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| Understanding of temperature and cooling effectiveness sensitivity of a film-cooled vane under coolant inlet temperature effect: A case study 期刊论文
CASE STUDIES IN THERMAL ENGINEERING, 2019, 卷号: 14, 页码: UNSP 100505
Authors: Prapamonthon P; Yin B(银波) ; Yang GW(杨国伟); Zhang MH
 View |  Adobe PDF(3342Kb) |  Favorite | View/Download：276/85 | Submit date：2020/03/21
TURBINE BLADE HEAT-TRANSFER |
| 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)
 Adobe PDF(1902Kb) | Favorite | View/Download：360/131 | Submit date：2020/03/21
Turbines turbomachinery flow turbomachinery aerodynamics turbine modeling |
| Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors: Zhu JJ; Wang XJ; Zhang HG; Li YW; Wang RX(王睿星); Qiu ZP
Adobe PDF(2082Kb) | Favorite | View/Download：463/197 | Submit date：2020/03/21
Hypersonic vehicle Six sigma robust optimization Successive response surface Thermal protection system 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)
Adobe PDF(3918Kb) | Favorite | View/Download：557/183 | Submit date：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66
Authors: Wang Q(汪球); Olivier H; Einhoff J; Li JP(李进平); Zhao W(赵伟)
Adobe PDF(1085Kb) | Favorite | View/Download：453/105 | Submit date：2019/05/29
Heat transfer measurement Lateral heat conduction Shock tunnel Thermocouple Hypersonic |
| Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
Authors: Zhong K; Yan C; Chen SS; Wang XY(王小永); Ju SJ
Adobe PDF(8635Kb) | Favorite | View/Download：266/74 | Submit date：2019/05/29
Aeroheating Heatshield configuration Sphere-cone angle Mars Turbulent |
| Influences of Domain Symmetry on Supersonic Combustion Modeling 期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
Authors: Yao W(姚卫); Wu K(吴坤); Fan XJ(范学军)
Adobe PDF(862Kb) | Favorite | View/Download：362/108 | Submit date：2019/04/11 |
| Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors: Yuan CK(苑朝凯); Zhou K(周凯); Liu YF(刘云峰); Hu ZM(胡宗民); Jiang ZL(姜宗林)
Adobe PDF(1468Kb) | Favorite | View/Download：374/113 | Submit date：2019/04/11
Spectral measurement Hypervelocity flow Radiation Expansion tunnel |
| CHT/CFD Analysis of Thermal Sensitivity of a Transonic Film-Cooled Guide Vane 期刊论文
CMES-COMPUTER MODELING IN ENGINEERING & SCIENCES, 2019, 卷号: 119, 期号: 3, 页码: 593-615
Authors: Prapamonthon P; Yooyen S; Sleesongsom S
Adobe PDF(3354Kb) | Favorite | View/Download：329/77 | Submit date：2019/09/09
Conjugate heat transfer film cooling thermal sensitivity |
