Numerical Study of the Turbulent Boundary Layer with an Adverse Pressure Gradient in Compressible Gas Flow

被引：0

作者：

V. G. Lushchik ^{[1
]}

S. S. Popovich ^{[1
]}

机构：

[1] Moscow State University,

[2] Institute of Mechanics,undefined

来源：

Fluid Dynamics | 2025年 / 60卷 / 1期

关键词：

RANS turbulence model; adverse pressure gradient; friction coefficient; Mach number; temperature factor; temperature recovery factor; Reynolds analogy;

D O I：

10.1134/S0015462824604583

中图分类号：

学科分类号：

摘要：

引用