RESULTS OF A FORCE TEST OF FOUR CONFIGURATIONS OF THE HI-LO INSTRUMENTED AND CHAFF ROCKETS IN THE SANDIA CORPORATION 12 X 12 INCH TRANSONIC WIND TUNNEL (PROGRAM III-46)
Technical Report
·
OSTI ID:4228703
Wind-tunnel festing of the Hi-Lo Test Vehicle was conducted through the transonic and supersonic Mach number ranges in a 12 x 12 in. transonic facility and a 20-in. supersonic wind tunnel. Complete results of the tests in the transonic range are presented. A short correlation study of the data obtained in both wind tunnels is also made. All configurations were statically stable throughout the Mach number range. The static stability of all configurations is lowest at the supersonic Mach numbers. Comparison of the 12-in. transonic tunnel force and stability data with the supersonic data indicates excellent correlation. (auth)
- Research Organization:
- Sandia Corp., Albuquerque, N. Mex.
- NSA Number:
- NSA-14-001597
- OSTI ID:
- 4228703
- Report Number(s):
- SCTM-299-59(51)
- Country of Publication:
- United States
- Language:
- English
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