Investigation of Oblique Breakdown in a Supersonic Boundary Layer at Mach 2 Using DNS-Reference-Cited by-同舟云学术

Investigation of Oblique Breakdown in a Supersonic Boundary Layer at Mach 2 Using DNS

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

Mayer Christian¹,Wernz Stefan¹,Fasel Hermann¹

Affiliation:

1. University of Arizona

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-949

Reference15 articles.

1. Numerical Simulation of Spatially Growing Three-Dimensional Disturbance Waves in Compressible Boundary Layers

2. 2Thumm, A., Numerische Untersuchungen zum laminar-turbulenten Stromungsumschlag in transsonischen Grenzschichtstromungen, Ph.D. thesis,Universität Stuttgart, 1991.

3. 4Chang, C.L. and Malik, M. R. “Linear and Nonlinear PSE for Compressible Boundary Layers,” Tech. Rep. CR-191537, NASA, 1993.

4. Oblique-mode breakdown and secondary instability in supersonic boundary layers

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