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Supersonic viscous perfect gas flow past a circular cylinder

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Abstract

The complete Navier-Stokes equations are used to calculate supersonic perfect gas flow past a circular isothermal cylinder by the method described in [1]. The effects of the Mach number M∞=2.5–10 and the Reynolds number Re=30-105 on the flowfield structure and heat transfer to the cylinder wall are investigated. Special attention is paid to the study of the near wake and the local characteristics on the leeward side of the cylinder.

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References

  1. I. V. Egorov and O. L. Zaitsev, “On an approach to the numerical solution of the two-dimensional Navier-Stokes equations by the shock capturing method,”Zh. Vychisl. Mat. Mat. Fiz.,31, 286 (1991); see also Preprint No. 6, TsAGI, Moscow (1990).

    Google Scholar 

  2. é. A. Gershbein, S. V. Peigin, and G. A. Tirskii, “Supersonic flow past bodies at small and moderate Reynolds numbers,” in:Advances in Science and Engineering. Fluid Mechanics, Vol. 19 [in Russian], VINITI (1985), p. 3.

  3. S.V. Peigin and G. A. Tirskii, “Three-dimensional problems of super- and hypersonic viscous gas flow past bodies,” in:Advances in Science and Engineering. Fluid Mechanics, Vol. 22 [in Russian], VINITI (1988), p. 3.

  4. V. A. Bashkin and I. Yu. Babaev, “Calculation of supersonic perfect gas flow past the front surface of a slipping circular cylinder,”Uch. Zap. TsAGI,23, 9 (1992).

    Google Scholar 

  5. V. P. Kolgan, “Application of the principle of minimum value of derivatives to the construction of finite-difference schemes for calculating discontinuous solutions of gas dynamics,”Uch. Zap. TsAGI,3, 68 (1972).

    Google Scholar 

  6. A. Harten, “High-resolution schemes for hyperbolic conservation laws,”J. Comput. Phys.,49, 357 (1983).

    Google Scholar 

  7. P. L. Roe, “Approximate Reimann solvers, parameter vectors, and difference schemes,”J. Comput. Phys.,43, 357 (1981).

    Google Scholar 

  8. R. J. Lipton, D. J. Rose, and R. E. Tarjan, “Generalized nested dissection,”SIAM J. Numer. Analys.,16, 346 (1979).

    Google Scholar 

  9. V. Ya. Borovoi, W. N. Brashko, and G. I. Maikapar, “Leeward separated supersonic flows,” in:Separated Flows and Jets. Proc. IUTAM Symp. Novosibirsk, USSR, 1990, Springer-Verlag, Berlin (1991), p. 311.

    Google Scholar 

  10. V. Ya. Neiland, “Asymptotic problems of the theory of viscous supersonic flow,”Tr. TsAGI, No. 1529 (1974).

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Authors and Affiliations

  1. Moscow

    V. A. Bashkin, I. V. Egorov & M. V. Egorova

Authors
  1. V. A. Bashkin
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  2. I. V. Egorov
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  3. M. V. Egorova
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Additional information

Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No.6, pp. 107–115, November–December, 1993.

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Bashkin, V.A., Egorov, I.V. & Egorova, M.V. Supersonic viscous perfect gas flow past a circular cylinder. Fluid Dyn 28, 833–838 (1993). https://doi.org/10.1007/BF01049787

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  • DOI: https://doi.org/10.1007/BF01049787

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