Improved Boundary Layer Quantities in the Shock Wave Boundary Layer Interaction Region on Bumps-Reference-Cited by-同舟云学术

Improved Boundary Layer Quantities in the Shock Wave Boundary Layer Interaction Region on Bumps

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:35th AIAA Fluid Dynamics Conference and Exhibit
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Author:

Bhanderi Harish¹,Babinsky Holger¹

Affiliation:

1. University of Cambridge

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4896

Reference13 articles.

1. Viscous-inviscid interactions in external aerodynamics

2. Shock wave/turbulent boundary layer interaction and its control

3. 4Sawyer, W. G. and Long, C. J. “A study of normal shock wave turbulent boundary layer interactions at Mach numbers of 1.3, 1.4 and 1.5,” Tech. Rep. 82099, Royal Aircraft Establishment, October 1982.

4. 5East, L. F. “A representation of second-order boundary layer effects in the momentum integral equation and in viscousinviscid interactions,” Tech. Rep. 81002, Royal Aircraft Establishment, January 1981.

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