Momentum and heat transfer in laminar boundary layer behind shock wave.

Analytical and numerical solutions are established for momentum and energy laminar boundary layer induced by a shock wave. The results indicated that skin friction σ decreases with increasing in velocity ratio ξ (1≤ξ<6). For each specified ξ (1≤ξ <6), temperature w( t) increases with increasing of T _w but decreases with T _e, and for a range of t ε [1, ξ], w( t) decreases with the increasing of t. Thermal diffusion increases with increasing of u _w but decreases with increasing u _e. [ABSTRACT FROM AUTHOR]