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Calculation of the laminar boundary layer on the flow-spreading line of the frontal surface of a segmental body in supersonic gas flow

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References

  1. I. V. Petukhov, “Numerical calculation of two-dimensional flows in a boundary layer”, collection: Numerical Methods for the Solution of Differential and Integral Equations and Quadrature Formulas [in Russian], Nauka, 1964.

  2. F. K. Moore, “Displacement Effect of a Three-Dimensional Boundary Layer.” NACA Rep. no. 1124, 1953.

  3. A. N. Minailos, “On the calculation of the flow on a blunt body of revolution at angle of attack in supersonic gas flow.” Zh. vychisl. matem. i matem. fiz., vol. 4, no. 1, 1964.

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  1. Moscow

    S. N. Seliverstov

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  1. S. N. Seliverstov
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Seliverstov, S.N. Calculation of the laminar boundary layer on the flow-spreading line of the frontal surface of a segmental body in supersonic gas flow. Fluid Dyn 3, 72–75 (1968). https://doi.org/10.1007/BF01019199

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  • DOI: https://doi.org/10.1007/BF01019199

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