FLEXSTAB computer program is used to evaluate trim state, static, and dynamic stability characteristics, inertial and aerodynamic loading, and elastic deformations of aircraft configurations at subsonic and supersonic speeds.
Stability of an elastic airplane
NASA Tech Briefs ; 1 , 4
01.03.1977
Sonstige
Keine Angabe
Englisch
Stability characteristics of elastic airplane
NTRS | 1978
|Engineering Index Backfile | 1929
|Measuring the elastic airplane
Engineering Index Backfile | 1942
|