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

被引：0
|
作者：
A. I. Leontiev
V. G. Lushchik
A. E. Yakubenko
机构：
[1] Bauman Moscow State Technical University,Institute of Mechanics
[2] NPO Glushko Energomash,undefined
[3] Moscow State University,undefined
来源：
High Temperature | 2006年 / 44卷
关键词：
Physical Chemistry; Boundary Layer; Heat Flux; Mach Number; Plasma Physics;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
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 Pr ≤ 0.7. The dependences on the values of Prandtl, Reynolds, and Mach numbers and of intensity of injection are obtained for the recovery factor.
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页码：234 / 242
页数：8
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