Investigation of a hypersonic viscous shock layer on rotating axisymmetric bodies in the presence of blowing

Author:

Krasilov N. A.,Levin V. A.,Yunitskii S. A.

Publisher

Springer Science and Business Media LLC

Subject

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

Reference19 articles.

1. C. R. Illingworth, ?The laminar boundary layer of a rotating body of revolution,? Philos Mag.,44, 339 (1953).

2. N. E. Khoskin, ?Laminar boundary layer on a rotating sphere,? in: The Boundary Layer Problem and Questions of Heat Transfer [in Russian], Énergoizdat, Leningrad (1960), pp. 114?118.

3. H. A. Dwyer and B. R. Sanders, ?A physically optimal difference scheme for three-dimensional boundary layers,? in: Mechanics. New Results in Foreign (Non-Soviet) Science, No. 14, Numerical Solution of Problems of Hydrodynamics [Russian translation], Mir, Moscow (1977), pp. 107?116.

4. R. Kobayashi, Y. Kohama, and M. Kurosava, ?Boundary-layer transition on a rotating cone in axial flow,? J. Fluid Mech.,127, 341 (1983).

5. A. N. Pokrovskii, V. N. Shmanenkov, and V. M. Shchuchinov, ?Determination of boundary-layer parameters on rotating axisymmetric cones,? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 34 (1984).

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