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.
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释义
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。
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