Semiempirical Method for Estimating the Rolling Moment Due to Yawing of Airplanes
1949
31 pages
Report
No indication
English
Aerodynamics , Yaw , Aircraft , Roll , Tail assemblies , Moments , Aspect ratio , Sweptback wings , Aq m00-10-3380
Semiempirical method for estimating rolling moment due to yawing of airplanes
Engineering Index Backfile | 1949
|Combined pitching and yawing motion of airplanes
NTRS | 1931
|Combined pitching and yawing motion of airplanes
Engineering Index Backfile | 1931
|