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Analysis of the turbulent boundary layer on a flat plate at M=6÷8.8 with the use of NERAT-2D code and algebraic turbulence models

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, , Citation S T Surzhikov 2018 J. Phys.: Conf. Ser. 1009 012016 DOI 10.1088/1742-6596/1009/1/012016

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surg@ipmnet.ru

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1 Ishlinsky Institute for Problems in Mechanics RAS,Vernadsky prospekt 101(1), Moscow, 119526, Russia

2 Moscow Institute of Physics and Technology (State University), 9 Institutskiy per., Dolgoprudny, Moscow Region, 141701, Russia

3 Dukhov All-Russian Scientific Research Institute of Automatics, Moscow, Russia

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1742-6596/1009/1/012016

Abstract

Experimental data on heat transfer of supersonic air flows to flat plate, which were analysed by Dilley A.D [NASA/CR-2001-210837, 2001], are compared for Mach numbers M = 6 ÷ 8.8 with the calculated data obtained using the Navier – Stokes flow model in conjunction with the analytical models of turbulent mixing of the Prandtl mixing length and the Baldwin-Lomax model. In the paper, the author's computer code NERAT-2D was used for numerical study.

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10.1088/1742-6596/1009/1/012016