System of computer programs uses linear theories to evaluate static and dynamic stability, trim state, inertial, and aerodynamic loading, and elastic deformations of aircraft configurations at subsonic and supersonic speeds. Primary emphasis is on analysis of stability and control characteristics of flexible aircraft. System also solves simple rigid aerodynamic problems.
Stability characteristics of elastic airplane
NASA Tech Briefs ; 3 , 1
1978-06-01
Miscellaneous
No indication
English
Stability of an elastic airplane
NTRS | 1977
|Engineering Index Backfile | 1929
|Measuring the elastic airplane
Engineering Index Backfile | 1942
|Longitudinal stability characteristics of the LASTA airplane
Emerald Group Publishing | 2017
|