Studies of shock/shock interaction on smooth and transpiration-cooled hemispherical nosetips in hypersonic flow-Reference-Cited by-同舟云学术

Studies of shock/shock interaction on smooth and transpiration-cooled hemispherical nosetips in hypersonic flow

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference
language:
Short-container-title:

Author:

HOLDEN M.¹,RODRIGUEZ K.¹,NOWAK R.²

Affiliation:

1. Calspan Corp., Buffalo, NY

2. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1765

Reference247 articles.

1. Edney, B. "Anomalous Heat Transfer and Pressure Distributions on BluntBodiesat Hypersonic Speeds in the Presence of an Impinging Shock," FFA Report 115, Aeronautical Research Institute of Sweden, 1968.

2. Holden, M.S., Moselle, J.R., Lee, J. Wieting, A.R., and Glass, C. "Studies of Aerothermal Loads Generated in Regions of ShocklShock Interaction in Hypersonic Flow," Revision to Final Report NAS1-17721 dated March 1990, April 1991.

3. Keyes, J.W. and Hains, F.D. "Analytical and Experimental Studies of Shock Interference Heating in Hypersonic Flow," NASA Report TND-7139, May 1973.

4. Shock/shock interference on a transpiration cooled hemispherical model

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