IMECH-IR

Browse/Search Results:  1-10 of 64 Help

Filters                        
Selected(0)Clear Items/Page:    Sort:
Objective Functions and Performance Optimization of Ocean Thermal Energy Conversion (OTEC) with CO2-Based Binary Zeotropic Mixture Power Cycle 期刊论文
JOURNAL OF MARINE SCIENCE AND ENGINEERING, 2023, 卷号: 11, 期号: 1, 页码: 14
Authors:  Shi, Weixiu;  Sun, Yin;  Pan LS(潘利生);  Song, Linjian;  Wei XL(魏小林)
Adobe PDF(1912Kb)  |  Favorite  |  View/Download:152/12  |  Submit date:2023/03/08
Ocean Thermal Energy Conversion (OTEC)  CO2-based mixture  objective function  working fluid optimization  application occasion  evaporating temperature  
Experimental investigation of combustion-induced starting hysteresis in the scramjet 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 9, 页码: 96103
Authors:  Zhang QF(张启帆);  Chen H(陈昊);  Wu ZJ(吴振杰);  Gao ZB(高占彪);  Luo WH(罗苇航);  Gu HB(顾洪斌);  Yue LJ(岳连捷)
Adobe PDF(2852Kb)  |  Favorite  |  View/Download:170/56  |  Submit date:2022/10/23
Starting and running performance of a pulsating heat pipe with micro encapsulated phase change material suspension 期刊论文
APPLIED THERMAL ENGINEERING, 2022, 卷号: 212, 页码: 9
Authors:  Shi, Weixiu;  Chen, Hongdi;  Pan LS(潘利生);  Wang, Qian
Adobe PDF(2643Kb)  |  Favorite  |  View/Download:254/65  |  Submit date:2022/07/18
Pulsating heat pipe (PHP)  Micro encapsulated phase change material   (MEPCM)  Starting performance  Running performance  
Energy-based drag decomposition analyses for a turbulent channel flow developing over convergent-divergent riblets 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 2, 页码: 16
Authors:  Guo TB(郭同彪);  Fang,Jian;  Zhong,Shan;  Moulinec,Charles
Adobe PDF(9532Kb)  |  Favorite  |  View/Download:256/78  |  Submit date:2022/03/28
Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:  Zhang WS(张文硕);  Zhang, Zijian;  Jiang ZL(姜宗林);  Han X(韩信);  Liu YF(刘云峰);  Wang C(王春)
Adobe PDF(15045Kb)  |  Favorite  |  View/Download:267/30  |  Submit date:2022/01/24
Error Analysis of Integrated Absorbance for TDLAS in a Nonuniform Flow Field 期刊论文
APPLIED SCIENCES-BASEL, 2021, 卷号: 11, 期号: 22, 页码: 15
Authors:  Li RJ(李仁杰);  Li F(李飞);  Lin X(林鑫);  Yu XL(余西龙)
Adobe PDF(7410Kb)  |  Favorite  |  View/Download:261/47  |  Submit date:2022/01/13
TDLAS  integrated absorbance  error analysis  
Optimization of 4D flow MRI velocity field in the aorta with divergence-free smoothing 期刊论文
MEDICAL & BIOLOGICAL ENGINEERING & COMPUTING, 2021, 卷号: 59, 期号: 11-12, 页码: 2237-2252
Authors:  Gao, Qi;  Liu, Xingli;  Wang, Hongping;  Wu, Peng;  Jin, Mansu;  Wei, RunJie;  Wang, Wei;  Niu, Zhaozhuo;  Zhao, Shihua;  Li F(李飞)
Adobe PDF(5562Kb)  |  Favorite  |  View/Download:183/92  |  Submit date:2022/10/25
4D flow MRI  Computational fluid dynamics  Wall shear stress  Divergence-free smoothing  
Shock wave and turbulent boundary layer interaction in a double compression ramp 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 15
Authors:  Tong FL(童福林);  Duan JY(段俊亦);  Li XL(李新亮)
Adobe PDF(10792Kb)  |  Favorite  |  View/Download:293/46  |  Submit date:2021/11/01
Shock wave  Turbulent boundary layer  Double compression ramp  Direct numerical simulation  
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
Adobe PDF(8841Kb)  |  Favorite  |  View/Download:290/109  |  Submit date:2021/11/01
Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
Authors:  Yang L(杨磊);  Ye, Zhengyin;  Li WH(李文皓);  Sun QH(孙泉华)
Adobe PDF(4621Kb)  |  Favorite  |  View/Download:287/63  |  Submit date:2021/11/01
Store separation  Aerodynamic modeling  Interference aerodynamics  Dynamic simulation  Air-launch-to-orbit