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| Numerical investigations of the transient cavitating vortical flow structures over a flexible NACA66 hydrofoil 期刊论文 JOURNAL OF HYDRODYNAMICS, 2020, 卷号: 32, 期号: 5, 页码: 865-878 Authors: Huang RF(黄仁芳); Du TZ(杜特专); Wang YW(王一伟); Huang CG(黄晨光) Adobe PDF(4739Kb)  |  Favorite  |  View/Download:352/99  |  Submit date:2020/12/28 Cloud cavitation LARGE-EDDY SIMULATION flexible hydrofoil VORTEX IDENTIFICATION METHODS Ω SPECIAL EMPHASIS method ADDED-MASS flow-induced vibration OMEGA VIBRATION DYNAMICS |
| A multi-time scale solution strategy for an elastomeric aircraft 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13 Authors: Yang L(杨磊); Sun QH(孙泉华) Adobe PDF(1858Kb)  |  Favorite  |  View/Download:231/91  |  Submit date:2020/08/26 Flight dynamic simulation Multi-time scale Elastomeric aircraft Reduced order models Store separation |
| Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition 期刊论文 INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362 Authors: Wang RX(王睿星); Wang, ZW; Zheng HW(郑洪伟); Song HW(宋宏伟) Adobe PDF(4182Kb)  |  Favorite  |  View/Download:315/89  |  Submit date:2020/06/22 Coupled flow-thermal analysis Thermal protection system Basic direct correction method (BDCM) Improved DCM (IDCM) Iteration solution method (ISM) |
| Aeroelastic Simulation Using CFD/CSD Coupling Based on Precise Integration Method 期刊论文 INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 页码: 18 Authors: Huang CD(黄程德); Huang J(黄杰); Song X(宋鑫); Zheng GN(郑冠男); Nie XY(聂雪媛) View  |  Adobe PDF(5463Kb)  |  Favorite  |  View/Download:253/84  |  Submit date:2020/04/07 Flutter Static aeroelasticity CFD CSD coupling Precise integration method |
| An sequential optimization and aeroelastic constraint transformation method for strength-aeroelastic comprehensive design 期刊论文 JOURNAL OF FLUIDS AND STRUCTURES, 2020, 卷号: 93, 页码: 14 Authors: Zhang ZS; Wang XJ; Chen XJ(陈贤佳) View  |  Adobe PDF(2381Kb)  |  Favorite  |  View/Download:320/106  |  Submit date:2020/04/07 Comprehensive design Sequential optimization strategy Airplane wing Structural strength Aeroelasticity |