The topics covered include the following: a test of a Space Shuttle model with various base enhancements intended to help reduce the drag of the Shuttle in the landing configuration; further tests conducted using a Shuttle model to explore base drag improvement techniques; testing of parafoils having different airfoil shapes and line lengths; a study of ground effects on a Shuttle model; and three dimensional velocity profiles in the wake aft of the Space Shuttle were determined to study the effects of wake velocities on the Orbiter drag chute.
Wind tunnel testing and research
1993-11-15
Report
Keine Angabe
Englisch
Wind Tunnel Testing and Research
NTIS | 1993
|SLUB | 1958
|SLUB | 1954
|Wind Tunnel Testing of a Common Research Model
AIAA | 2023
|Wind Tunnel Testing of a Common Research Model
TIBKAT | 2023
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