Results of a strong interaction, wake-like model of supersonic separated and reattaching turbulent flows
Author:
Affiliation:
1. Avco Systems Division, Wilmington, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6251
Reference29 articles.
1. Integral theory for supersonic turbulent base flows.
2. Surface mass injection at supersonic and hypersonic speeds as a problem in turbulent mixing. I.
3. Effect of finite plate length on supersonic turbulent boundary layerwith large distributed surface injection
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