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| Efficient strategy for reliability-based optimization design of multidisciplinary coupled system with interval parameters 期刊论文 APPLIED MATHEMATICAL MODELLING, 2019, 卷号: 75, 页码: 349-370 Authors: Wang RX(王睿星); Luo Y View  |  Adobe PDF(4483Kb)  |  Favorite  |  View/Download:244/87  |  Submit date:2019/11/25 Multidisciplinary design optimization Non-probabilistic reliability Uncertainty propagation analysis Gradient information Interval reliability displacement |
| Tip leakage flow analysis of an axial turbine under the effect of separation at low Reynolds number 期刊论文 PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2019, 页码: 15 Authors: Shao ZY; Li W; Zhu YL; Wang X; Zhang XH; Chen HS; Qin W(秦伟) View  |  Adobe PDF(1902Kb)  |  Favorite  |  View/Download:331/121  |  Submit date:2020/03/21 Turbines turbomachinery flow turbomachinery aerodynamics turbine modeling |
| Mechanical design and multifunctional applications of chiral mechanical metamaterials: A review 期刊论文 MATERIALS & DESIGN, 2019, 卷号: 180, 页码: 13 Authors: Wu WW; Hu WX; Qian GA(钱桂安); Liao HT; Xu XY; Berto F View  |  Adobe PDF(3503Kb)  |  Favorite  |  View/Download:401/165  |  Submit date:2019/10/14 Chiral Mechanical metamaterials Auxetics Multifunctional |
| Finite obstacle effect on the aerodynamic performance of a hovering wing 期刊论文 PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 10, 页码: 12 Authors: Yin B(银波); Yang GW(杨国伟); Prapamonthon P View  |  Adobe PDF(5326Kb)  |  Favorite  |  View/Download:249/88  |  Submit date:2020/03/11 |
| A nonlinear model for aerodynamic configuration of wake behind horizontal-axis wind turbine 期刊论文 APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2019, 卷号: 40, 期号: 9, 页码: 1313-1326 Authors: Li DS; Guo T; Li RN; Yang CX; Cheng ZX; Li Y; Hu WR(胡文瑞) View  |  Adobe PDF(1504Kb)  |  Favorite  |  View/Download:183/74  |  Submit date:2019/10/21 nonlinear wake aerodynamic model vortex-induced velocity integral equation of vortex-induced velocity horizontal-axis wind turbine O355 |
| Construction of bi-layer biluminophore fast-responding pressure sensitive coating for non-contact unsteady aerodynamic testing 期刊论文 POLYMER TESTING, 2019, 卷号: 77, 页码: 8 Authors: Yang D; Ren JK; Li JW(栗继伟); Wang QL; Wang Q(汪球); Xie Z; Qu XZ View  |  Adobe PDF(2608Kb)  |  Favorite  |  View/Download:1039/798  |  Submit date:2019/11/25 Pressure sensitive paint (PSP) Bi-layer structured coating Fast-response Self-referenced measurement |
| Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文 EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478 Authors: Luo ZT(罗长童); Wang YP(汪运鹏); Hu ZM(胡宗民); Li JP(李进平); Jiang ZL(姜宗林) View  |  Adobe PDF(2227Kb)  |  Favorite  |  View/Download:277/67  |  Submit date:2019/10/21 Aerodynamic force measurement Dynamic system Impact response Cross-validation System identification |
| Comparison of the reliability-based and safety factor methods for structural design 期刊论文 APPLIED MATHEMATICAL MODELLING, 2019, 卷号: 72, 页码: 68-84 Authors: Wang XJ; Shi QH; Fan WC; Wang RX(王睿星); Wang L View  |  Adobe PDF(1921Kb)  |  Favorite  |  View/Download:362/80  |  Submit date:2019/09/09 Safety factor method Reliability-based design optimization Structural design Uncertainty |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇) View  |  Adobe PDF(3918Kb)  |  Favorite  |  View/Download:542/174  |  Submit date:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306 Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林) View  |  Adobe PDF(2165Kb)  |  Favorite  |  View/Download:415/95  |  Submit date:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |