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| Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors: Wang Y(王粤) ; Wang YP(汪运鹏); Jiang ZL(姜宗林)
 Adobe PDF(9707Kb) |  Favorite | View/Download：328/95 | Submit date：2022/11/14
Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 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)
Adobe PDF(15045Kb) | Favorite | View/Download：262/29 | Submit date：2022/01/24 |
| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors: Lin MY(林明月); Wang C(王春); Peng J(彭俊); Jiang ZL(姜宗林)
Adobe PDF(4805Kb) | Favorite | View/Download：335/62 | Submit date：2022/01/12 |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童)
Adobe PDF(1806Kb) | Favorite | View/Download：292/63 | Submit date：2021/05/17
Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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)
Adobe PDF(3790Kb) | Favorite | View/Download：410/67 | Submit date：2021/03/03
Hypersonics Shock tunnels Flow characteristics |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors: Zhang ZJ(张子健); Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(3599Kb) | Favorite | View/Download：367/92 | Submit date：2021/03/03
Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |
| 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 |
| 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：196/56 | 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)
Adobe PDF(1551Kb) | Favorite | View/Download：266/79 | Submit date：2020/11/30
Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| 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)
 View | Adobe PDF(1871Kb) | Favorite | View/Download：545/157 | Submit date：2019/09/09
Al particle cellular detonation heat capacity hybrid model |
