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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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  收藏  |  浏览/下载:361/69  |  提交时间: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  
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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9707Kb)  |  收藏  |  浏览/下载:287/82  |  提交时间:2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
作者:  Jiang ZL(姜宗林);  Teng, Honghui
Adobe PDF(13641Kb)  |  收藏  |  浏览/下载:101/2  |  提交时间:2023/03/23
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
作者:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
Adobe PDF(4805Kb)  |  收藏  |  浏览/下载:293/49  |  提交时间:2022/01/12
Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
作者:  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)  |  收藏  |  浏览/下载:323/88  |  提交时间:2021/03/03
Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation  
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
作者:  Xiang GX(项高翔);  Yang PF(杨鹏飞);  Teng HH(滕宏辉);  Jiang ZL(姜宗林)
Adobe PDF(1871Kb)  |  收藏  |  浏览/下载:500/142  |  提交时间:2019/09/09
Al particle  cellular detonation  heat capacity  hybrid model  
Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
作者:  Ma KF(马凯夫);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(1657Kb)  |  收藏  |  浏览/下载:263/90  |  提交时间:2020/08/26
Scramjet engines  Shock-induced combustion ramjet engines  Supersonic combustion  Chapman-Jouguet detonation  
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
作者:  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)  |  收藏  |  浏览/下载:261/100  |  提交时间:2020/08/26
Simulation of shear layers interaction and unsteady evolution under different double backward-facing steps 期刊论文
Theoretical and Applied Mechanics Letters, 2020, 卷号: 10, 页码: 224-229
作者:  Deng F(邓芳);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Adobe PDF(1546Kb)  |  收藏  |  浏览/下载:167/42  |  提交时间:2021/06/11
Interaction  Jet  Numerical simulation  Shear layer  Unsteady evolution  
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
作者:  Zhang ZJ(张子健);  Wen CY;  Liu YF(刘云峰);  Zhang DL(张德良);  Jiang ZL(姜宗林)
Adobe PDF(4374Kb)  |  收藏  |  浏览/下载:382/132  |  提交时间:2019/09/09
Two-phase detonation  CE/SE  Eulerian-Lagrangian  MPI  Aluminum-air detonation