NAVWEPS 00-8OT-80  INDEX  Psge  !a”ding gear configuration stability.  ...........  305  landing performance.  ......  ...  ....  ...  192  factors affecting performance.  ....  ...........  196  lateral co”trol,  ...............................  300  lateral stability.  .......................  ....  294  lift  characteristics.  ...........................  24  coefficient  ..................................  23  equation ...................................  23  generation  ..  ............  ............  ...  16, 63  lift-drag ratio. ...............................  32  limit load. .................................  326  linespeeds ...................................  394  load factor  ................................  37, 331  load spectrum. .............  _  .................  328  longitudinal  control  ....................................  275  dynamic stability. ..........................  279  static stability. ...........................  250  Mach number  definition.  ..................................  202  critical Mach “umber. ......................  2!5  maneuvering load factor  .....................  331  maneuvering performance.  ........  ...........  176  maneuvering stability.  ......................  268  mean aerodynamic chord, MAC.  .............  63  mirror landing system  .........................  358  normal shock wave. ..........................  207  obliqueshockwave  ..........................  207  operating limitations  propellers,  .....................  ....  148  reciproczring c  ...  ..................  144  turbojet  ...................................  124  .. turboprop. ...............................  133  Operating Strength Limitations, Chapter V.  ....  325  overstress,  effect  on service  life.  ................  344  parasite area, equivalent. ....  ..............  89  parasitedrag  .................................  87  performance,  Airplane Performance,  Chapter II.  95  pilot induced oscillarion.  .....................  314  pitching moment  airfoil.  ....................................  47  longitudinal. ..................  ........  249, 251  pitch-up  .....................................  313  pitot-static system.  ...............  ...........  9  planform effects.  .............................  61  power effects  on stability. .....................  259  power off stability  ...  ........................  259  power required. ...................  ..........  96  power settling. ...................  ........  4c3  preignition,  ...........  ....  ....  140  pressure  altitude.  .........  ....  ...  ...  ..  4  pressure  distribution.  ..  .........  .....  14  endurance  Pwe  off-optimum. ..............................  172  performance.  ...............  ....  .........  170  specific  .................................  158, 170  engine failure  effect  on multiengine airplane.  ............  294, 376  power off glide performance.  ................  369  equilibrium conditions. .......................  150  equivalent airspeed,  EAT.  ....................  11  equivalent parasite area. ......................  89  equivalent shaft horsepower, ESHP.  ...........  133  expansionwave ..............................  211  factorofsafcty ...............................  326  fatigue considerations.  ........................  328  feathering and governing of propellers.  .........  148  flap  aerodynamic effects.  .......................  37, 43  typCS  ......................................  41  flutter .......................................  342  force divergence. .............................  218  friction  braking,  .............................  388  cocfficicnt. ................................  388  skin friction. ..............................  54  frost ........................................  373  fuel qualities. ................................  141  glide performance.  ...........................  369  governing apparatus, turbine engines.  ..........  121  governing and feathering of propellers.  .........  147  gusts and wind shear. ....................  ...  367  gust load factor. ...........................  332  groundeffect  .................................  379  heating, aerodynamic. ........................  242  helicopter, problems. .........................  399  helicopter stability and control.  .............  319  high lift  devices  ..  ......  ............  ...  ., .,  39  flight at high lift conditions  .................  35  High Speed  Aerodynamics,  Chapter III.  ........  201  humidity, effect  on power.  ....................  144  ice ..........................................  373  indicated airspeed,  IAS. .........  .............  10  induced  angle of attack. ...........................  66  drag. ....................................  66  drag coefficient.  ...........................  68  flow. .....................................  63  inertia coupling. ...................  .......  315  inlets, supersonic  powerplant.  .................  238  interference  between airplanes in flight.  ........  383  items of airplane performance.  .................  150  landing and ground loads. ....................  343  landing flare and touchdown,  .............  362  415 