Calculation of the interaction of a laminar boundary layer with an external supersonic flow behind an obstacle

Author:

Antonov A. N.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference16 articles.

1. L. Crocco and L. Lees, ?Mixing theory to determine the interaction of dissipative and almost isentropic flows,? Vopr. Raketn. Tekh., No. 2 (1953).

2. C. B. Cohen and E. Reshotko, ?Similar solution for the compressible laminar boundary layer with heat transfer and pressure gradient,? NACA Rep. No. 1293 (1956).

3. C. B. Cohen and E. Reshotko, ?The compressible laminar boundary layer with heat transfer and arbitrary pressure gradients,? NACA Rep. No. 1294 (1956).

4. V. Reeves and L. Lees, ?Supersonic separated and attached laminar flows. Part 1. General theory and its application to analysis of interaction between a shock and an adiabatic boundary layer,? Raketn. Tekh. Kosm, No. 11 (1964).

5. L. Lees and V. Reeves, ?Theory of the laminar near wake behind blunt bodies in hypersonic flow,? Raketn. Tekh. Kosm., No. 11 (1965).

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