Abstract
An engineering method is proposed for determining the initiation of turbulence in a subsonic (M ⩽ 1) laminar boundary layer with a heat supply in the presence of a pressure gradient and injection.
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Literature cited
G. Schlichting, Boundary Layer Theory, McGraw-Hill (1966).
D. C. Wilcox, “A model for transitional flow,” AIAA Paper No. 77-126 (1977) (translation No. 561 in TsAGI, 1–21 (1979)),
W. H. Dorrance, Hypersonic Flows of a Viscous Gas [Russian translation], Mir, Moscow (1966).
E. I. Polyak, “Study of solutions of the equation of a laminar boundary layer with small temperature factors and large M numbers,” Inzh.-Fiz. Zh.,31, No. 5, 850–856 (1976).
S. F. Shen, Stability of Laminar Flow. Theory of Laminar Flows, IV (ed. F. K. Morrow), Princeton University Press (1964), pp. 719–853.
Additional information
Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 45, No. 1, pp, 21–25, July, 1983.
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Polyak, E.I. Possibility of rapid determination of turbulence generation in a laminar boundary layer. Journal of Engineering Physics 45, 724–728 (1983). https://doi.org/10.1007/BF00845430
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DOI: https://doi.org/10.1007/BF00845430