Selected(0)Clear
Items/Page: Sort: |
| 跨流域发动机两相喷焰/羽流流动及辐射研究 学位论文 博士论文,北京: 中国科学院大学, 2022 Authors: 包醒东 Adobe PDF(10986Kb)  |  Favorite  |  View/Download:295/7  |  Submit date:2022/07/12 跨流域 发动机 两相流 喷焰/羽流 红外辐射 数值算法 |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著 Beijing:Springer Nature, 2022 Authors: Jiang ZL(姜宗林); Teng, Honghui Adobe PDF(13641Kb)  |  Favorite  |  View/Download:133/2  |  Submit date:2023/03/23 |
| 颗粒的高通量微流动操控机理研究 学位论文 博士论文,北京: 中国科学院大学, 2021 Authors: 苏敬宏 Adobe PDF(7268Kb)  |  Favorite  |  View/Download:345/6  |  Submit date:2022/01/12 微流动 颗粒操控 非球形效应 惯性升力 弹性-惯性迁移 |
| Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14 Authors: Yao W(姚卫); Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬) Adobe PDF(2954Kb)  |  Favorite  |  View/Download:312/77  |  Submit date:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Parametric Study on Lateral–Directional Stability of Hypersonic Waverider 期刊论文 AIAA Journal, 2021, 卷号: 59, 期号: 8, 页码: 3025-3042 Authors: 刘文; 张陈安; Wang Xiao-Peng; Li Jin-Jie; 王发民 Adobe PDF(7528Kb)  |  Favorite  |  View/Download:429/63  |  Submit date:2021/08/30 |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文 COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436 Authors: Zhang ZJ(张子健); Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(3599Kb)  |  Favorite  |  View/Download:402/95  |  Submit date:2021/03/03 Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |
| Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines 期刊论文 INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5 Authors: Zhai J; Zhang CA(张陈安); Wang FM(王发民); Zhang WW Adobe PDF(510Kb)  |  Favorite  |  View/Download:232/91  |  Submit date:2020/08/26 Hypersonic inlet lateral spillage waverider design method streamline tracing technology mass-flow ratio |
| Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文 AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020 Authors: Yao W(姚卫); Chen L(陈留) Adobe PDF(2272Kb)  |  Favorite  |  View/Download:300/154  |  Submit date:2021/06/11 |
| 全乘波背部进气高超声速飞机新概念构型研究 学位论文 博士论文,北京: 中国科学院大学, 2018 Authors: 肖尧 Adobe PDF(10334Kb)  |  Favorite  |  View/Download:933/20  |  Submit date:2018/05/24 高超声速飞行器 乘波体 背部进气布局 升阻比 气动设计与优化 |
| 乘波飞行器气动布局初步设计研究 学位论文 硕士论文,北京: 中国科学院研究生院, 2014 Authors: 贾子安 Adobe PDF(3417Kb)  |  Favorite  |  View/Download:645/15  |  Submit date:2014/08/28 |