Interaction Between a Conical Shock Wave and a Plane Turbulent Boundary Layer
Author:
Affiliation:
1. Australian Defence Force Academy, Canberra, Australian Capital Territory 2600, Australia
2. Nanyang Technological University, Singapore 639798, Republic of Singapore
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1060
Reference16 articles.
1. Three-Dimensional Shock-Wave Reflections
2. Interaction of incident three-dimensional shock with a turbulent boundary layer
3. Investigation of a Three-Dimensional Shock Wave Separated Turbulent Boundary Layer
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