Prediction of hypersonic shock-wave/turbulent-boundary-layer interaction flows-Reference-Cited by-同舟云学术

Prediction of hypersonic shock-wave/turbulent-boundary-layer interaction flows

Published:1987-06-08 Issue: Volume: Page:
ISSN:
Container-title:19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference
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Author:

HORSTMAN C.¹

Affiliation:

1. NASA, Ames Research Center, Moffett Field, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1367

Reference17 articles.

1. 'Coleman, G. T. and Stollery,J. L. "Heat Transfer in Hypersonic Turbulent Separated Flow,'' 1'. C. Aero Report 12-05, Imperial College of Science and Technology, London,March 1912.

2. 'Coleman, G. T. "A Study of Hypersonic Boundary Layers over a Family of Axisymetric Bodies at Zero Incidence: Data Tabulation," I. C. Aero Report 13-06, Imperial College of Science and Technology, London, Sept. 1913.

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