Selected(0)Clear
Items/Page: Sort: |
| Optimal design of E-type coaxial thermocouples for transient heat measurements in shock tunnels 期刊论文 APPLIED THERMAL ENGINEERING, 2023, 卷号: 218, 页码: 11 Authors: Qi L(齐力) ; Han GL(韩桂来) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(5274Kb)  |   Favorite  |  View/Download:211/10  |  Submit date:2022/11/21 Coaxial thermocouples Lateral heat conduction Maximum temperature point Optimal design Numerical simulation |
| Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels 期刊论文 APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8 Authors: Han GL(韩桂来) ; Qi L(齐力) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(1715Kb)  |   Favorite  |  View/Download:293/49  |  Submit date:2022/11/08 Heat flux Measurement Data processing Error Approximate solution |
| Numerical investigations of the lateral heat transfer in coaxial thermocouples 期刊论文 NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2022, 页码: 19 Authors: Qi L(齐力) ; Han GL(韩桂来) ; Hu ZM(胡宗民) ; Wang C(王春) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(3726Kb)  |   Favorite  |  View/Download:297/67  |  Submit date:2022/07/18 Coaxial thermocouples lateral heat transfer maximum temperature point numerical simulation surface heat flux |
| Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文 AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17 Authors: Zhang WS(张文硕) ; Zhang, Zijian; Jiang ZL(姜宗林) ; Han X(韩信); Liu YF(刘云峰); Wang C(王春)![](/image/person.jpg)
Adobe PDF(15045Kb)  |   Favorite  |  View/Download:270/31  |  Submit date:2022/01/24 |
| Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 12 Authors: Yuan CK(苑朝凯) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(3790Kb)  |   Favorite  |  View/Download:421/74  |  Submit date:2021/03/03 Hypersonics Shock tunnels Flow characteristics |
| 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)![](/image/person.jpg)
Adobe PDF(1129Kb)  |   Favorite  |  View/Download:356/178  |  Submit date:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Cellular Aluminum Particle-Air Detonation Based on Realistic Heat Capacity Model 期刊论文 COMBUSTION SCIENCE AND TECHNOLOGY, 2020, 卷号: 192, 期号: 10, 页码: 1931-1945 Authors: Xiang GX(项高翔); Yang PF(杨鹏飞); Teng HH(滕宏辉) ; Jiang ZL(姜宗林)![](/image/person.jpg)
View  |   Adobe PDF(1871Kb)  |   Favorite  |  View/Download:554/160  |  Submit date:2019/09/09 Al particle cellular detonation heat capacity hybrid model |
| 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)![](/image/person.jpg)
Adobe PDF(1090Kb)  |   Favorite  |  View/Download:278/101  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文 JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40 Authors: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(4374Kb)  |   Favorite  |  View/Download:425/146  |  Submit date:2019/09/09 Two-phase detonation CE/SE Eulerian-Lagrangian MPI Aluminum-air detonation |
| 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)![](/image/person.jpg)
Adobe PDF(2165Kb)  |   Favorite  |  View/Download:423/99  |  Submit date:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |