Blunt body near-wake flow field at Mach 10-Reference-Cited by-同舟云学术

Blunt body near-wake flow field at Mach 10

Published:1997-01-06 Issue: Volume: Page:
ISSN:
Container-title:35th Aerospace Sciences Meeting and Exhibit
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Author:

Horvath Thomas¹,Hannemann Klaus²,Horvath Thomas¹,Hannemann Klaus²

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

2. DLR, Inst. fuer Stroemungsmechanik, Goettingen, Germany

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-986

Reference50 articles.

1. Heat transfer in supersonic separated flow over a two-dimensional backward-facing step

2. Numerical simulation of chemical and thermal nonequilibrium flows behind compression shocks

3. Numerical simulation of shock/shock and shock-wave/boundary-layer interactions in hypersonic flows

4. Cook, William J. (1970): Unsteady Heat Transfer Measurements to a Semi-Infinite Solid With Arbitrary Surface Temperature History andVariable Thermal Properties. Iowa State Univ. Tech Report ISU-ERIAMES-67500.

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