Results of Force Tests of Doorknob Model in the Sandia Corporation 12-inch Transonic Wind Tunnel (Program III-20)
Technical Report
·
OSTI ID:10152238
- Organization 5142
Wind tunnel aerodynamic test results on Doorknob instrumentation missile for high altitude nuclear tests. Lift, drag, and pitching moment coefficients at nominal Mach Nos. of 0.7, 0.8, 0.9, 1.0, 1.1, 1.2, and 1.3.
- Research Organization:
- Sandia National Laboratories, Albuquerque, NM
- OSTI ID:
- 10152238
- Report Number(s):
- SC-TM-282-57(51); ALSNL199700001044; ON: DE98056819; CNN: AT-(29-1)-789
- Country of Publication:
- United States
- Language:
- English
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