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.是什么意思_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.在線(xiàn)翻譯_英語(yǔ)_讀音_用法_例句