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| Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors: Yao W(姚卫)
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Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |
| The Effects of Laser Parameters and the Ablation Mechanism in Laser Ablation of C/SiC Composite 期刊论文
MATERIALS, 2019, 卷号: 12, 期号: 19, 页码: 14
Authors: Pan SN(潘斯宁); Li QY(李青宇); Xian ZK; Su NGg; Zeng FZ
View | Adobe PDF(4453Kb) | Favorite | View/Download：493/282 | Submit date：2020/03/21
Laser ablation C SiC composite Surface morphology Ablation mechanism Scanning electron microscopy (SEM) |
| 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：270/65 | Submit date：2019/10/21
Aerodynamic force measurement Dynamic system Impact response Cross-validation System identification |
| 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：410/94 | Submit date：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| 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)
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Heat transfer measurement Lateral heat conduction Shock tunnel Thermocouple Hypersonic |
| External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
Authors: Chen H; Tan H; Liu YZ; Zhang QF(张启帆)
View | Adobe PDF(4679Kb) | Favorite | View/Download：277/97 | Submit date：2019/09/09 |
| 大尺度高焓激波风洞喷管设计研究 期刊论文
中国科学:物理学 力学 天文学, 2019, 卷号: 49, 期号: 07, 页码: 63-72
Authors: 唐蓓; 汪运鹏; 姜宗林
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超高速高焓激波风洞 喷管设计 边界层修正 高温气体效应 CFD |
| Numerical study of chemically reacting flow in a shock tube using a high-order point-implicit scheme 期刊论文
COMPUTERS & FLUIDS, 2019, 卷号: 184, 页码: 107-118
Authors: Chen S; Sun QH(孙泉华); Klioutchnikov I; Olivier H
View | Adobe PDF(1365Kb) | Favorite | View/Download：320/120 | Submit date：2019/06/10
Shock wave/boundary-layer interactions Real gas effects Chemical nonequilibrium High-order scheme |
| 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
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Aeroheating Heatshield configuration Sphere-cone angle Mars Turbulent |
| Experimental investigation of liquid film cooling in hypersonic flow 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10
Authors: Yuan CK(苑朝凯); Li JP(李进平); Jiang ZL(姜宗林); Yu HR(俞鸿儒)
View | Adobe PDF(4383Kb) | Favorite | View/Download：447/128 | Submit date：2019/06/10 |
