已选(0)清除
条数/页: 排序方式: |
| 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 |