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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：363/69 | 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：296/85 | 提交时间：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
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：302/53 | 提交时间：2022/01/12 |
| 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
作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
Adobe PDF(1129Kb) | 收藏 | 浏览/下载：321/168 | 提交时间：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
作者: Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(1551Kb) | 收藏 | 浏览/下载：238/67 | 提交时间：2020/11/30
Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| 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：268/103 | 提交时间：2020/08/26 |
| 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
作者: 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)
Adobe PDF(1090Kb) | 收藏 | 浏览/下载：252/101 | 提交时间：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
作者: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良); Jiang ZL(姜宗林)
 浏览 | Adobe PDF(4374Kb) | 收藏 | 浏览/下载：391/137 | 提交时间：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
作者: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
浏览 | Adobe PDF(2165Kb) | 收藏 | 浏览/下载：396/92 | 提交时间：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者: Wang Q(汪球); Lu P(卢盼); Li JW(栗继伟); Wu S(吴松); Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林)
Adobe PDF(299Kb) | 收藏 | 浏览/下载：83/33 | 提交时间：2023/03/17 |
