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| 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 |
| 激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文 航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126 作者: 王粤; 汪运鹏; 姜宗林 Adobe PDF(6797Kb)  |  收藏  |  浏览/下载:346/35  |  提交时间:2022/12/01 两级入轨 轨迹捕获 激波风洞 多体分离 动态试验 试验技术 |
| 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:175/1  |  提交时间:2022/11/21 Coaxial thermocouples Lateral heat conduction Maximum temperature point Optimal design Numerical simulation |
| 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 |
| 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:252/39  |  提交时间:2022/11/08 Heat flux Measurement Data processing Error Approximate solution |
| 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:291/83  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 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:305/81  |  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 |
| 卷积神经网络在风洞天平静态校准中的应用分析 期刊论文 空气动力学学报, 2022, 卷号: 40, 期号: 暂无, 页码: 1-8 作者: 汪运鹏; 聂少军; 王粤; 姜宗林 Adobe PDF(1217Kb)  |  收藏  |  浏览/下载:134/35  |  提交时间:2022/10/17 气动力测量 风洞应变天平 静态校准 深度学习 卷积神经网络 |
| 高超声速高焓条件下的内嵌式温敏漆测量方法 期刊论文 力学学报, 2022, 卷号: 54, 期号: 01, 页码: 48-58 作者: 苑朝凯; 姜宗林 Adobe PDF(1381Kb)  |  收藏  |  浏览/下载:125/28  |  提交时间:2022/03/16 温敏漆 热流密度场 辐射效应 高超声速流动 辨识方法 |
| 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 |