Approximate calculation of the interaction of supersonic flow with a laminar layer in the flow separation region

Author:

Bondarev E. N.

Publisher

Springer Science and Business Media LLC

Subject

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

Reference11 articles.

1. L. Crocco and L. Lees ?A mixing theory for the interaction between dissipative flows and nearly isentropic streams?, J. Aeronaut. Sci., vol. 19, no. 10, 1952.

2. K. N. C. Bray, G. E. Gadd, and M. Woodger, ?Some calculations by the Crocco-Lees and other methods of interactions between shock waves and laminar boundary layers, including effects of heat transfer and suction?, ARC C. P., no. 556, 1961.

3. Makofski, ?A two-parameter method for shock wave-laminar boundary layer interaction and flow separation?, Proc. Heat Transfer and Fluid Mechanics Institute, Stanford, California, 1963.

4. Yu. G. El'kin and V. Ya. Neiland, ?On the calculation of the characteristics of laminar separation zones?, Inzh. zh., vol. 5, no. 5, 1961.

5. L. Lees and B. L. Reeves, ?Supersonic separated and reattaching laminar flow: 1, General theory and application to adiabatic boundary layer; Shock-wave interactions?, AIAA Journ., vol. 2, no. 11, 1964.

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