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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:365/69  |  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:297/85  |  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:105/2  |  提交时间:2023/03/23
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  收藏  |  浏览/下载:280/55  |  提交时间:2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
斜爆轰发动机的推力性能理论分析 期刊论文
力学学报, 2021, 卷号: 53, 期号: 10, 页码: 2853-2864
作者:  杨鹏飞;  张子健;  杨瑞鑫;  滕宏辉;  姜宗林
Adobe PDF(1224Kb)  |  收藏  |  浏览/下载:416/41  |  提交时间:2022/03/16
斜爆轰波  发动机  推力性能  燃烧模式  
A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文
16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安,中国, 19-21 December 2020
作者:  Chen Z(陈阵);  Li S(李森);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
Adobe PDF(1545Kb)  |  收藏  |  浏览/下载:147/39  |  提交时间:2021/02/01
Numerical investigation of wavelet features in rotating detonations with a two-step induction-reaction model 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 7, 页码: 4991-5001
作者:  Teng HH(滕宏辉);  Zhou L;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(2507Kb)  |  收藏  |  浏览/下载:288/95  |  提交时间:2020/04/07
Rotating detonation  Induction-reaction kinetics  Wavelet pattern  Oscillations  
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:392/137  |  提交时间:2019/09/09
Two-phase detonation  CE/SE  Eulerian-Lagrangian  MPI  Aluminum-air detonation  
宽速域下斜爆轰波加速起爆的数值研究 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
作者:  韩信;  张子健;  刘云峰;  姜宗林
Adobe PDF(4511Kb)  |  收藏  |  浏览/下载:423/69  |  提交时间:2019/11/21
斜爆轰波  宽速域  加速起爆  斜爆轰发动机  半圆柱型鼓包  数值模拟  
Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel 期刊论文
JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381
作者:  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
Adobe PDF(1208Kb)  |  收藏  |  浏览/下载:621/130  |  提交时间:2018/10/30
copper calorimeter  high enthalpy shock tunnel  heat transfer  hypersonic