Experimental study on fluctuating thermal loads in swept shock wave/turbulent boundary-layer interactions
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering
Link
http://link.springer.com/content/pdf/10.1007/BF02945733.pdf
Reference17 articles.
1. Alvi, F. S., Settles, G. S., 1991, “Physical Flowfield Model of the Swept Shock/Boundary-Layer Interaction Flowfield,”AIAA Paper 91 1768.
2. Dolling, D. S. and Murphy, M. T., 1983, “Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield,”AIAA Journal, Vol. 21, No. 12, pp. 1628–1634.
3. Dolling, D. S., 1993, “Fluctuating Loads in Shock Wave/Turbulent Boundary-Layer Interactions: Tutorial and Update,”AIAA paper 93-0284.
4. Erengil, B. and Dolling, D. S., 1993, “Effects of Sweepback on Unsteady Separation in Mach 5 Compression Ramp Interactions,”AIAA Journal, Vol. 31, No. 2, pp. 302–311.
5. Garg, S. and Settle, G. S., 1996, “Unsteady Pressure Loads Generated by Swept-Shock-Wave/Boundary-Layer Interactions,”AIAA Journal, Vol. 34, No. 6, pp. 1174–1181.
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1. Shock Wave and Boundary Layer Interactions;Theoretical and Experimental Aerodynamics;2018-12-16
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