Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /
| Main Author: | |
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| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
U.S. National Aeronautics and Space Administration ;
1976.
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| Series: | NASA technical memorandum ;
NASA TM X-3376. |
| Subjects: |
Evans: US Documents (Annex 5th floor)
| Call Number: |
NAS 1.15:X-3376 |
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|---|---|---|
| Call Number | Status | Get It |
| NAS 1.15:X-3376 | Available | |