Computational method and CRMBP code, based on Chapman-Korst theory, of supersonic base pressure with an exhaust jet is described and applied to inquire into an experimental technique concerning the jet in wind tunnels.

• 本文简要地叙述了作者发展的基于Chapman-Korst理论的超声速底部压强计算方法及计算程序CRMBP,并用它分析了在风洞中做有关喷流的一种实验方法。