An experimental investigation of the unsteady behavior of blunt fin-induced shock wave turbulent boundary layer interaction
Author:
Affiliation:
1. Princeton University, Princeton, NJ
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1287
Reference36 articles.
1. Investigation of Three-Dimensional Shock/Boundary-Layer Interactions at Swept Compression Corners
2. 3Settles, G. S. "An Experimental Study of Compressible Turbulent Boundary Layer Separation a t High Reynolds Number," Ph.D. Dissertation. Aerospace and Mechanical Sciences Dept.Princeton University, Princeton, NJ,Sept. 1975.
3. 'Settles, G. S., Bogdonoff, 5. M. and Vas, 1. E. "Incipient Separation of a Suoersonic Turbulent Boundary Layer a t High Reynolds Numbers," aIahJournal, Vol. 14,Jan. 1976, pp.50-56.
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