In this study, the transonic shock-wave/ boundary-layer interaction and viscous shear stress for the turbine and compressor stator were simulated used the implicit two-factor flux-splitting schemes for solving the thin-layer compressible flow.

• 除验证各式正确性外并仿真叶片外形对气流分离、波/界层相互干扰及压缩比等关系，以及流体黏滞性等影响下，引擎能量损失与效益分析。