A numerical investigation about effects of boundary layer suction in low - speed compressor stator cascade with large turning angle was carried out 摘要本文采用數(shù)值方法研究了低速條件下附面層抽吸對大折轉(zhuǎn)角矩形葉柵流場的影響。
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 除驗(yàn)證各式正確性外并仿真葉片外形對氣流分離、震波/邊界層相互干擾及壓縮比等關(guān)系,以及流體黏滯性等影響下,引擎能量損失與效益分析。
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 除驗(yàn)證各式正確性外并模擬葉片外形對氣流分離、震波/邊界層相互干擾及壓縮比等關(guān)系,以及流體黏滯性等影響下,引擎能量損失與效益分析。