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