Numerical investigation of the impingement of an oblique shock on a flat plate-Reference-Cited by-同舟云学术

Numerical investigation of the impingement of an oblique shock on a flat plate

Published:1988-03 Issue:2 Volume:23 Page:123-125
ISSN:0042-9929
Container-title:Wärme- und Stoffübertragung
language:en
Short-container-title:Wärme- und Stoffübertragung

Author:

Mehta R. C.,Sastri V. M. K.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF01637135.pdf

Reference9 articles.

1. Sayano, S.: Heat transfer in shock wave-turbulent boundary layer interaction regions. Douglas Aircraft Co., Santa Monica, Rept. SM-42567, Nov. 1962

2. Haslett, R. A.; Kaufman, L. G.; Romanowski, R. F.; Urkowitz, M: Interference heating due to shock impingement. Air Force Flight Dynamics Lab., Wright-Patterson AFB, Ohio, AFF DL-TR-72-66, July 1972

3. Levin, V.; Fabish, T. J.: Thermal effects of shock wave turbulent boundary layer interaction at Mach number 3 and 5. North American Aviation, Downey, Calif., Rept. NA 62H-795, Nov. 1962

4. Magan, J. D.; Spurlin, C. J.: Investigation of flow field interference caused by shock impingement on a flat plate at Mach numbers of 6, 8 and 10. Arnold Engineering Development Center, Arnold AFB, Tenn., AEDC-TR-66-85, 1966

5. Johnson, C. B.; Kaufman, L. G.: Interference heating from interactions of shocks with turbulent boundary layers at Mach 6. NASA TN D-7649, Sept. 1974

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