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Asymptotic solution of the shock layer equations near the stagnation point of a sphere with intense blowing

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Literature cited

  1. É. A. Gershbein and G. A. Tirskii, “Flow of a viscous, heat-conducting, multicomponent gas in a shock layer near the stagnation point with intense blowing,” Nauch. Tr. In-ta Mekhan. MGU, No. 1 (1970).

  2. V. N. Filimonov, “Asymptotic solution of the equations of the incompressible boundary layer with negative pressure gradient for strong blowing,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. i Gaza, No. 5 (1967).

  3. É. A. Gershbein, “The laminar multicomponent boundary layer with strong blowing,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. i Gaza, No. 1 (1970).

  4. É, A. Gershbein, “Numerical and asymptotic similarity solution of the boundary-layer equations with strong blowing,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. i Gaza, No. 3 (1971).

  5. G. A. Danilin, “An asymptotic solution of the Navier-Stokes equations for flow of a compressible fluid in a two-dimensional channel with intense blowing from the walls,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. i Gaza, No. 6 (1971).

  6. W. D. Hayes and R. F. Probstein (editors), Hypersonic Flow Theory, Academic Press (1967).

  7. K. M. Magomedov, “Hypersonic flow of a viscous gas over blunt bodies,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. i Gaza, No. 2 (1970).

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  1. Moscow

    G. A. Danilin

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  1. G. A. Danilin
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 164–168, January–February, 1973.

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Danilin, G.A. Asymptotic solution of the shock layer equations near the stagnation point of a sphere with intense blowing. Fluid Dyn 8, 152–156 (1973). https://doi.org/10.1007/BF01017652

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  • DOI: https://doi.org/10.1007/BF01017652

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