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Approximate calculation of the critical pressures for turbulent boundary layer separation and attachment in supersonic flow

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References

  1. S. M. Bogdonoff, “Some experimental studies of the separation of supersonic turbulent boundary layers”, Princeton University Report, 336, 1955.

  2. M. S. Solomonov, June General Assembly of the Division of Technical Sciences of the Academy of Sciences USSR. Comment on the report of G. I. Petrov”, Izv. AN SSSR, OTN, no. 9, 1958.

  3. D. R. Chapman, D. M. Kuehn, and H. H. Larson, Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition, NACA Rep. no. 1356, 1958.

  4. G. L. Grodzovskii, “Experimental study of the interaction of compression shocks and the boundary layer in the range M=1.0–1.8”, Izv. AN SSSR, OTN, Energetika i avtomatika, no. 4, 1961.

  5. H. H. Korst, “Theory for base pressure in transonic and supersonic flow”, Journal of Applied Mechanics, vol. 23, no. 4, 1956.

  6. M. Sirieix, “Pression de culot et processus de melange turbulent en ecoulement supersonique plan”, Rech. Aeronaut., no. 78, 1960.

  7. A. Mager, “On the model of the free shock-separated turbulent boundary-layer”, Journal of Aeronautical Science, no. 2, 1956.

  8. L. Crocco and L. Lees, “A mixing theory for the interaction between dissipative flows and nearly isentropic streams”, Journal of Aeronautical Science, vol. 19, no. 10, 1952.

  9. L. Crocco, “Considerations of the shock-boundary layer interaction”, Proc. Conf. on High-Speed Aeronautics, 1955.

  10. G. N. Abramovich, Turbulent Jet Theory [in Russian], Fizmatgiz, 1960.

  11. A. S. Ginevskii, “Turbulent wake and jet in a parallel flow with a longitudinal pressure gradient”, Izv. AN SSSR, OTN, Mekhanika i mashinostroenie, no. 2, 1959.

  12. L. Crocco, “One-dimensional consideration of the gasdynamics of steady flows”, in: Fundamentals of Gasdynamics, ed. H. W. Emmons [Russian translation], Izd-vo inostr. lit., 1963.

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Authors and Affiliations

  1. Moscow

    L. V. Gogish

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  1. L. V. Gogish
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In conclusion the author wishes to thank G. Yu. Stepanov for the problem formulation and continued insistence on its solution.

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Gogish, L.V. Approximate calculation of the critical pressures for turbulent boundary layer separation and attachment in supersonic flow. Fluid Dyn 3, 68–71 (1968). https://doi.org/10.1007/BF01019198

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  • DOI: https://doi.org/10.1007/BF01019198

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