Study of Shock–Wave/Boundary–Layer Interaction Flowfield on a 24° Ramp Model
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Publisher
Springer Berlin Heidelberg
Link
http://link.springer.com/content/pdf/10.1007/978-3-540-45466-3_18.pdf
Reference9 articles.
1. A.L. Kistler. Fluctuating wall pressure under a separated supersonic flow. Journal of the Acoustical Society of America, 36 (No.3):pp. 543–550, 1964.
2. D.S. Dolling and M.T. Murphy. Unsteadiness of the separation shock wave structure in a supersonic compression ramp field. AIAA Journal Vol. 21(No. 12):pp. 1628–1634, 1983.
3. B.T. Gibson and D.S. Doffing. Exploratory study of wall pressure fluctuations in a mach 5 sharp fin-induced turbulent interaction. AIAA Journal, 30 (9): 2188–2195, 1992.
4. D.J. Maull. Hypersonic flow over axially symmetric spiked bodies. Journal of Fluid Mechanics, Vol. 8 (Part 4):pp. 584–592, 1969.
5. C.C. Horstman and F.K. Owen. New diagnostic technique for the study of turbulent boundary layer separation. AIAA Journal, Vol. 12 (No.10):pp. 1436–1438, 1974.
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