O'Reilly logo

General Aviation Aircraft Design by Snorri Gudmundsson

Stay ahead with the world's most comprehensive technology and business learning platform.

With Safari, you learn the way you learn best. Get unlimited access to videos, live online training, learning paths, books, tutorials, and more.

Start Free Trial

No credit card required

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 ...

With Safari, you learn the way you learn best. Get unlimited access to videos, live online training, learning paths, books, interactive tutorials, and more.

Start Free Trial

No credit card required