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Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration 期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(7258Kb)  |  Favorite  |  View/Download：121/21  |  Submit date：2024/01/15
Two-stage-to-orbit  Wind tunnel test  Numerical simulation  Stage separation  Hypersonic  Shock waves  
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download：71/12  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
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：413/43  |  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  
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：207/43  |  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  
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：197/55  |  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：616/93  |  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：437/84  |  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  
基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
Adobe PDF(1844Kb)  |  Favorite  |  View/Download：185/45  |  Submit date：2023/02/09
高超声速进气道  不起动  再起动  主动射流  流动控制  
Experimental study of the high-power laser resistance of ablative material-filled sandwich panels with truss cores under hypersonic airflow 期刊论文
COMPOSITE STRUCTURES, 2022, 卷号: 301, 页码: 116139
Authors:  Yuan W(袁武);  Wang JT(王江涛);  Wang RX(王睿星);  Wang Z(王喆);  Song HW(宋宏伟);  Huang CG(黄晨光)
Adobe PDF(9765Kb)  |  Favorite  |  View/Download：201/58  |  Submit date：2022/10/23
Sandwich panel  Thermal insulation  Lightweight structure  Failure point  
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：345/101  |  Submit date：2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference