This work is financially supported by the National Key Research and Development Project of China(Grant No.2016YFB0200901);National Natural Science Foundation of China(Grant No.51776154);National Science and Technology Major Project of China(Grant No.2017-II-0006-0020);Shaanxi Key Research and Development Project(Grant No.2018KWZ-01).
Existing aerodynamic design systems for multi-stage axial-flow compressor suffer from several limitations,such as experience dependent models and time costly simulations.Few attempts,however,have been devoted to the r...
Financial supports for the work presented are provided by National Natural Science Foundation of China (Project No: 50806073);China Postdoctoral Science Foundation (Project No: 20070420068);K C Wong Education Foundation, these supports are greatly appreciated
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