Abstract
A method is proposed for calculating a turbulent boundary layer on a surface with a viscoelastic coating. The method is based on the introduction of the van Driest damping function to account for the effect of the coating on the boundary layer.
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M. G. Fisher, L. M. Weinstein, D. M. Bushnell, and R. L. Ash, “Compliant wall-turbulent skin friction reduction research,” AIAA Paper, No. 75–833, 1–30 (1975).
D. T. Tsahalis, “On the theory of skin friction reduction by compliant walls,” AIAA Paper, No. 686, 1–11 (1977).
G. A. Voropaev, “Calculation of certain characteristics of a turbulent boundary layer on a compliant surface,” in: Mathematical Methods of Studying Flow Hydrodynamics [in Russian], Naukova Dumka, Kiev (1978), pp. 9–13.
K. K. Fedyaevskii, A. S. Ginevskii, and A. V. Kolesnikov, Calculation of the Turbulent Boundary Layer of an Incompressible Fluid [in Russian], Sudostroenie, Leningrad (1973).
W. B. Nicoll, A. B. Strong, and K. A. Woolner, “On the laminar motion of a fluid near an oscillating porous infinite plane,” Trans. ASME, Ser. E,35, No. 1, 324–327 (1968).
A. B. Airapetov, “Laminar motion of a viscous incompressible fluid next to a permeable cylinder vibrating in the fluid,” Uch. Zap. TsAGI,4, No. 5, 88–92 (1973).
K. R. Sreenivasan and R. A. Antonia, “Properties of wall shear stress fluctuations in a turbulent duct flow,” Trans. ASME, Ser. E,44, No. 3, 389–395 (1977).
B. M. Efimtsov and S. E. Shubin, “Probability characteristics of pressure pulsations in a boundary layer on the surface of an aircraft,” in: Aeronautical Acoustics, Tr. TsAGI, No. 1655 (1975), pp. 3–14.
P. M. Ogivalov, N. I. Malinin, V. P. Netrebenko, and B. P. Kishkin, Structural Polymers [in Russian], Vol. 1, Moscow State Univ. (1972).
Additional information
Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 40, No. 4, pp. 657–663, April, 1981.
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Airapetov, A.B. One approach to calculating a turbulent boundary layer on a surface with a compliant coating. Journal of Engineering Physics 40, 393–398 (1981). https://doi.org/10.1007/BF00825378
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DOI: https://doi.org/10.1007/BF00825378