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Investigation of Flow past a Flat Plate in the Strong Interaction Regime

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Abstract

Viscous gas flow past a finite-length plate in the strong interaction regime is investigated. The expansions of the flow functions in the vicinity of the leading edge are derived and the boundary value problems for the viscous and inviscid flow regions are formulated and jointly solved. The effect of the adiabatic exponent and the temperature factor on the flow parameters in these regions and the eigenvalue determining the intensity of the upstream disturbance transfer is studied. It is shown that in the non-self-similar case a transitional layer arises at the outer edge of the boundary layer.

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References

  1. L. Lees, “On the Boundary-Layer Equations and Their Approximate Solution,” J. Aeron. Sci. 20(2), 143 (1953).

    Article  MATH  Google Scholar 

  2. K. Stewartson, “On the Motion of a Flat Plate at High Speed in a Viscous Compressible Fluid. II. Steady Motion,” J. Aeron. Sci. 22(5), 303 (1955).

    Article  MathSciNet  MATH  Google Scholar 

  3. V. Ya. Neiland, “Propagation of Perturbations Upstream with Interaction between a Hypersonic Flow and a Boundary Layer,” Fluid Dynamics 5(4), 559 (1970).

    Article  ADS  Google Scholar 

  4. S. N. Brown and K. Stewartson, “A Non-Uniqueness of the Hypersonic Boundary Layer,” Quart. J. Mech. Appl.Math. 28(1), 75 (1975).

    Article  MATH  Google Scholar 

  5. W. B. Bush, “Hypersonic Strong-Interaction Similarity Solution for Flow past a Flat Plate,” J. Fluid Mech. 25(1), 51 (1966).

    Article  ADS  MathSciNet  MATH  Google Scholar 

  6. R. S. Lee and H. K. Cheng, “On the Outer-Edge Problem of a Hypersonic Boundary Layer,” J. Fluid Mech. 38(1), 161 (1969).

    Article  ADS  MATH  Google Scholar 

  7. W. D. Hayes and R. F. Probstein, Hypersonic Flow Theory (Acad. Press, New York, 1966).

    MATH  Google Scholar 

  8. K. Stewartson, The Theory of Laminar Boundary Layer in Compressible Fluids (Oxford Univ. Press, Oxford, 1964).

    MATH  Google Scholar 

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Authors and Affiliations

  1. Moscow Institute of Physics and Technology, Institutskii per. 9, Dolgoprudnyi, Moscow oblast, 141701, Russia

    A. A. Balashov

  2. Central Aerohydrodynamic Institute (TsAGI), ul. Zhukovskogo 1, Zhukovskii, Moscow oblast, 140180, Russia

    G. N. Dudin

Authors
  1. A. A. Balashov
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  2. G. N. Dudin
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Correspondence to A. A. Balashov.

Additional information

Original Russian Text © A.A. Balashov, G.N. Dudin, 2018, published in Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, 2018, No. 3, pp. 63–70.

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Balashov, A.A., Dudin, G.N. Investigation of Flow past a Flat Plate in the Strong Interaction Regime. Fluid Dyn 53, 394–401 (2018). https://doi.org/10.1134/S0015462818030035

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  • DOI: https://doi.org/10.1134/S0015462818030035

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