Features of Heat Transfer on a Permeable Surface in a Compressible-Gas Flow

被引：5
|
作者：
Leont'ev, A. I. [1 ,2 ]
Lushchik, V. G. [1 ]
Makarova, M. S. [1 ]
机构：
[1] Moscow MV Lomonosov State Univ, Res Inst Mech, Moscow 117192, Russia
[2] Bauman Moscow State Tech Univ, Moscow 107005, Russia
来源：
DOKLADY PHYSICS | 2018年 / 63卷 / 09期
基金：
俄罗斯科学基金会;
关键词：
Permeable Surface; Compressible Laminar Boundary Layer; Permeable Plate; Wall Permeability; Impenetrable Wall;
D O I：
10.1134/S1028335818090033
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
A laminar compressible boundary layer on a permeable plate under blowing at small and large Prandtl numbers is investigated numerically. For Prandtl numbers Pr < 1 and the temperature of the gas blown lower than the temperature of the adiabatic impenetrable wall, the calculations carried out confirm the existence of a region of the permeable wall where the temperature is lower than the temperature of the blown gas. For Prandtl numbers Pr > 1 at a blown-gas temperature higher than that of the adiabatic impenetrable wall, the temperature of the permeable wall is higher than that of the blown gas.
引用
收藏
页码：371 / 374
页数：4
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