Analysis of the turbulent boundary layer on a flat plate at M=6 divided by 8.8 with the use of NERAT-2D code and algebraic turbulence modelsстатья
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Дата последнего поиска статьи во внешних источниках: 6 декабря 2018 г.
Аннотация: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 divided by 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.