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| Advances in Plasma Diagnostics and Applications 专著 Beijing:MDPI, 2022 作者: Editors:Chen ZT; Attri P; Wang Q(汪球) Adobe PDF(20682Kb)  |  收藏  |  浏览/下载:407/1  |  提交时间:2022/12/03 |
| 复现飞行条件大尺度模型高超声速边界层转捩实验研究 学位论文 博士论文,北京: 中国科学院大学, 2022 作者: 刘美宽 Adobe PDF(7635Kb)  |  收藏  |  浏览/下载:197/14  |  提交时间:2022/06/28 高超声速 边界层转捩 大尺度模型 圆锥 平板 |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著 Beijing:Springer Nature, 2022 作者: Jiang ZL(姜宗林); Teng, Honghui Adobe PDF(13641Kb)  |  收藏  |  浏览/下载:103/2  |  提交时间:2023/03/23 |
| Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文 ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120 作者: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Peng JL(彭锦龙); Liu, Yan; Zhang ZL(张泽林); Fang SH(方思晗); Yu XL(余西龙) Adobe PDF(6496Kb)  |  收藏  |  浏览/下载:269/47  |  提交时间:2021/11/01 Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |
| Shock wave and turbulent boundary layer interaction in a double compression ramp 期刊论文 COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 15 作者: Tong FL(童福林); Duan JY(段俊亦); Li XL(李新亮) Adobe PDF(10792Kb)  |  收藏  |  浏览/下载:261/37  |  提交时间:2021/11/01 Shock wave Turbulent boundary layer Double compression ramp Direct numerical simulation |
| Direct numerical simulation of hypersonic boundary layer transition over a lifting-body model HyTRV 期刊论文 Advances in Aerodynamics, 2021, 卷号: 3, 期号: 1 作者: Qi H(齐涵); Li XL(李新亮); Yu ZP(于长平); Tong FL(童福林) Adobe PDF(4454Kb)  |  收藏  |  浏览/下载:260/30  |  提交时间:2021/11/01 Lifting body model Hypersonic transition Direct numerical simulation |
| Direct numerical simulation of a supersonic turbulent boundary layer over a compression–decompression corner 期刊论文 Physics of Fluids, 2021, 卷号: 33, 页码: 065111 作者: 段俊亦; 李欣; 李新亮; 刘洪伟 Adobe PDF(5069Kb)  |  收藏  |  浏览/下载:167/40  |  提交时间:2021/11/23 |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:315/165  |  提交时间:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Wall-shear stress fluctuations in a supersonic turbulent boundary layer over an expansion corner 期刊论文 JOURNAL OF TURBULENCE, 2020, 页码: 20 作者: Tong FL(童福林); Chen JQ; Sun D; Li XL(李新亮) Adobe PDF(5228Kb)  |  收藏  |  浏览/下载:191/83  |  提交时间:2020/08/26 Wall-shear stress expansion corner supersonic turbulent boundary layer direct numerical simulation |
| 超声速燃烧模态转换和迟滞的燃烧流动特性研究 学位论文 博士论文,北京: 中国科学院大学, 2020 作者: 张旭 Adobe PDF(18956Kb)  |  收藏  |  浏览/下载:326/19  |  提交时间:2020/05/31 超声速燃烧 凹腔稳焰 燃烧迟滞 模态转换 推力突变 |