Impact of pure favorable pressure gradient on a supersonic flat-plate turbulent boundary layer
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference30 articles.
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4. Effect of adverse pressure gradient on high speed boundary layer transition;Franko;Phys. Fluids,2014
5. Structural characteristics of the supersonic turbulent boundary layer subjected to concave curvature;Wang;Appl. Phys. Lett.,2016
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