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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
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两级入轨  轨迹捕获  激波风洞  多体分离  动态试验  试验技术  
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)
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Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
循环神经网络在智能天平研究中的应用 期刊论文
力学学报, 2021, 卷号: 53, 期号: 08, 页码: 2336-2344
Authors:  聂少军;  王粤;  汪运鹏;  赵敏;  隋婧
Adobe PDF(6901Kb)  |  Favorite  |  View/Download：240/64  |  Submit date：2021/11/12
气动力测量  风洞天平  动态校准  人工智能  循环神经网络  
激波风洞高低压段钢膜片破裂特性研究 期刊论文
力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1747-1757
Authors:  聂少军;  汪运鹏;  薛晓鹏;  姜宗林
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激波风洞  主膜片  爆轰驱动  破裂特性  数值模拟  
高超声速喷管设计理论与方法 期刊论文
力学进展, 2020, 卷号: 51, 期号: 02, 页码: 257-294
Authors:  汪运鹏;  姜宗林
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Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download：356/178  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
基于深度学习技术的激波风洞智能测力系统研究 期刊论文
力学学报, 2020, 卷号: 52, 期号: 05, 页码: 1304-1313
Authors:  汪运鹏;  杨瑞鑫;  聂少军;  姜宗林
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激波风洞  人工智能  测力系统  动态校准  气动力测量  应变天平  
Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis 期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478
Authors:  Luo ZT(罗长童);  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Li JP(李进平);  Jiang ZL(姜宗林)
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Aerodynamic force measurement  Dynamic system  Impact response  Cross-validation  System identification  
AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林);  Teng HH(滕宏辉)
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Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1080Kb)  |  Favorite  |  View/Download：532/133  |  Submit date：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel