Large-Scale Roughness Influence on Turbulent Hypersonic Boundary Layers Approaching Compression Corners-Reference-Cited by-同舟云学术

Large-Scale Roughness Influence on Turbulent Hypersonic Boundary Layers Approaching Compression Corners

Published:1997-01 Issue:1 Volume:34 Page:70-75
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Babinsky H.¹,Edwards J. A.²

Affiliation:

1. Cranfield University, Craneld MK43 OAL, England, United Kingdom

2. Defence Research Agency, Fort Halstead, Sevenoaks TN14 7BP, England, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3174

Reference10 articles.

1. Turbulent boundary-layer characteristics over a flat-plate/wedge configuration at Mach 6

2. Babinsky, H. “A Study of Roughness in Turbulent Hypersonic Boundary-layers,” Ph.D. Thesis,College of Aeronautics, Cranfield Univ., Cranfield, England, UK,Dec. 1994.

3. Automatic liquid crystal thermography for transient heat transfer measurements in hypersonic flow

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