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| 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:564/79  |  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:292/83  |  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:104/2  |  提交时间:2023/03/23 |
| 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:140/27  |  提交时间:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |
| Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 14 作者: Zhou, Lin; Teng, Honghui; Ng, Hoi Dick; Yang PF(杨鹏飞); Jiang ZL(姜宗林) Adobe PDF(6382Kb)  |  收藏  |  浏览/下载:217/32  |  提交时间:2021/11/01 Cellular detonation Lead shock evolution Multi-layer perceptron Numerical simulations |
| 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:206/57  |  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:320/168  |  提交时间:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| 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:145/39  |  提交时间:2021/02/01 |
| 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:262/108  |  提交时间:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |