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| 高超声速喷管设计理论与方法 期刊论文
力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294
Authors: 汪运鹏 ; 姜宗林
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| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
Adobe PDF(1129Kb) | Favorite | View/Download：351/177 | Submit date：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430
Authors: Jiang YZ; Wen CY; Zhang DL(张德良)
Adobe PDF(6207Kb) | Favorite | View/Download：261/101 | Submit date：2021/02/09 |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247
Authors: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林)
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Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文
SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2149Kb) | Favorite | View/Download：195/56 | Submit date：2020/12/28
artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |
| Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors: Wang YP(汪运鹏); Jiang ZL(姜宗林)
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Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | Favorite | View/Download：274/116 | Submit date：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Design of a new supersonic biplane 期刊论文
Acta Astronautica, 2020, 卷号: 175, 期号: 10, 页码: 216-233
Authors: Zhai J; Zhang CA(张陈安); Wang FM(王发民); Zhang WW
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| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
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Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements 期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
Authors: Zhang SZ(张仕忠); Wang Q(汪球); Li JP(李进平); Zhang XY(张晓源); Chen H(陈宏)
Adobe PDF(8566Kb) | Favorite | View/Download：205/50 | Submit date：2020/11/30
calorimeter shock tunnel heat transfer measurement hypersonic |
