Finite element analysis of critical stress distribution in canopy of deployed twin keel parawing, predicting failure stress levels
Structural analysis of a parawing during deployment
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AERODYNAMIC DECELERATION SYSTEMS CONFERENCE ; 1970 ; DAYTON, OH
01.09.1970
Aufsatz (Konferenz)
Keine Angabe
Englisch
Structural Analysis of a Parawing during Deployment
AIAA | 1972
|Structural analysis of a parawing during deployment
AIAA | 1970
|Engineering Index Backfile | 1963
|