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| Influence of non-thermal plasma and electric field on non-premixed methane flame 期刊论文
THERMAL SCIENCE AND ENGINEERING PROGRESS, 2024, 卷号: 47, 页码: 15
作者: Zhang YF(张玉锋) ; Li T(李腾); Wei XL(魏小林)
  收藏 | 浏览/下载：18/0 | 提交时间：2024/03/11
Non -thermal plasma Coaxial micro -tube burner Methane flame Combustion stability |
| 高压捕获翼构型宽速域气动特性数值研究 学位论文
博士论文，北京: 中国科学院大学, 2023
作者: 王浩祥
Adobe PDF(15950Kb) | 收藏 | 浏览/下载：275/5 | 提交时间：2023/06/25
高超声速飞机 宽速域 高压捕获翼 气动干扰 计算流体力学 |
| 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 |
| 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 |
| 机体尾缘形状对高压捕获翼构型亚声速特性影响 期刊论文
航空学报, 2022, 期号: 06, 页码: 16
作者: 王浩祥; 肖尧; 张凯凯; 李广利; 常思源; 田中伟; 崔凯
Adobe PDF(2111Kb) | 收藏 | 浏览/下载：152/41 | 提交时间：2022/10/17
高压捕获翼 亚声速 流动特性 流动分离 数值模拟 |
| 高超声速钝前缘乘波体优化设计研究 学位论文
硕士论文，北京: 中国科学院大学, 2022
作者: 郭帅旗
收藏 | 浏览/下载：152/10 | 提交时间：2022/07/08
高超声速 乘波体 前缘钝化 符号回归 |
| Numerical and Experimental Study on Vertical Takeoff and Separation of the Compound Aircraft 期刊论文
IEEE ACCESS, 2022, 卷号: 10, 页码: 47597-47617
作者: Wang D; Hong QZ(洪启臻); Huang X(黄鑫); Pei XB; Wang J
Adobe PDF(4750Kb) | 收藏 | 浏览/下载：154/23 | 提交时间：2022/07/18
Aircraft Aircraft propulsion Compounds Aerodynamics Engines Automotive components Tail Compound aircraft CFD vertical take-off dynamical separation of two aircraft |
| Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
作者: Li, Mengzhe; Wang, Zhikai; Xu, Rongguang; Zhang, Xiaoliang; Chen, Zhitong; Wang Q(汪球)
Adobe PDF(8841Kb) | 收藏 | 浏览/下载：268/107 | 提交时间：2021/11/01
Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| 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：261/57 | 提交时间：2021/11/15
Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者: Zhou GX(周功喜); Zhang X(张旭); Li JP(李进平); Zhang XY(张晓源); Zhang SZ(张仕忠); Lin X(林鑫); Li F(李飞); Chen H(陈宏); Yue LJ(岳连捷); Yu XL(余西龙)
Adobe PDF(4108Kb) | 收藏 | 浏览/下载：329/47 | 提交时间：2021/09/07
High mach number scramjet Circular cross-section TDLAS Multi-view simultaneous imaging POD |
