The research of laminar-turbulent transition in hypersonic three-dimensional boundary layer

Author:

Goldfeld Marat A.,Orlik Evgeniy V.

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference15 articles.

1. Gutov, B I, Zotoloka, V V. Design and Experimental Investigation of the Convergent Inlet Configurations with 3-D Flow Combinations. Preprint ITAM SD USSR AS N30-83, Novosibirsk, 1983

2. Goldfeld, M A. Experimental Study of 3-D Inlets for High Supersonic Flight Velocities. ICAR N5, 1994

3. Gogish, L V, Stepanov, G Yu. Turbulent Separated Flows. Nauka, Moscow, 1979

4. Goldfeld, M A, Tyutina, E G. Investigations of the Compressible Axisymmetric Turbulent Boundary Layer under the Complicated Conditions with the Flow Separation. Preprint ITAM SD USSR AS N17-83, Novosibirsk, 1983

5. Sasman, P K, Cresci, R S. Compressible Turbulent Boundary Layer with Pressure Gradient and Heat Transfer. AIAA J, 1966, (1): 19–25

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