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Study of the Interaction of a Streamwise-Oscillating Shock with the Boundary Layer on a Flat Plate

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Abstract

The distinctive features of the flow in the region of interaction between an oscillating shock and a flat-plate boundary layer are studied for the laminar, transitional, and turbulent flow regimes. The flow patterns and the pressure and heat transfer distributions in the interaction region are analyzed at different intensities, frequencies, and amplitudes of the oscillating shock. The results of the interaction of oscillating and steady shocks with the flat-plate boundary layer are compared.

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REFERENCES

  1. G. I. Petrov, High-Velocity Aeromechanics and Space Research. Selected Works[in Russian], Nauka, Moscow (1992).

    Google Scholar 

  2. G. I. Petrov, V. Ya. Likhushin, I. P. Nekrasov, and L. I. Sorkin, "Viscosity effect on a supersonic flow with shocks," Tr. TsIAM, No. 224 (1952).

  3. R. J. Hanniken, I. Greber, L. Trilling, and S. S. Abarbanel, "The interaction of an oblique shock wave with a laminar boundary layer," NASA Mem., NT. 2-18-59 W (1959).

  4. J. G. Marvin, C. C. Horstman, M. W. Rubesin, T. J. Coakley, and M. I. Kussoy, "An experimental and numerical investigation of shock wave induced turbulent boundary layer separation at hypersonic speeds," AGARD CP168, Paper 25, Göttingen (1975).

  5. D. R. Chapman, M. Kuehn, and K. Larson, "Investigation of separated flows in supersonic and subsonic stream with emphasis on the effect of transition," NASA Rep., No. 1356 (1958).

  6. I. A. Kondrat'yev, "Experimental investigation of heat transfer on a flat plate on interaction of an oblique shock with a laminar boundary layer," Uch. Zap TsAGI, 2, No. 2, 18 (1971).

    Google Scholar 

  7. S. Sayano, "Heat transfer in shock wave-turbulent boundary layer interaction regions," Douglas Aircraft Co. Rep.SM 42567 (1962).

  8. U. Rist, A. Pagella, O. Krause, and A. Babucke, "Interaction of an oscillating shock with a laminar boundary layer," in: Euromech 440. Aerodynamics and Thermochemistry of High Speed Flows, Marseilles (2002), p. 119.

  9. J. L. Amick, "Semiempirical relation for laminar separation," J. Aero/Space Sci., 26, 603 (1959).

    Google Scholar 

  10. W. J. Guman, "On the plateau and peak pressure of regions of pure laminar and fully turbulent separation in two-dimensional supersonic flows," J. Aero/Space Sci., 26, 56 (1959).

    Google Scholar 

  11. P. K. Chang, Separation of Flows, Pergamon, Oxford (1970).

    Google Scholar 

  12. A. A. Zheltovodov, "Properties of two-and three-dimensional separation flows at supersonic velocities," Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 42 (1979).

  13. V. Ya. Neiland, "Asymptotic problems of theory of viscous supersonic flows," Tr. TsAGI, No. 1529 (1974).

  14. G. N. Abramovich, Applied Gas Dynamics[in Russian], Nauka, Moscow (1969).

    Google Scholar 

  15. J. W. Kayes and F. D. Hains, "Analytical and experimental studies of shock interference heating in hypersonic flows," NASA TN D-7139 (1973).

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Pilyugin, N.N., Khlebnikov, V.S. Study of the Interaction of a Streamwise-Oscillating Shock with the Boundary Layer on a Flat Plate. Fluid Dynamics 39, 485–494 (2004). https://doi.org/10.1023/B:FLUI.0000038567.54882.7a

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  • DOI: https://doi.org/10.1023/B:FLUI.0000038567.54882.7a

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