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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:54/0  |  Submit date:2024/03/11 |
| 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:179/50  |  Submit date:2022/11/28 |
| 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:235/56  |  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:413/75  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 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 Adobe PDF(2765Kb)  |  Favorite  |  View/Download:369/47  |  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 |