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| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 作者: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童) Adobe PDF(1806Kb)  |  收藏  |  浏览/下载:278/54  |  提交时间:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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:142/38  |  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 |
| 基于物理过程的高超声速风洞实验干扰信号消除方法 会议论文 中国力学大会, 中国浙江杭州, 2019年8月25-28日 作者: 李帅; 罗长童; 姜宗林 浏览  |  Adobe PDF(1822Kb)  |  收藏  |  浏览/下载:200/42  |  提交时间:2019/11/21 可控样条 滤波方法 机器学习 热流信号 高超声速 |
| Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文 EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478 作者: Luo ZT(罗长童); Wang YP(汪运鹏); Hu ZM(胡宗民); Li JP(李进平); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(2227Kb)  |  收藏  |  浏览/下载:249/57  |  提交时间:2019/10/21 Aerodynamic force measurement Dynamic system Impact response Cross-validation System identification |
| Aerodynamic Force Measurement in a Large-Scale Shock Tunnel 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 作者: Wang YP(汪运鹏); Liu YF(刘云峰); Luo ZT(罗长童); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(556Kb)  |  收藏  |  浏览/下载:157/40  |  提交时间:2020/01/06 |
| A Multi-space Interrelation Theory for Correlating Aerodynamic Data from Hypersonic Ground Testing 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 作者: Jiang ZL(姜宗林); Luo ZT(罗长童) 浏览  |  Adobe PDF(377Kb)  |  收藏  |  浏览/下载:140/30  |  提交时间:2020/01/06 |
| A Fast Mathematical Modeling Method for Aerodynamic-Heating Predictions 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 作者: Luo ZT(罗长童); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(252Kb)  |  收藏  |  浏览/下载:162/33  |  提交时间:2020/01/06 |
| Aerodynamic Force Measurement Techniques in JF12 Shock Tunnel 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 作者: Liu YF(刘云峰); Wang YP(汪运鹏); Yuan CK(苑朝凯); Luo ZT(罗长童); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(532Kb)  |  收藏  |  浏览/下载:185/65  |  提交时间:2020/01/06 |
| Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342 作者: Meng BQ(孟宝清); Han GL(韩桂来); Luo ZT(罗长童); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(1937Kb)  |  收藏  |  浏览/下载:262/86  |  提交时间:2018/10/30 Hypersonic Shock tunnel Start-up process Impulse force Vibration |