law of effectiveness, 349
Mach number effect, 280f
NACA airfoils, 267
sweep angle
on stall characteristics, 318
on structural loads, 318
wind-tunnel model, 451
Pitching moment
aerodynamic center, 104
airfoil at angles-of-attack, 256
airfoil’s pitching moments, 121–122
airfoils, 104
combinations, 378f
impact of ground effect on, 352f
Mach number effect on, 280f
modeling for simple wing-HT system, 466
NACA series airfoils, 268f
short-bubble leading edge stall, 252
stall effect types on, 123f
swept-back and straight wing configurations, 498f
wing partition method, 437–438
Pitching moment coefficient
compressibility effects, 278–280
estimation, 439–441
impact on longitudinal trim, 289
magnitude, 256
NACA five-digit airfoils, 261
three-dimensional ...
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