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Israel Lavi, 674, 689
J
jet aircraft
     climbing flight, 97-99, 101-102
      cruise altitude,  J II-I I3
       endurance of,  I 14-t 15
   ground run, 148
    Ievel flight, 85, 87-90
     power effects on, 200
    range, 107-109
    service ceiling, 100
     stability and, 278  .
    turning performance, 130-134
K
Karm5n vortices, 7-1 J, 692, 719
KC135 aerial-tanker aircraft, 31
INDEX
L
 laminar flow, 9-t 1, 12, 719-720
landing
     crosswinds and, 281-282
    hazards during, 156-158
    sequences of, l52-t53
 Laptace transform, 440-446
lateral control departure parameter (LCDP),
 732-735
 lateral stability
     control, 304-309
    elemenrs of, 294-295
     evaluation of, 295-304
     overview, 293-294
 lateral-directional response
     approximatians, 572-577
     frequency response, 588-591
     overview, 564-572
     transfer functions, 577-588
latend-directional stability augmentation
              system, 607-611
LCDP. see Iatexal control departure parameter
 (LCDP)
Iead/lag compensator, 492
Ieading edges. 23. 47-49
    corrcction factor, 178, 182-183
     shapes, 219-220
    wings, I71-I73
Ieading-edge extensions (LEX), 674, 686-690
level flighi, 81-94, 230-235
LEX..ue Ieading-edge extensions (LEX)
Lidar devices, 158
Iift, 6,  I 7-19, 42-43, 2 t I
lift-curve slope,  l73-t 86, 390. 396
liRing line theory, 26-31
lifting surface theories, 26-31
limit cycle oscillation, 705
linear systems
     Laplace r.ransform, 440-445
    overview, 439
Ioad factor. 126, 129-130, 133-134, 248-256
loiter, 106-107
Jongicudinal control, 206-213
longitudinal response
    frequency response. 562-564
    overview, 537-545
       short period approxinwian, 545-547
     static stability effect on, 551-. 557
    transfer function and. 557-562
longitudinal stability, 630
    aerodynamic balancing, 219-224
    analysis of, 200-201
     ccrUer of gravity and, 213-215
    fuselage conmibution to, 169-173
     ground effecrs of, 215, 2J 6, 217
      longitudinal control, 206-213
     neutral points in flight. 230, 231
    power effect on, t98-200
     stick force in, 230-235
    stick-fixed neutral poim, 20J-203, 230
    sOck-free, 215-218
stick-free margin, 228
stick-free neutral point and, 224-228, 230,
 231
    tail and, 194-198
        tail lift, 203-207
    trim tab, 228-230
    wing and, 173-183 '
   wing-fuselage and, 183-193
longitudinal stability derivatives, estimation of,
390-403
M
Mach cone. 36-37, 39, 47, 54
Mach numbers
      compressibility delay effects, 45-59
    definition, ;1-2
     freestream, 40-45
     vortex breakdown and, 685-686
 Mach wedge, 36
 magnitude crossover frequency, 590
 Magnus effect, 717-719
 major-loop compensation, 493-494
 Maneuver Technology Demonstrator, 674
maneuvers
    coning morion, 139
     horizontal plane, 254-256
     pitch-down, 737-739
    pitch-up, 735-736
     pull-out, 249-250
    pull-up, 248-254
     rolling, 628-637
     stability in, 248-256
    stick force gradient, 253-254
     stick-fixed, 251
     stick-free, 252-253
mapping, 473-478     .
　
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