Investigation of a Compressible Laminar Boundary Layer on a Permeable Plate with Uniform Injection for Gas Prandtl Numbers Pr = 0.1…1.0

被引：0

作者：

A. I. Leontiev

V. G. Lushchik

M. S. Makarova

机构：

[1] Moscow State University,

[2] Institute of Mechanics,undefined

[3] Bauman Moscow State Technical University,undefined

来源：

Doklady Physics | 2022年 / 67卷

关键词：

adiabatic wall; critical injection; Prandtl number; laminar compressible boundary layer;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：27 / 31

页数：4

共 23 条

[1] Investigation of a Compressible Laminar Boundary Layer on a Permeable Plate with Uniform Injection for Gas Prandtl Numbers Pr=0.1 horizontal ellipsis 1.0
Leontiev, A. I.
Lushchik, V. G.
Makarova, M. S.
[J]. DOKLADY PHYSICS, 2022, 67 (01) : 27 - 31
[2] Compressible turbulent boundary layer on a permeable plate with injection of foreign gas
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[3] Compressible turbulent boundary layer on a permeable plate with injection of foreign gas
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[J]. High Temperature, 2007, 45 : 488 - 496
[4] LAMINAR BOUNDARY LAYER WITH UNIFORM INJECTION OF A FOREIGN GAS
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[8] Distinctive features of heat transfer on a permeable surface in a laminar compressible gas flow at Prandtl number Pr < 1
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Makarova, M. S.
[J]. INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2020, 147
[9] HEAT TRANSFER IN LAMINAR COMPRESSIBLE BOUNDARY LAYER ON A POROUS FLAT PLATE WITH FLUID INJECTION
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[10] FOREIGN-GAS INJECTION INTO A COMPRESSIBLE TURBULENT BOUNDARY LAYER ON A FLAT PLATE
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