Selected(0)Clear
Items/Page: Sort: |
| Self-similar unstart characteristics of supersonic contraction duct with an expansion corner 期刊论文 PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 20 Authors: Tong XT(仝晓通); Yue LJ(岳连捷); Wu WN(邬婉楠); Zhang QF(张启帆); Chen H(陈昊) Favorite  |  View/Download:11/0  |  Submit date:2024/03/11 |
| Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184 Authors: Dai, Chunliang; Sun, Bo; Yue LJ(岳连捷); Zhou, Shengbing; Zhuo, Changfei; Zhou, Changsheng; Yu, Jianyi Favorite  |  View/Download:15/0  |  Submit date:2024/02/19 Scramjet inlet Starting ability Thermochemical Work performance |
| Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文 AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18 Authors: Yang F(杨帆); Lin MY(林明月); Hu ZM(胡宗民); Han GL(韩桂来) Favorite  |  View/Download:54/0  |  Submit date:2023/11/28 oblique detonation engine cantilevered injection localized high heat flux boundary layer separation reattachment |
| 激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文 航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126 Authors: 王粤; 汪运鹏; 姜宗林 Adobe PDF(6797Kb)  |  Favorite  |  View/Download:321/32  |  Submit date:2022/12/01 两级入轨 轨迹捕获 激波风洞 多体分离 动态试验 试验技术 |
| Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194 Authors: Duan JY(段俊亦); Tong FL(童福林); Li XL(李新亮); Liu HW(刘洪伟) Favorite  |  View/Download:81/0  |  Submit date:2023/11/13 Compressible flow Boundary layers Direct numerical simulation Shock waves Skin friction Turbulent flow |
| Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120 Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(9327Kb)  |  Favorite  |  View/Download:177/56  |  Submit date:2023/05/26 Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |
| 超声速激波/湍流边界层干扰机理的直接数值模拟研究 学位论文 博士论文,北京: 中国科学院大学, 2023 Authors: 段俊亦 Adobe PDF(85007Kb)  |  Favorite  |  View/Download:105/11  |  Submit date:2023/06/25 激波/湍流边界层干扰 直接数值模拟 平均摩擦阻力分解 尺度分解 |
| 复杂因素影响下激波/边界层干扰特性研究 学位论文 硕士论文,北京: 中国科学院大学, 2023 Authors: 李江江 Adobe PDF(14509Kb)  |  Favorite  |  View/Download:105/8  |  Submit date:2023/07/04 激波/边界层干扰 膨胀波 真实气体效应 数值仿真 |
| 复杂湍流的大涡模拟建模与应用研究 学位论文 博士论文,北京: 中国科学院大学, 2023 Authors: 齐涵 Adobe PDF(16629Kb)  |  Favorite  |  View/Download:185/10  |  Submit date:2023/06/26 大涡模拟,亚格子模型,亚格子螺旋度,亚格子动能,转捩 |
| 二元高超声速进气道不起动/再起动相似律研究 学位论文 博士论文,北京: 中国科学院大学, 2023 Authors: 仝晓通 Adobe PDF(26068Kb)  |  Favorite  |  View/Download:148/7  |  Submit date:2023/07/03 高超声速进气道,相似律,不起动,再起动 |