α-EFFECTS ARE NEGLIGIBLE IN HYPERSONIC UNSTEADY AERODYNAMICS—FACT OR FICTION?

Author:

ERICSSON L.E.

Publisher

Elsevier

Reference19 articles.

1. Hypersonic Flow Theory;HAYES,1959

2. Comparison of Static Pressures on Flared Bases in Non-Uniform Hypersonic Flow as Calculated by Exact and Approximate Methods;FINK;J. Aero. Sci.,1962

3. Free-flight tests of a blunt-nosed flare-stabilized body at speeds to 8.2 km/sec;KIRK;J. Spacecraft and Rockets,1966

4. SEIFF, A., Secondary Flow-Fields Embedded in Hypersonic Shock Layers, NASA TND-1304 (May 1962)

5. KUEHN, D. M., Experimental and Theoretical Pressures on Blunt Cylinders for Equilibrium and Non-equilibrium Air at Hypersonic Speeds, NASA TND-1979(1963)

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Delta wing separation can dominate shuttle dynamics;2nd Atmospheric Flight Mechanics Conference;1972-08-16

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