Response of a Supersonic Turbulent Boundary Layer to Periodic Surface Roughness-Reference-Cited by-同舟云学术

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Response of a Supersonic Turbulent Boundary Layer to Periodic Surface Roughness

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Ekoto Isaac¹,Bowersox Rodney¹,Beutner Thomas²,Goss Larry³

Affiliation:

1. Texas A&M University

2. DARPA

3. Innovative Scientific Solutions Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1142

Reference45 articles.

1. 1Nikuradse,J."StromungsgesetzeinRauhenRohren,"ForschungArb.Ingenieurwesen,No.361,1933.

2. 2Corrsin,S.,andKistler,A."Free-StreamBoundariesofTurbulentFlow,"NACAReport1244,1955.

3. Rough wall turbulent boundary layers

4. A generalized correlation of roughness density effects on the turbulent boundary layer.

5. Calculation of a Turbulent Boundary Layer Downstream of a Small Step Change in Surface Roughness

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experiments on a smooth wall hypersonic boundary layer at Mach 6;Experiments in Fluids;2018-03-22

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