An experimental study of transonic shock/turbulent boundary layer interaction on a roughened surface
Author:
Affiliation:
1. Iowa State Univ., Ames
2. British Aerospace Airbus, Ltd., Filton, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-65
Reference20 articles.
1. Ilolden, M. S. "Studies of Boundary Layer Transitionand Surface RoughnessEffects in Hypersonic Flow," AFOSR Report 6430-A-5, Oct. 1983, Washington, DC.
2. Babinsky, H. "A Study of Roughness in Turbulent HypersonicBoundaryLayer,"Ph.D. Thesis,Cranfield University, United Kingdom, Dec. 1993.
3. Pearcy, H.H. "Shock-Induced Separationmid its Preventionby Design and Boundary layer Control," Vol.2, Pergamon Press, 1961, pp.1166-1345.
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