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Application of Simple Gradient-Based Method and Multi-Section Blade Parameterization Technique to Aerodynamic Design Optimization of a 3D Transonic Single Rotor Compressor 会议论文
ASME:Turbomachinery: Design Methods & CFD Modeling for Turbomachinery, 2009
N. X. Chen, H. W. Zhang, Q. Xu, and W. G. Huang
收藏  |  浏览/下载:8/0  |  提交时间:2011/11/30
Application of Simple Gradient-Based Method and Multi-Section Blade Parameterization Technique to Aerodynamic Design Optimization of a 3D Transonic Single Rotor Compressor 会议论文
2009
作者:  N. X. Chen, H. W. Zhang, Q. Xu, and W. G. Huang
收藏  |  浏览/下载:5/0  |  提交时间:2011/11/30
Effect of Maximum Camber Location on Aerodynamic Performance of Transonic Compressor Blades 会议论文
ASME:TURBOMACHINERY: DESIGN METHODS AND CFD MODELING FOR TURBOMACHINERY, 2005
N. X. Chen, H. W. Zhang, H. Du, Y. J. Xu, and W. G. Huang
收藏  |  浏览/下载:7/0  |  提交时间:2011/11/28


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