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Effect of supersonic stream parameters on the characteristic time of transient step flow

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Abstract

There have been many studies of viscous compressible gas flow in wakes and behind steps [1–6] in which attention has been focused on the steady-state flow regime. The problem of the supersonic flow of a viscous compressible heat-conducting gas past a plain backward-facing step is considered. The problem is solved numerically within the framework of the complete system of Navier-Stokes equations. The passage of the solution from the initial data to the steady-state regime and the effect of the gas dynamic parameters of the external flow on the characteristic flow stabilization time are investigated.

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Literature cited

  1. P. K. Chang, Separation of Flow, Pergamon, Oxford (1970).

    Google Scholar 

  2. A. I. Shvets abd I. T. Shvets, Gas Dynamics of the Near Wake [in Russian], Naukova Dumka, Kiev (1976).

    Google Scholar 

  3. R. K. Tagirov, “Experimental investigation of separated flow behind a plane step at M=1.97,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 4, 153 (1969).

    Google Scholar 

  4. I. Yu. Brailovskaya, “Flow in the near wake,” Dokl. Akad. Nauk SSSR,197, 542 (1971).

    Google Scholar 

  5. V. I. Myshenkov, “Numerical investigation of viscous gas flow in the wake of a plane body,” Zh. Vychisl. Mat. Mat. Fiz., No. 3, 673 (1972).

    Google Scholar 

  6. T. B. Luzyanina and V. M. Paskonov, “Calculation of axisymmetric viscous gas flows in the near wake behind bodies with a complex rear-end geometry,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 2, 31 (1987).

    Google Scholar 

  7. A. E. Bondarev, “Numerical investigation of supersonic viscous compressible gas flow past a plane backward-facing step,” Preprint No. 16 [in Russian], M. V. Keldysh Institute of Problems of Mechanics, USSR Academy of Sciences, Moscow (1988).

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  8. V. M. Paskonov, V. I. Polezhaev, and L. A. Chudov, Numerical Modeling of Heat and Mass Transfer Processes [in Russian], Nauka, Moscow (1984).

    Google Scholar 

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Authors and Affiliations

  1. Moscow

    A. E. Bondarev

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  1. A. E. Bondarev
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 137–140, July–August, 1989.

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Bondarev, A.E. Effect of supersonic stream parameters on the characteristic time of transient step flow. Fluid Dyn 24, 604–607 (1989). https://doi.org/10.1007/BF01052425

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  • DOI: https://doi.org/10.1007/BF01052425

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