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Unsteady boundary layer with self-induced pressure near rapidly heated segment of flat plate in supersonic flow

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Literature cited

  1. P. G. Daniels, “The flow about the trailing edge of a supersonic oscillating aerofoil,” J. Fluid Mech.,72, No. 3 (1975).

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  4. V. I. Zhuk and O. S. Ryzhov, “Solutions of dispersion equation using the theory of free boundary-layer interaction,” Dokl. Akad. Nauk SSSR,247, No. 5 (1979).

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Translated from Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki, No. 1, pp. 38–43, January–February, 1983.

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Kazakov, A.V. Unsteady boundary layer with self-induced pressure near rapidly heated segment of flat plate in supersonic flow. J Appl Mech Tech Phys 24, 33–37 (1983). https://doi.org/10.1007/BF00914474

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  • DOI: https://doi.org/10.1007/BF00914474

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