曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

   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
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL4(114)