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Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation 期刊论文
Acta Astronautica, 2024, 卷号: 216, 页码: 488-503./通讯作者:汪运鹏
Authors:  Wang Y(王粤);  Wang YP(汪运鹏)
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Multibody separation  Hypersonic  Dynamic stability  Center of pressure  Aerodynamic interaction  Numerical simulation  
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./通讯作者:汪运鹏
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Two-stage-to-orbit  Wind tunnel test  Numerical simulation  Stage separation  Hypersonic  Shock waves  
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./通讯作者:汪运鹏
Authors:  王粤;  汪运鹏;  姜宗林
Adobe PDF(6797Kb)  |  Favorite  |  View/Download:516/75  |  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  
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./通讯作者:汪运鹏
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  
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./通讯作者:Wang YP(汪运鹏)(1,2)
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
Design and Optimization Method for Hypersonic Quasi-Waverider 期刊论文
AIAA Journal, 2020, 卷号: 58, 期号: 5, 页码: 2132-2146./通讯作者:张陈安
Authors:  Liu W(刘文);  Zhang CA(张陈安);  Wang FM(王发民);  Ye ZY
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Local Piston Theory with Viscous Correction and Its Application 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
Authors:  Liu W(刘文);  Zhang CA(张陈安);  Han HQ;  Wang FM(王发民);  Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1329Kb)  |  Favorite  |  View/Download:891/163  |  Submit date:2017/03/28
Hypersonic  Unsteady Aerodynamics  Piston Theory  Aeroelasticity