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| 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 |
| 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 |
| Similarity Analysis on Two-Dimensional Hypersonic Inlets Unstart 期刊论文 AIAA JOURNAL, 2023, 卷号: 61, 期号: 2, 页码: 555-572 Authors: Tong XT(仝晓通); Yue LJ(岳连捷); Chen H(陈昊); Zhang QF(张启帆); He CM(何成明) Adobe PDF(6058Kb)  |  Favorite  |  View/Download:127/34  |  Submit date:2022/11/28 |
| 一种超高速冲压发动机 专利 发明专利. 一种超高速冲压发动机, 专利号: ZL202111347088.0, 申请日期: 2021-11-15, 授权日期: 2022-11-22 Inventors: 仝晓通; 岳连捷; 张启帆; 陈昊; 杨理 Adobe PDF(355Kb)  |  Favorite  |  View/Download:82/20  |  Submit date:2023/01/10 |
| Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass Injection 期刊论文 AIAA JOURNAL, 2022, 页码: 5 Authors: Li JJ(李江江); Chen H(陈昊); Tong XT(仝晓通); Gao X; Zhang QF(张启帆); Yue LJ(岳连捷) Adobe PDF(1812Kb)  |  Favorite  |  View/Download:188/35  |  Submit date:2022/05/17 |
| Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22 Authors: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(8067Kb)  |  Favorite  |  View/Download:369/58  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 廉价航天发射路在何方? 科普文章 2020 Authors: 仝晓通 Adobe PDF(2158Kb)  |  Favorite  |  View/Download:197/42  |  Submit date:2020/11/27 |
| 内压缩波系对高超声速进气道自起动性能影响研究 期刊论文 实验流体力学, 2019, 卷号: 33, 期号: 03, 页码: 60-67 Authors: 贾轶楠; 张启帆; 仝晓通; 岳连捷; 张新宇 View  |  Adobe PDF(2765Kb)  |  Favorite  |  View/Download:336/39  |  Submit date:2019/09/12 自起动性能 肩部膨胀扇 侧压式 边界层厚度 几何喉道 气动喉道 |