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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 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 |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247 作者: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林) Adobe PDF(2818Kb)  |  收藏  |  浏览/下载:263/108  |  提交时间:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| 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:266/91  |  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:266/102  |  提交时间: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 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 |
| Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342 作者: Meng BQ(孟宝清); Han GL(韩桂来); Luo ZT(罗长童); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(1937Kb)  |  收藏  |  浏览/下载:262/86  |  提交时间:2018/10/30 Hypersonic Shock tunnel Start-up process Impulse force Vibration |
| 气液两相爆轰与气相爆轰绕射的对比与分析 会议论文 北京力学会第17届学术年会, 中国北京, 2011 作者: 戴旭刚; 张德良; 王春; 姜宗林 Adobe PDF(847Kb)  |  收藏  |  浏览/下载:782/183  |  提交时间:2012/04/01 气液两相爆轰 爆轰波 绕射 Ce/se算法 |
| One-Step Direct Aeroacoustic Simulation Using Space-Time Conservation Element and Solution Element Method 会议论文 6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011 作者: Ho CY; Leung RCK; Zhou K; Lam GCY; Jiang ZL(姜宗林) Adobe PDF(400Kb)  |  收藏  |  浏览/下载:495/201  |  提交时间:2014/01/14 Aeroacoustics Caa Ce/se Method Acoustic Wave Supersonic Jet |
| 频散可控格式的一种推广形式及其在爆轰波马赫反射中应用 期刊论文 计算物理, 2005, 卷号: 22, 期号: 3, 页码: 189-196 作者: 常利娜; 张德良; 胡宗民; 姜宗林 Adobe PDF(350Kb)  |  收藏  |  浏览/下载:751/237  |  提交时间:2007/06/15 频散可控格式 非结构网格 爆轰波 |
| The cellular structure of a two-dimensional H2/O2/Ar detonation wave 期刊论文 Combustion Theory and Modelling, 2004, 卷号: 8, 期号: 2, 页码: 339-359 作者: Hu XY; Khoo BC; Zhang DL(张德良); Jiang ZL(姜宗林) Adobe PDF(669Kb)  |  收藏  |  浏览/下载:738/295  |  提交时间:2007/06/15 |