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Similar solutions of the boundary layer equations for a slender body of revolution in the presence of a positive pressure gradient

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References

  1. K. Stewartson, “Further solutions of the Falkner-Skan equation”, Proc. Cambridge Philos. Soc., vol. 50, pt. 3, 1954.

  2. V. M. Falkner and S. W. Skan, “Some approximate solutions of the boundary layer equations”, Aeronaut. Res. Council Rept. no. 1314, 1930.

  3. L. Lees, and B. L. Reeves, “Supersonic separated and reattaching laminar flows, 1: General theory and application to adiabatic boundary layer/shock-wave interactions”, AIAA Journal, vol. 2, no. 11, 1964.

  4. E. N. Bondarev, “Approximate calculation of the interaction of supersonic flow with a laminar layer in the flow separation region”, Izv. AN SSSR, MZhG [Fluid Dynamics], vol. 1, no. 5, 1966.

  5. H. Wei, “Asymptotic boundary layer over a slender body of revolution in axial compressible flow”, AIAA Journal, vol. 3, no. 5, pp. 809–816, 1965.

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  1. Moscow

    L. M. Kolesnikova, L. G. Frolov & V. N. Shmanenkov

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  1. L. M. Kolesnikova
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  2. L. G. Frolov
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  3. V. N. Shmanenkov
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Kolesnikova, L.M., Frolov, L.G. & Shmanenkov, V.N. Similar solutions of the boundary layer equations for a slender body of revolution in the presence of a positive pressure gradient. Fluid Dyn 5, 161–163 (1970). https://doi.org/10.1007/BF01015016

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