Impact of Shock Wave Boundary Layer Interaction on the Internal Flow and Performance of Scramjet Intake
Author:
Publisher
Pleiades Publishing Ltd
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1134/S0015462821060069.pdf
Reference31 articles.
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3. Sziroczak, D. and Smith, H., A review of design issues specific to hypersonic flight vehicles, Progress in Aerospace Sciences, 2016, vol. 84, pp. 1–28.
4. Heiser, W.H. and Pratt, D.T., Hypersonic Air-Breathing Propulsion, AIAA, 1994.
5. Schulte, D., Henckels, A., and Neubacher, R., Manipulation of shock/boundary-layer interactions in hypersonic inlets, Journal of Propulsion and Power, 2001, vol. 17, no. 3, pp. 585–590.
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