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Standing oblique detonation for hypersonic propulsion: A review 期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
作者:  Jiang ZL(姜宗林)
Adobe PDF(10386Kb)  |  收藏  |  浏览/下载:31/2  |  提交时间:2024/02/26
Standing oblique detonation  Scramjet engine  Oblique detonation engine  Shock wave  Supersonic combustion  Hypersonic ramjet propulsion  
Force measurement using strain-gauge balance in shock tunnel based on deep learning 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53
作者:  Nie SJ(聂少军);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2346Kb)  |  收藏  |  浏览/下载:21/2  |  提交时间:2024/02/26
Convolutional neural net-works  Deep learning  Frequency domain analysis  Force measurement  Time domain analysis  Recurrent neural networks  
Characteristics of cellular structure of detonation waves propagating in annular channels 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13
作者:  Yao KP(姚克鹏);  Yang PF(杨鹏飞);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(8005Kb)  |  收藏  |  浏览/下载:25/2  |  提交时间:2024/02/19
Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration 期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(7258Kb)  |  收藏  |  浏览/下载:76/15  |  提交时间:2024/01/15
Two-stage-to-orbit  Wind tunnel test  Numerical simulation  Stage separation  Hypersonic  Shock waves  
Experimental demonstration of forced initiation of kerosene oblique detonation by an on-wedge trip in an ODE model 期刊论文
COMBUSTION AND FLAME, 2023, 卷号: 258, 页码: 6
作者:  Han X(韩信);  Liu YF(刘云峰);  Zhang, Zijian;  Zhang WS(张文硕);  Yuan CK(苑朝凯);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Adobe PDF(1092Kb)  |  收藏  |  浏览/下载:70/4  |  提交时间:2023/11/28
Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 8, 页码: 86124
作者:  Wang DG(王大高);  Han GL(韩桂来);  Liu MK(刘美宽);  Jiang ZL(姜宗林)
Adobe PDF(10056Kb)  |  收藏  |  浏览/下载:49/0  |  提交时间:2023/09/26
Transitional criterion and hysteresis of multiple shock-shock interference 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 46110
作者:  Lin MY(林明月);  Yang F(杨帆);  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5430Kb)  |  收藏  |  浏览/下载:70/3  |  提交时间:2023/06/15
Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9327Kb)  |  收藏  |  浏览/下载:191/62  |  提交时间:2023/05/26
Two-stage-to-orbit  Hypersonic  Numerical simulation  Stage separation  Aerodynamic interaction  Unsteady flow  Center of gravity  
Characteristics of reattached oblique detonation induced by a double wedge 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 3, 页码: 36112
作者:  Yao KP(姚克鹏);  Yang PF(杨鹏飞);  Li HY(李昊洋);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(2986Kb)  |  收藏  |  浏览/下载:95/3  |  提交时间:2023/04/20
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:104/2  |  提交时间:2023/03/23
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
Influence of Dual Ignition on Test Conditions of a High-Enthalpy Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Wang Q(汪球);  Zhao W(赵伟);  Li JW(栗继伟);  Li JP(李进平);  Lu P(卢盼);  Jiang ZL(姜宗林)
Adobe PDF(240Kb)  |  收藏  |  浏览/下载:55/25  |  提交时间:2023/03/17
Divide and Conquer: A Quick Scheme for Symbolic Regression 期刊论文
INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2022, 卷号: 19, 期号: 08, 页码: 25
作者:  Luo ZT(罗长童);  Chen C(陈辰);  Jiang ZL(姜宗林)
Adobe PDF(204Kb)  |  收藏  |  浏览/下载:154/34  |  提交时间:2023/02/07
Symbolic regression  machine learning  divide and conquer  bi-correlation test  mathematical modeling  genetic programming  
Numerical investigation on unsteady interaction of oblique/bow shock during rotation based on non-inertial coordinate system 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 12, 页码: 9
作者:  Wang DG(王大高);  Han GL(韩桂来);  Liu MK(刘美宽);  Jiang ZL(姜宗林)
Adobe PDF(3151Kb)  |  收藏  |  浏览/下载:191/39  |  提交时间:2023/02/03
Experimental study on the effects of the cone nose-tip bluntness 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 10, 页码: 7
作者:  Liu MK(刘美宽);  Han GL(韩桂来);  Li, Zongxian;  Jiang ZL(姜宗林)
Adobe PDF(2020Kb)  |  收藏  |  浏览/下载:165/46  |  提交时间:2022/12/29
Optimal design of E-type coaxial thermocouples for transient heat measurements in shock tunnels 期刊论文
APPLIED THERMAL ENGINEERING, 2023, 卷号: 218, 页码: 11
作者:  Qi L(齐力);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Adobe PDF(5274Kb)  |  收藏  |  浏览/下载:177/2  |  提交时间:2022/11/21
Coaxial thermocouples  Lateral heat conduction  Maximum temperature point  Optimal design  Numerical simulation  
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  
Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels 期刊论文
APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8
作者:  Han GL(韩桂来);  Qi L(齐力);  Jiang ZL(姜宗林)
Adobe PDF(1715Kb)  |  收藏  |  浏览/下载:256/40  |  提交时间:2022/11/08
Heat flux  Measurement  Data processing  Error  Approximate solution  
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  
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  收藏  |  浏览/下载:306/81  |  提交时间:2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering