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背负式两体分离流动机理与安全分离方案研究 学位论文
博士论文,北京: 中国科学院大学, 2024
Authors:  王粤
Adobe PDF(35220Kb)  |  Favorite  |  View/Download:27/5  |  Submit date:2024/06/04
两级入轨  级间分离  高超声速  非定常流动  气动干扰  
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
Authors:  Zhang YF(张玉锋);  Li T(李腾);  Wei XL(魏小林)
Favorite  |  View/Download:58/0  |  Submit date:2024/03/11
Non -thermal plasma  Coaxial micro -tube burner  Methane flame  Combustion stability  
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
Authors:  王粤;  汪运鹏;  姜宗林
Adobe PDF(6797Kb)  |  Favorite  |  View/Download:412/43  |  Submit date: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  
基于神经网络和Volterra级数的非定常气动力建模方法研究 学位论文
硕士论文,北京: 中国科学院大学, 2023
Authors:  刘佳昕
Adobe PDF(8498Kb)  |  Favorite  |  View/Download:90/3  |  Submit date:2023/06/25
非定常气动力建模  数据增强  神经网络  Volterra级数  数值模拟  
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:192/52  |  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:613/93  |  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:431/82  |  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  
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
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9707Kb)  |  Favorite  |  View/Download:340/100  |  Submit date: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
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download:336/93  |  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  
GPU 加速的超大规模可压缩湍流直接数值模拟研究 学位论文
博士论文,北京: 中国科学院大学, 2022
Authors:  党冠麟
Adobe PDF(39646Kb)  |  Favorite  |  View/Download:496/17  |  Submit date:2023/02/06
软件,湍流,高超声速,直接数值模拟,图形处理器