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| 不同大气条件下超声速降落伞系统气动特性分析 期刊论文 航天返回与遥感, 2020, 卷号: 41, 期号: 06, 页码: 77-89 作者: 姜璐璐; 林明月; 薛晓鹏; 贾贺; 荣伟; 王奇 Adobe PDF(6000Kb)  |  收藏  |  浏览/下载:300/48  |  提交时间:2021/01/29 火星大气 超声速降落伞 气动干扰 数值模拟 火星探测器 |
| 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:139/36  |  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:261/107  |  提交时间:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
| Unsteady combustion mode with a super-high frequency induced by a curved shock 期刊论文 PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 11, 页码: 116101 作者: Teng HH(滕宏辉); Liu S; Zhang ZJ(张子健) Adobe PDF(5194Kb)  |  收藏  |  浏览/下载:249/67  |  提交时间:2020/12/28 PROJECTILE MECHANISM SYSTEMS |
| Cellular Aluminum Particle-Air Detonation Based on Realistic Heat Capacity Model 期刊论文 COMBUSTION SCIENCE AND TECHNOLOGY, 2020, 卷号: 192, 期号: 10, 页码: 1931-1945 作者: Xiang GX(项高翔); Yang PF(杨鹏飞); Teng HH(滕宏辉); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(1871Kb)  |  收藏  |  浏览/下载:500/142  |  提交时间:2019/09/09 Al particle cellular detonation heat capacity hybrid model |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9 作者: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(2608Kb)  |  收藏  |  浏览/下载:262/109  |  提交时间:2020/11/30 Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| PaSR和CMC模型在超声速燃烧模拟中的应用研究 学位论文 硕士论文,北京: 中国科学院大学, 2020 作者: 陈刘 Adobe PDF(5929Kb)  |  收藏  |  浏览/下载:813/11  |  提交时间:2020/09/28 超声速燃烧,湍流燃烧模型,部分搅拌反应器模型(pasr),条件矩封闭模型(cmc),可压缩性修正,大涡模拟(les) |
| Two-step weighting method for constructing fourth-order hybrid central WENO scheme 期刊论文 COMPUTERS & FLUIDS, 2020, 卷号: 207, 页码: 15 作者: Liu SP(刘升平); Shen YQ(申义庆); Peng J(彭俊); Zhang J(张俊) Adobe PDF(7646Kb)  |  收藏  |  浏览/下载:292/100  |  提交时间:2020/10/23 Hybrid central WENO scheme Discontinuity-detecting method Two-step weighting method |
| Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22 作者: Jin Y; Liao F(廖飞); Cai JS; Morris PJ Adobe PDF(7457Kb)  |  收藏  |  浏览/下载:238/87  |  提交时间:2020/07/06 Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文 4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020 作者: Yang L; 岳连捷; 张启帆; 张新宇 Adobe PDF(1289Kb)  |  收藏  |  浏览/下载:193/45  |  提交时间:2021/01/12 |