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Surrogate-based shape optimization and sensitivity analysis on the aerodynamic performance of HCW configuration 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 152, 页码: 109347./通讯作者：Li GL
Authors:  Xi XZ(席小喆);  Li GL(李广利);  Zhang KK(张凯凯);  Xiao Y(肖尧);  Chang SY(常思源);  Cui K(崔凯)
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High-pressure capturing wing configuration  Surrogate-based optimization  Sensitivity analysis  Hypersonic flow  Aerodynamic performance  
Coupling effect of strain gradient strengthening and thermal softening on the microscale plastic behavior of metallic materials 期刊论文
EUROPEAN JOURNAL OF MECHANICS A-SOLIDS, 2023, 卷号: 102, 页码: 16./通讯作者：Liu, Yanwei
Authors:  Liu, Yanwei;  Long, Hao;  Zhang, Siyuan;  Song JR(宋晶如);  Zhou, Qianqian;  Wei, Yueguang
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Thermo-mechanical coupled  Microscale plasticity model  Plastic strain gradient  Radial return method  Staggered solution scheme  
Multi-scale indentation model of stiff film-compliant substrate structures 期刊论文
APPLIED MATHEMATICAL MODELLING, 2023, 卷号: 119, 页码: 566-585./通讯作者：Wei, YG
Authors:  Liu, Yanwei;  Ma HS(马寒松);  Long, Hao;  Wei, Shiyuan;  Zhang, Siyuan;  Wei, Yueguang
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Multi -scale indentation model  Stiff film -compliant substrate structures  Strain gradient theory  Surface elastic model  Size effect  
翼反角对高压捕获翼构型高超气动特性的影响 期刊论文
航空学报, 2023, 卷号: 44, 期号: 08, 页码: 45-58./通讯作者：肖尧
Authors:  常思源;  肖尧;  李广利;  田中伟;  张凯凯;  崔凯
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高压捕获翼  高超声速  数值模拟  上/下反角  稳定性  
机体尾缘形状对高压捕获翼构型亚声速特性影响 期刊论文
航空学报, 2023, 卷号: 44, 期号: 06, 页码: 10.7527/S1000-6893.2022.27215./通讯作者：肖尧
Authors:  王浩祥;  肖尧;  张凯凯;  李广利;  常思源;  田中伟;  崔凯
Adobe PDF(2111Kb)  |  Favorite  |  View/Download：276/105  |  Submit date：2022/10/17
高压捕获翼  亚声速  流动特性  流动分离  数值模拟  
前缘后掠角对高压捕获翼构型亚声速气动特性影响 会议论文
第十二届全国流体力学学术会议, 中国陕西西安, 2022-11-19
Authors:  张凯凯;  肖尧;  王浩祥;  常思源;  李广利;  田中伟;  崔凯
Adobe PDF(163Kb)  |  Favorite  |  View/Download：194/109  |  Submit date：2023/04/14
高压捕获翼  亚声速  前缘后掠角  气动特性  数值模拟  
Properties of the compressibility and transport motion in wall-bounded turbulent flows at Mach 8 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2022, 卷号: 33, 期号: 7, 页码: 2250090./通讯作者：Zhang, SY (corresponding author), Univ Shanghai Sci & Technol, Sch Mech Engn, Shanghai 200093, Peoples R China.
Authors:  Li, Xin;  Zhang, Siyuan;  Duan JY(段俊亦);  Liu, Xiaobo;  Wu, Wanghao
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Direct numerical simulation  turbulent boundary layer  wall temperature effect  high Mach number  
发动机凸轮轴准工况试验台 专利
发明授权.发动机凸轮轴准工况试验台, 授权公告号: CN103091097B, 申请日期: 2013-01-31, 授权公告日期: 2015-07-29
Inventors:  孔海瑞;  张坤;  郇勇;  王明杰;  程思远;  陈光南
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