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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
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：396/75  |  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  
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：316/93  |  Submit date：2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
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：321/58  |  Submit date：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
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：349/90  |  Submit date：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
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：535/154  |  Submit date：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
Authors:  Ma KF(马凯夫);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(1657Kb)  |  Favorite  |  View/Download：275/97  |  Submit date：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
Authors:  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)  |  Favorite  |  View/Download：282/110  |  Submit date：2020/08/26
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)
View  |  Adobe PDF(4374Kb)  |  Favorite  |  View/Download：411/141  |  Submit date：2019/09/09
Two-phase detonation  CE/SE  Eulerian-Lagrangian  MPI  Aluminum-air detonation  
Initiation structure of oblique detonation waves behind conical shocks 期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 8
Authors:  Yang PF(杨鹏飞);  Ng, Hoi Dick;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Teng, HH (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
View  |  Adobe PDF(5788Kb)  |  Favorite  |  View/Download：460/103  |  Submit date：2017/11/16
A reconstructed discontinuous Galerkin method based on a Hierarchical WENO reconstruction for compressible flows on tetrahedral grids 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2013, 卷号: 236, 页码: 477-492
Authors:  Luo H;  Xia YD;  Spiegel S;  Nourgaliev R;  Jiang ZL(姜宗林);  Luo, H (reprint author), N Carolina State Univ, Dept Mech & Aerosp Engn, Raleigh, NC 27695 USA.
Adobe PDF(2739Kb)  |  Favorite  |  View/Download：1375/501  |  Submit date：2013/03/25
Discontinuous Galerkin Method  Weno Reconstruction  Unstructured Grids