INVISCID HYPERSONIC FLOW AROUND SPHERES WITH MASS INJECTION. Paper 9 of GENERAL RESEARCH IN FLIGHT SCIENCES, JANUARY 1959-JANUARY 1960. VOLUME I. FLUID MECHANICS. PART 1
Technical Report
·
OSTI ID:4166707
Lighthill's constant-density solution for the inviscid hypersonic flow around spheres is extended to include mass injection from the body. It is shown that the shocklayer thickness, injection-layer thickness and surfacepressure distribution depend only on the injection momentum, for fixed free-stream conditions. The dependence is shown graphically for the case when the injection layer is irrotational. (auth)
- Research Organization:
- Lockheed Aircraft Corp. Missiles and Space Div., Sunnyvale, Calif.
- NSA Number:
- NSA-14-019090
- OSTI ID:
- 4166707
- Report Number(s):
- LMSD-288139(Vol. I, Pt. 1)(pap
- Country of Publication:
- Country unknown/Code not available
- Language:
- English
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