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采用非交错网格压力修正法计算不可压及可压亚、跨、超音速流动 被引量:1

A NON-STAGGERED PRESSURE-BASED METHOD FOR FLOW CALCULATION AT ALL SPEEDS
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摘要 采用非交错网格压力修正法计算不可压及可压亚、跨、超音速流动朱斌,蔡睿贤,蒋洪德(中国科学院工程热物理研究所北京100080)关键词:压力修正法,亚、跨、超音速流动一、前言源于计算不可压流动的压力修正方法,由于具有计算时间短及不受马赫数限制的优点,近年... A non-staggered pressure correction numerical method has been developed to calculate both incompressible and compressible flows at all speeds. The pressure oscillation is solved by a special treatment of pressure interpolation on collocated grids, with all variables being located at the center of the control volume. Both convection and diffusion terms of the governing equations are discretized with the second-order central differencing scheme. The method is verified on a number of test cases, and the results compare favourably with other numerical results.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 1994年第3期284-287,共4页 Journal of Engineering Thermophysics
关键词 压力修正法 超音速流动 亚音速流动 pressure correction, subsonic, transonic and supersonic flow.
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  • 1[1]航空航天部高效节能发动机编委会.见:高效节级发动机文集第三分册,风扇、压气机设计与制造.航空工业出版社,1991

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