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| Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文 Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995 作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(9707Kb)  |  收藏  |  浏览/下载:297/85  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文 AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946 作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2434Kb)  |  收藏  |  浏览/下载:309/82  |  提交时间:2022/08/23 Aerodynamic Coefficients Two Stage to Orbit Aerodynamic Performance Hypersonic Flight Hypersonic Wind Tunnels Solenoid Valves Oblique Shock Pneumatic Actuator Hypersonic Flows Computer Aided Engineering |
| 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:409/1  |  提交时间:2022/12/03 |
| 高超声速 V 型前缘气动特性及流场作用机理研究 学位论文 硕士论文,北京: 中国科学院大学, 2022 作者: 姜文清 Adobe PDF(4250Kb)  |  收藏  |  浏览/下载:231/4  |  提交时间:2022/07/08 高超声速 V 形前缘 激波干扰 真实气体效应 |
| 基于泛函学习的斜激波与弓形激波干扰规律研究 学位论文 硕士论文,北京: 中国科学院大学, 2022 作者: 李帅 Adobe PDF(6690Kb)  |  收藏  |  浏览/下载:138/9  |  提交时间:2022/07/05 激波干扰,高温气体效应,多层分块算法,高超声速流动,气动热 |
| 斜爆轰推进中的起爆与驻定问题研究 学位论文 硕士论文,北京: 中国科学院大学, 2022 作者: 韩信 Adobe PDF(7629Kb)  |  收藏  |  浏览/下载:474/16  |  提交时间:2022/06/30 斜爆轰发动机 航空煤油RP-3 强制起爆 JF-12复现高超声速飞行条件激波风洞 斜爆轰波-边界层干扰 |
| 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:105/2  |  提交时间:2023/03/23 |
| Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator 期刊论文 ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425 作者: Xie, Wei; Luo, Zhenbing; Zhou, Yan; Gao, Tianxiang; Wu, Yun; Wang Q(汪球) Adobe PDF(8485Kb)  |  收藏  |  浏览/下载:119/59  |  提交时间:2022/10/25 SparkJet High-enthalpy hypersonic flow Shock control Shock-on-shock interaction Air supply |
| 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 作者: Yao W(姚卫); Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬) Adobe PDF(2954Kb)  |  收藏  |  浏览/下载:265/58  |  提交时间:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone 期刊论文 APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14 作者: Chen, Jianqiang; Yi, Shihe; Li XL(李新亮); Han GL(韩桂来); Zhang, Yifeng; Yang, Qiang; Yuan, Xianxu Adobe PDF(11175Kb)  |  收藏  |  浏览/下载:321/89  |  提交时间:2021/08/03 Hypersonic boundary layer Stability Transition Thermal protection |