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| Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet 期刊论文 JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17 作者: Liu H(刘杭); Yao W(姚卫); Zhang X(张旭); Zhang XY(张晓源); Liu, Jianwen; Yue LJ(岳连捷); Sun QH(孙泉华) 收藏  |  浏览/下载:30/0  |  提交时间:2024/03/11 Scramjet Dynamic Zone Flamelet Model High Enthalpy Shock Tunnel Combustors Improved Delayed Detached Eddy Simulation Vibrational Energy nonequilibrium heating cooling effects thermal nonequilibrium chemical nonequilibrium hydrogen |
| Research, Application and Future Prospect of Mode Decomposition in Fluid Mechanics 期刊论文 SYMMETRY-BASEL, 2024, 卷号: 16, 期号: 2, 页码: 22 作者: Long, Yun; Guo, Xi'an; Xiao TB(肖天白) 收藏  |  浏览/下载:27/0  |  提交时间:2024/04/15 fluid mechanics modal decomposition technology proper orthogonal decomposition |
| 激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文 航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126 作者: 王粤; 汪运鹏; 姜宗林 Adobe PDF(6797Kb)  |  收藏  |  浏览/下载:346/35  |  提交时间:2022/12/01 两级入轨 轨迹捕获 激波风洞 多体分离 动态试验 试验技术 |
| 动态飞行轨迹冲压发动机燃烧室性能与预测方法研究 学位论文 博士论文,北京: 中国科学院大学, 2023 作者: 周芮旭 Adobe PDF(9460Kb)  |  收藏  |  浏览/下载:96/8  |  提交时间:2023/06/28 动态飞行轨迹 超声速燃烧动态过程 燃烧室低维预测模型 |
| Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor 期刊论文 JOURNAL OF PROPULSION AND POWER, 2023 作者: Wu ZJ(吴振杰); Zhang QF(张启帆); Yu FY(于方游); Luo WH(罗苇航); Gao ZB(高占彪); Yue LJ(岳连捷) Adobe PDF(582Kb)  |  收藏  |  浏览/下载:45/0  |  提交时间:2023/06/15 Scramjet Engines Combustor Design flame stabilization mode transition path dependence |
| Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文 Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229 作者: Wang Y(王粤); Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(5479Kb)  |  收藏  |  浏览/下载:363/69  |  提交时间:2022/08/24 Multistage Launch Vehicle Aerodynamic Characteristics Shock Wave Interaction Angle of Attack Waverider Boundary Layer Flow Total Variation Diminishing Adverse Pressure Gradient Hypersonic Flows Hypersonic Wind Tunnels |
| 一种并联两级入轨飞行器纵向分离方案的数值研究 期刊论文 航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634 作者: 王粤; 汪运鹏; 王春; 姜宗林 Adobe PDF(4901Kb)  |  收藏  |  浏览/下载:565/79  |  提交时间:2022/07/11 两级入轨 高超声速 纵向分离 气动干扰 非定常流动 |
| Supersonic Combustion Mode Analysis of a Cavity Based Scramjet 期刊论文 AEROSPACE, 2022, 卷号: 9, 期号: 12, 页码: 826 作者: Meng, Yu; Sun WM(孙文明); Gu HB(顾洪斌); Chen, Fang; Zhou RX(周芮旭) Adobe PDF(3719Kb)  |  收藏  |  浏览/下载:52/11  |  提交时间:2023/04/20 scramjet combustion mode POD instability |
| 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:294/83  |  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:305/81  |  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 |