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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：361/179 | Submit date：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| 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)
Adobe PDF(2818Kb) | Favorite | View/Download：327/120 | Submit date：2021/01/29
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：211/62 | 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)
Adobe PDF(1551Kb) | Favorite | View/Download：287/86 | Submit date：2020/11/30
Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| Effects of Different Particle Size Distributions on Aluminum Particle-Air Detonation 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 7, 页码: 3115-3128
Authors: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良); Jiang ZL(姜宗林)
Adobe PDF(2342Kb) | Favorite | View/Download：307/117 | Submit date：2020/08/26 |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒)
Adobe PDF(1090Kb) | Favorite | View/Download：285/102 | Submit date：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
