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INVISCID: 作品数：56被引量：36H指数：3; 导出分析报告; 相关作者：李杰周洲更多>>; 相关机构：西北工业大学更多>>; 相关期刊：《Advances in Applied Mathematics and Mechanics》《Chinese Physics Letters》《Communications in Computational Physics》《Acta Mathematica Scientia》更多>>; 相关基金：国家自然科学基金国家重点基础研究发展计划福建省自然科学基金国家教育部博士点基金更多>>

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期刊=Chinese Journal of Aeronautics

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Numerical and experimental investigation of quantitative relationship between secondary flow intensity and inviscid blade force in axial compressors: 《Chinese Journal of Aeronautics》2023年第10期101-111,共11页Chenghua ZHOU Zixuan YUE Hanwen GUO Xiwu LIU Donghai JIN Xingmin GUI; the National Science and Technology Major Project,China(Nos.2017-I-0005-0006&2019-II-0020-0041).; The secondary flow attracts wide concerns in the aeroengine compressors since it has become one of the major loss sources in modern high-performance compressors.But the research about the quantitative relationship bet...; 关键词：Axial compressor cascade Corner separation Spanwise inviscid blade force Secondary flow intensity Quantitative correlation

High-order compact finite volume methods on unstructured grids with adaptive mesh refinement for solving inviscid and viscous flows被引量：4: 《Chinese Journal of Aeronautics》2018年第9期1829-1841,共13页Jianhua PAN Qian WANG Yusi ZHANG Yuxin REN; supported by the National Natural Science Foundation of China(Nos.91752114 and 11672160); In the present paper, high-order finite volume schemes on unstructured grids developed in our previous papers are extended to solve three-dimensional inviscid and viscous flows. The highorder variational reconstructio...; 关键词：Adaptive mesh refinement Compact stencil High-order finite volume scheme Unstructured grids Variational reconstruction

Numerical simulation of multi-dimensional inviscid compressible flows by using TV-HLL scheme: 《Chinese Journal of Aeronautics》2016年第6期1553-1562,共10页Pascalin Tiam Kapen Ghislain Tchuen; This paper deals with the numerical solution of inviscid compressible flows. The threedimensional Euler equations describing the mentioned problem are presented and solved numerically with the finite volume method. Th...; 关键词：Euler equations Finite volume method HYPERSONIC Low speed flows Three-dimensional aerodynamics applications Toro Vazquez-Harten Lax Leer(TV-HLL)

A Structured Mesh Euler and Interactive Boundary Layer Method for Wing/Body Configurations: 《Chinese Journal of Aeronautics》2008年第1期19-27,共9页李杰周洲; Aeronautics Science Foundation (2006ZA53009); To compute transonic flows over a complex 3D aircraft configuration, a viscous/inviscid interaction method is developed by coupling an integral boundary-layer solver with an Eluer solver in a ＂semi-inverse＂ manner. ...; 关键词：viscous/inviscid interaction far-field drag prediction transonic flow wing/body configuration

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