Experimental investigation of the effects of leading edge bluntness on supersonic flow over a double compression ramp
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
https://link.springer.com/content/pdf/10.1007/s12206-020-0911-z.pdf
Reference33 articles.
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3. D. Gaitonde, Progress in shock wave/boundary layer interactions, Progress in Aerospace Science, 72 (2015) 80–99.
4. B. John and V. Kulkarni, Effect of leading edge bluntness on the interaction of ramp induced shock wave with laminar boundary layer at hypersonic speed, Computer & Fluids, 96 (2014) 177–190.
5. B. John, V. Kulkarni and G. Natarajan, Shock wave boundary layer interactions in hypersonic flow, International Journal of Heat and Mass Transfer, 70 (2014) 81–90.
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