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| 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 |
| 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 |
| 一种并联两级入轨飞行器纵向分离方案的数值研究 期刊论文 航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634 作者: 王粤; 汪运鹏; 王春; 姜宗林 Adobe PDF(4901Kb)  |  收藏  |  浏览/下载:566/79  |  提交时间:2022/07/11 两级入轨 高超声速 纵向分离 气动干扰 非定常流动 |
| 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 |
| Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2554Kb)  |  收藏  |  浏览/下载:141/28  |  提交时间:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |
| 激波风洞高低压段钢膜片破裂特性研究 期刊论文 力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1747-1757 作者: 聂少军; 汪运鹏; 薛晓鹏; 姜宗林 Adobe PDF(7665Kb)  |  收藏  |  浏览/下载:231/61  |  提交时间:2021/11/12 激波风洞 主膜片 爆轰驱动 破裂特性 数值模拟 |
| 高超声速喷管设计理论与方法 期刊论文 力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294 作者: 汪运鹏; 姜宗林 Adobe PDF(2086Kb)  |  收藏  |  浏览/下载:207/57  |  提交时间:2021/01/29 |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:321/168  |  提交时间:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| 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 |
| Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文 SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2149Kb)  |  收藏  |  浏览/下载:182/53  |  提交时间:2020/12/28 artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |