FAN/COMPRESSOR

作品数：3被引量：31H指数：3
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相关领域：航空宇航科学技术更多>>
相关作者：王静更多>>
相关机构：北京航空航天大学更多>>
相关期刊：《Journal of Thermal Science》《Chinese Journal of Aeronautics》更多>>
相关基金：国家自然科学基金更多>>
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Influence of Non-Axisymmetric Terms on Circumferentially Averaged Method in Fan/Compressor被引量：7
《Journal of Thermal Science》2013年第1期13-22,共10页Ke Wan Hailiang Jin Donghai Jin Xingmin Gui 
supported by National Natural Science Foundation of China (50736007, 51006005)
The governing equations are derived by circumferentially averaging the three-dimensional （3D） Navier-Stokes equations, which are solved using a time marching finite volume approach. Both Euler throughflow model and ...
关键词：throughflow model circumferentiaily averaged non-axisymmetric terms FAN 
Flow Stability Model for Fan/Compressors with Annular Duct and Novel Casing Treatment被引量：14
《Chinese Journal of Aeronautics》2012年第2期143-154,共12页LIU Xiaohua SUN Dakun SUN Xiaofeng WANG Xiaoyu 
National Natural Science Foundation of China (50736007, 50890181);the Innovation Foundation of BUAA for PhD Graduates (300383)
A three-dimensional compressible flow stability model is presented in this paper, which focuses on stall inception of multi-stage axial flow compressors with a finite large radius annular duct configuration for the fi...
关键词：COMPRESSOR STABILITY rotating stall casing treatment EIGENVALUE 
Application of Tandem Cascade to Design of Fan Stator with Supersonic Inflow被引量：10
《Chinese Journal of Aeronautics》2010年第1期9-14,共6页Li Qiushi,Wu Hong,Zhou Sheng School of Jet Propulsion,Beijing University of Aeronautics and Astronautics,Beijing 100191,China 
National Natural Science Foundation of China(10577002);Innovation Foundation of BUAA for PhD Graduates
This article proposes a tandem cascade constructed to tackle the thorny problem of designing the high-loaded stator with a supersonic inflow and a large turning angle. The front cascade adopts a supersonic profile to ...
关键词：FAN/COMPRESSOR tandem cascade STATOR supersonic inflow 
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