Control of shock-wave boundary layer interaction using steady micro-jets
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/s00193-014-0508-5.pdf
Reference33 articles.
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3. Dolling, D.S., Murphy, M.T.: Unsteadiness of the separation shock wave structure in a supersonic compression ramp flowfield. AIAA J. 21(12), 1628–1634 (1983)
4. Dolling, D.S.: Fifty years of shock-wave/boundary layer interaction research: what next? AIAA J. 39(8), 1517–1531 (2001)
5. Dolling, D.S., Or, C.T.: Unsteadiness of the shock wave structure in attached and separated compression ramp flows. Exp. Fluids 3, 24–32 (1985)
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