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激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors:  王粤;  汪运鹏;  姜宗林
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两级入轨  轨迹捕获  激波风洞  多体分离  动态试验  试验技术  
Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 8, 页码: 86124
Authors:  Wang DG(王大高);  Han GL(韩桂来);  Liu MK(刘美宽);  Jiang ZL(姜宗林)
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Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9327Kb)  |  Favorite  |  View/Download：233/72  |  Submit date：2023/05/26
Two-stage-to-orbit  Hypersonic  Numerical simulation  Stage separation  Aerodynamic interaction  Unsteady flow  Center of gravity  
一种并联两级入轨飞行器纵向分离方案的数值研究 期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
Authors:  王粤;  汪运鹏;  王春;  姜宗林
Adobe PDF(4901Kb)  |  Favorite  |  View/Download：628/99  |  Submit date：2022/07/11
两级入轨  高超声速  纵向分离  气动干扰  非定常流动  
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  Favorite  |  View/Download：468/89  |  Submit date：2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
A theoretical method for solving shock relations coupled with chemical equilibrium and its applications 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:  Zhang, Zijian;  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Chemical equilibrium  Detonation  Dissociated air  Shock relation  Theoretical solution  
Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
Authors:  Jiang ZL(姜宗林);  Teng, Honghui
Adobe PDF(13641Kb)  |  Favorite  |  View/Download：133/2  |  Submit date：2023/03/23
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)
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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：363/179  |  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)
View  |  Adobe PDF(1871Kb)  |  Favorite  |  View/Download：570/167  |  Submit date：2019/09/09
Al particle  cellular detonation  heat capacity  hybrid model