A WIND TUNNEL INVESTIGATION OF THE DRAG CHARACTERISTICS OF VARIOUS DISC CONFIGURATIONS. (PROGRAM III-34)
Technical Report
·
OSTI ID:4265027
A wind tunnel force test was conducted in September 1958 at the Sandia Corporation 12 x 12 in. transonic wind tunnel. The drag characteristics of 18 disc configurations were determined. Drag coefficients were obtained over the Mach range from 0.5 to 1.33 at zero degrees angle of attack. The Reynolds number varied from 0.45 x 10/sup 6/ to 1.99 x 10/sup 6/, based on maximum model diameter. (auth)
- Research Organization:
- Sandia corp., Albuquerque, N. Mex.
- NSA Number:
- NSA-13-012786
- OSTI ID:
- 4265027
- Report Number(s):
- SCTM-113-59(51)
- Country of Publication:
- United States
- Language:
- English
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