Momentum and Heat Transfer in Laminar Boundary Layer Behind Shock Wave

被引:3
|
作者
Zheng, Liancun [1 ]
Zhang, Xinxin [2 ]
He, Jicheng [3 ]
机构
[1] Univ Sci & Technol Beijing, Dept Math & Mech, Beijing 100083, Peoples R China
[2] Univ Sci & Technol Beijing, Sch Mech Engn, Beijing 100083, Peoples R China
[3] Northeastern Univ, Dept Thermal Engn, Shenyang 110006, Peoples R China
关键词
shock wave boundary layer; momentum and heat transfer; analytical solution;
D O I
10.1007/s11630-002-0063-8
中图分类号
O414.1 [热力学];
学科分类号
摘要
Analytical and numerical solutions are established for momentum and energy laminar boundary layer induced by a shock wave. The results indicated that skin friction sigma decreases with increasing in velocity ratio xi(1 <= xi < 6). For each specified xi (1 <= xi < 6), temperature w(t) increases with increasing of T-w but decreases with T-e , and for a range of t is an element of[1, xi], w(t) decreases with the increasing of t. Thermal diffusion increases with increasing of u(w) but decreases with increasing U-e.
引用
收藏
页码:255 / 258
页数:4
相关论文
共 50 条