Supersonic Viscous-Inviscid Interaction of a Swept Compression Ramp with a Turbulent Boundary-Layer

Author:

Inger G. R.

Publisher

Springer Berlin Heidelberg

Reference15 articles.

1. Inger, G. R., “Upstream Influence and Skin Friction in Non-Separate Shock/Turbulent Boundary Layer Interactions,” AIAA Paper 80-1411, July 1980 [see also article in Numerical and Physical Aspects of Aerodynamic Flows (T. Cebeci, Ed.), Springer-Verlag, N.Y. 1982].

2. Melnik, R., “A Survey of Turbulent Viscid-Inviscid Interaction Theory in Aerodynamics,” AIAA Paper 84-0264, Reno, Nevada, January 10.

3. Inger, G. R., “Some Features of a Shock-Boundary Layer Interaction Theory in Transonic Flow Fields,” in AGARD CP-291 (“Computation of Viscous-Inviscid Interactions”), September 1980, pp. 18-1 to 18–66.

4. Nandanan, M., E. Stanewsky and G. R. Inger, “A Computational Procedure for Transonic Airfoil Flow Including a Special Solution for Shock-Boundary Layer Interaction,” AIAA Journal 19, December 1981, pp. 1840–1846.

5. Walz, A., Boundary Layers of Flow and Temperature, M.I.T. Press, 1969, pp. 113–115.

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