已选(0)清除
条数/页: 排序方式: |
| 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:255/40  |  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:294/83  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| TSTO马赫7安全级间分离问题的数值研究 期刊论文 力学学报, 2022, 卷号: 54, 期号: 2, 页码: 526-542 作者: 王粤; 汪运鹏; 薛晓鹏; 姜宗林 Adobe PDF(3565Kb)  |  收藏  |  浏览/下载:345/71  |  提交时间:2021/12/23 两级入轨 高超声速 分离流动 气动干扰 级间分离 |
| 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:126/28  |  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 |
| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文 AIAA JOURNAL, 2021, 页码: 12 作者: Lin MY(林明月); Wang C(王春); Peng J(彭俊); Jiang ZL(姜宗林) Adobe PDF(4805Kb)  |  收藏  |  浏览/下载:302/53  |  提交时间:2022/01/12 |
| 超常环境力学领域研究新进展—–《力学学报》极端力学专题研讨会综述报告 期刊论文 力学学报, 2021, 卷号: 53, 期号: 02, 页码: 589-599 作者: 姜宗林; 刘俊丽; 苑朝凯; 陈海璇; 陆夕云 Adobe PDF(532Kb)  |  收藏  |  浏览/下载:270/62  |  提交时间:2021/04/19 极端力学 力学学报 超常环境力学领域 研究进展 研究展望 |
| Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 12 作者: Yuan CK(苑朝凯); Jiang ZL(姜宗林) Adobe PDF(3790Kb)  |  收藏  |  浏览/下载:380/57  |  提交时间:2021/03/03 Hypersonics Shock tunnels Flow characteristics |
| 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 |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文 NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207 作者: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒) Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:252/101  |  提交时间:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |