Effect of Small Bluntness on Formation of Görtler Vortices in a Supersonic Compression Corner Flow
Author:
Publisher
Pleiades Publishing Ltd
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://link.springer.com/article/10.1134/S0021894417060037/fulltext.html
Reference35 articles.
1. J. K. H. Holger Babinsky, Shock Wave-Boundary-Layer Interactions: Cambridge Aerospace (Cambridge University Press, Cambridge, 2011).
2. P. K. Chang, “Characteristics of Separated Flows,” in Separation of Flow, Ed. by P. K. Chang (Pergamon Press, Oxford, London–Edinburgh, 1970), Chapter 7, pp. 272–335.
3. E. H. Hirschel, Basics of Aerothermodynamics (Springer, 2015).
4. H. Schlichting, Boundary Layer Theory (McGraw, New York, 1960).
5. R. E. Spall and M. R. Malik, “Goertler Vortices in Supersonic and Hypersonic Boundary Layers,” Phys. Fluids, A: Fluid Dyn. 1 (11), 1822–1835 (1989).
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