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Research on the effect of channel parameter on the aerodynamic design and performance of two-dimensional high-subsonic compressor cascade

The design of two-dimensional axial compressor cascades is essential to the development of high-performance aero engines; however, there remains no unified guideline for aerodynamic design. In this study, it employed a blade modeling method, introducing the concepts of load distribution coefficient and equivalent chann...

Yi Wang, Zan Yang, Chuangxin Zhou et al. · 0 citations

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