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| 高压捕获翼低阻力机体外形数值研究 学位论文
硕士论文，北京: 中国科学院大学, 2024
Authors: 席小喆
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高压捕获翼 机体外形 流动分离 最小阻力外形 数值模拟 |
| Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18
Authors: Guo SQ(郭帅旗); Liu W(刘文); Zhang CA(张陈安); Liu Y(刘洋); Wang FM(王发民)
Favorite | View/Download：34/0 | Submit date：2024/02/05
Hypersonic waverider Aerodynamic model Symbolic regression Bluntness effect |
| Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120
Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
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Two-stage-to-orbit Hypersonic Numerical simulation Stage separation Aerodynamic interaction Unsteady flow Center of gravity |
| 高超声速动导数理论建模与数值模拟研究 学位论文
硕士论文，北京: 中国科学院大学, 2023
Authors: 周翔
Adobe PDF(11234Kb) | Favorite | View/Download：196/6 | Submit date：2023/06/26
高超声速 乘波体 动导数 粘性干扰效应 理论建模 |
| 翼反角对高压捕获翼构型高超气动特性的影响 期刊论文
航空学报, 2023, 卷号: 44, 期号: 08, 页码: 45-58
Authors: 常思源; 肖尧; 李广利; 田中伟; 张凯凯; 崔凯
Adobe PDF(3584Kb) | Favorite | View/Download：222/46 | Submit date：2022/10/17
高压捕获翼 高超声速 数值模拟 上/下反角 稳定性 |
| Influence of Non Uniform Bluntness on Aerodynamic Performance and Aerothermal Characteristics of Waverider 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 3, 页码: 205
Authors: Qu, Zhipeng; Wang, Wanyu; Xiao, Houdi; Xiao Y(肖尧); Li GL(李广利); Cui K(崔凯)
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waverider non uniform hypersonic computational fluid dynamics (CFD) |
| 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, 2023, 卷号: 44, 期号: 06, 页码: 10.7527/S1000-6893.2022.27215
Authors: 王浩祥; 肖尧; 张凯凯; 李广利; 常思源; 田中伟; 崔凯
Adobe PDF(2111Kb) | Favorite | View/Download：203/59 | Submit date：2022/10/17
高压捕获翼 亚声速 流动特性 流动分离 数值模拟 |
| 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
Authors: 王粤; 汪运鹏; 王春; 姜宗林
Adobe PDF(4901Kb) | Favorite | View/Download：628/99 | Submit date：2022/07/11
两级入轨 高超声速 纵向分离 气动干扰 非定常流动 |
| 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
Authors: Wang Y(王粤); Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林)
Adobe PDF(5479Kb) | Favorite | View/Download：466/89 | Submit date：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 |
| 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
Authors: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(2434Kb) | Favorite | View/Download：350/102 | Submit date：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 |
