RESEARCH IN HYPERSONICS AND MAGNETOHYDRODYNAMICS
Technical Report
·
OSTI ID:4030078
The hypersonic shock tunnel and the calibration shock tube are described, and their performance is discussed. The nonequilibrium character of expanding flows, hypersonic flow of low-density gas over cone models, and the electrical conductivity between electrodes in a moving plasma were studied experimentally. Nonequilibrium inviscid flows were also investigated theoretically. The studies are discussed in detail. (D.C.W.)
- Research Organization:
- Rensselaer Polytechnic Inst., Troy, N.Y.
- NSA Number:
- NSA-18-020119
- OSTI ID:
- 4030078
- Report Number(s):
- ARL-64-5
- Country of Publication:
- United States
- Language:
- English
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