The Development of Turbulent Boundary Layers
Author:
Affiliation:
1. Cambridge University Aeronautics Laboratory,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.3494
Reference26 articles.
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5. An Experimental Investigation of Nozzle-Exit Boundary Layers of Highly Heated Free Jets;Journal of Turbomachinery;1992-04-01
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