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fiap chord, 226
 flaps, 24-26, 50, 207-213
     hinge moment and, 220, 222
    srability and, 304-309
flat spin, 648-649, 663
tlattest glide, 75-77
flight
     climbing, 94-104
    gliding, 73-79
    level, 81-94
    vertical plane, 70-73
flight control sysrems, 57, 595-596
    see tDso closed-loop systems
flight phases, 592
fluid disturbances, 35-36
INDEX
fluid flow
    compressible, 35-36
    flow separation, 5~7, 9
    supersoruc speeds, 36-40
    theory of, 2-3
flying qualities
    lateral-directional, 594-595
    longitudinal, 593-594
   overview, 591-593
force equations, 364-372
forced response, 537
forebodies, 690-695
    actuated forebody strakes, 740-743
    blowing, 725-729, 744-746
    geometry effect, 692-693, 715-717
    induced wing rock, 714-725
    Reynolds number and, 692
     sucLion, 746-748 .
    vortex control, 739-746
    wing rock and, 695-700
     wing vortex flow fields and, 693-695
Forward Swept Wing (FSW) Technology
           Demonstrator aircraft, 56
free flight, 389
 free response. 537-540
free-to-roll delta wings, 7001-701, 711
French Rafale, 674, 689
frequency response, 456-458, 562-564,
  565
frequency-domain techniques, 484-486
fuel consumption, 68, 108~109
full-state feedback, 599-604
full-state observer, 522
fuselage
    autorotation of, 641-645
   interference effects, l74
   modifications to, 666-668
   srability and, J69-I73, 183-193,
               270-272, 295
    wings and, 170-171, 295-296
G
 gain margin, 481-483
glide angle, 152-153
 glide nuio, 76
 gliders, 73-78, 122, 134-136
 ground, effect on stability, 215, 216. 217
ground run
     crosswinds and, 281
      landing, .t53- 154
   takeoff, 146-149
Grumman X-29 aircraft, 55-57
gyroscopes, 656-659
H
headwinds, 110-11 1, 150
Heinkel l62 aircraft, 627-628
Helmholtz theorem, 27
Herbst maneuver, 122, 139, 674
Herbst, Wolfgang, t 39
HFB 320 Hansa aircraft, 55, 56
761
762
high angles of attack
    control phases, 735-749
    control problems, 695-696
     delta wings and, 676-686                         .
    departure criteria application, 733-735
    forebodies and, 690-695
    forebody suction, 746, 748        .
    forebody voriex control, 739-746
    high-alpha problems and, 674-676
     bistory, 673-674, 675
    pitch-down, 737-739
    pitch up, 735-736
    roll damping and, 727-731
    thrust vector control, 746-749
     velocity vector rolI, 736-737
High Incidence Research Model (HIRM),
           746, 748
hinge moment, 217-224, 283-284
HIRM. see High Jncidence Research Model
    (HIRM)  '
hodograph, 96-97
horizontal plane
    disturbance in, 258-260
     turrung flight in, 123-134, 254-256
horn balance, 219-220
horseshoe vorrex, 27
hydrodynamic theory of fiuids, 2-3
hysteresis, 696, 698, 700, 703. 709
I       .
imaginary axis. 470, 483
impulse function, 441-442
induced camber, 223, 227
induced drag, 12, 28-32, 50, 67-68
inertia coupling
    overview, 627-628
    pitch divergence, 628-630
    prevention of, 637-638
    yaw divergence, 628-630
inertial axes system, 320, 326-328
infrared devices, 158
interceptor aircraft, 673
internal balance, 219-220
　
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