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| Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18
作者: Yang F(杨帆); Lin MY(林明月); Hu ZM(胡宗民) ; Han GL(韩桂来)
 Adobe PDF(8946Kb) |  收藏 | 浏览/下载：61/1 | 提交时间：2023/11/28
oblique detonation engine cantilevered injection localized high heat flux boundary layer separation reattachment |
| Transitional criterion and hysteresis of multiple shock-shock interference 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 46110
作者: Lin MY(林明月); Yang F(杨帆); Hu ZM(胡宗民); Wang C(王春); Jiang ZL(姜宗林)
Adobe PDF(5430Kb) | 收藏 | 浏览/下载：66/1 | 提交时间：2023/06/15 |
| Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
作者: Peng J(彭俊); Li S(李帅); Yang F(杨帆); Lin MY(林明月); Han GL(韩桂来); Hu ZM(胡宗民)
Adobe PDF(2838Kb) | 收藏 | 浏览/下载：56/0 | 提交时间：2023/04/20
Shock interactions Transitional configuration Aerodynamic heating Shear layer Mach interaction |
| Numerical investigations of the lateral heat transfer in coaxial thermocouples 期刊论文
NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2022, 页码: 19
作者: Qi L(齐力); Han GL(韩桂来); Hu ZM(胡宗民); Wang C(王春); Jiang ZL(姜宗林)
Adobe PDF(3726Kb) | 收藏 | 浏览/下载：238/47 | 提交时间：2022/07/18
Coaxial thermocouples lateral heat transfer maximum temperature point numerical simulation surface heat flux |
| 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
作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
Adobe PDF(1129Kb) | 收藏 | 浏览/下载：313/165 | 提交时间：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
作者: 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) | 收藏 | 浏览/下载：261/107 | 提交时间：2021/01/29
Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| 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
作者: 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) | 收藏 | 浏览/下载：244/100 | 提交时间：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
作者: Yuan CK(苑朝凯); Zhou K(周凯); Hu ZM(胡宗民); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1471Kb) | 收藏 | 浏览/下载：227/55 | 提交时间：2020/07/06 |
| 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
作者: 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)
 浏览 | Adobe PDF(2227Kb) | 收藏 | 浏览/下载：245/56 | 提交时间：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
作者: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
浏览 | Adobe PDF(2165Kb) | 收藏 | 浏览/下载：391/92 | 提交时间：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
