Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers /
Saved in:
| Main Author: | |
|---|---|
| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington : Springfield, Va. :
U.S. National Aeronautics and Space Administration ; For sale by the National Technical Information Service,
1976.
|
| Series: | NASA technical memorandum ; NASA TM X-3376
|
| Subjects: |