 308
stability
axes system, 321-322
closed-loap systems,.461-465
derivatives, 390-403
effect on longitudinal response, 551-557
maneuvers and, 248-256
Nyquist stability criterion, 473-478 .
overview, 165-168
Routh's stability criterion, 463-465, 543,
552, 634-636
see also directiona~ stability; lateral stability;
longitudinal stability
stability augmentation system (SAS), 537,
599-604, 607-611, 731
stability axes system, 321-322
stability derivatives
lateral-directional, 404-420
longitudinal, 390-403
overview, 389-390
stagnation points, 2-3, 6, 12 .
stall, 52-54, 646-649, 738-739
delta wings and, 678-686
wing sections, 22-23
stare observer, 522-525
state-space analysis
controllability, 512-513
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL4(114)
