A. I. Leont'ev, V. G. Lushchik, A. E. Yakubenko, “The recovery factor in a supersonic flow of gas with a low Prandtl number”, TVT, 2006, Volume 44, Issue 2,Pages <nobr>238

This article is cited in 16 papers

Heat and Mass Transfer and Physical Gasdynamics

The recovery factor in a supersonic flow of gas with a low Prandtl number

A. I. Leont'ev^a, V. G. Lushchik^b, A. E. Yakubenko^c

^a Bauman Moscow State Technical University
^b NPO Energomash, Khimki, Moscow region
^c Institute of Mechanics, M. V. Lomonosov Moscow State University

Abstract: A three-parameter differential model of turbulence supplemented with a transport equation for turbulent heat flux is used to perform calculations of the boundary layer on a heat-insulated wall in a supersonic gas flow with a value of Prandtl number $\mathrm{Pr}\le0.7$. The dependences on the values of Prandtl, Reynolds, and Mach numbers and of intensity of injection are obtained for the recovery factor.

UDC: 533.6

PACS: 44.20.+b,47.11.bc,47.27.te