Supersonic flow past a system of two swept wedges mounted on a preliminary compression surface

Author:

Gun’ko Yu. P.,Mazhul’ I. I.

Publisher

Pleiades Publishing Ltd

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Reference7 articles.

1. H. Babinsky and J.K. Harvey, Shock Wave-Boundary Layer Interactions, Cambridge Univ. Press, Cambridge (2011).

2. A.V. Lokotko and A.M. Kharitonov, “Special Features of a Supersonic Flow in a Stepwise Channel with Different Inlets,” Thermophys. Aeromech. No. 3, 275 (1999).

3. G.S. Settles, J.J. Perkins, and S.M. Bogdonoff, “Investigation of Three-Dimensional Shock/Boundary-Layer Interactions at Swept Compression Corners,” AIAA J. 18, 779 (1980).

4. A.A. Zheltovodov and A.M. Kharitonov, “On the Analogy between Two-Dimensional and Three-Dimensional Separation Flows,” in: Physical Gasdynamics (Aerophysical Studies, Issue 6) [in Russian], Institute of Theoretical and Applied Mechanics, Novosibirsk (1976), p. 130.

5. E.E. Zukoski, “TurbulentBoundary-Layer Separation in Front of a Forward-Facing Step,” AIAA J. 5, 1746 (1967).

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