个人详细信息
汪运鹏

汪运鹏

博士 副研究员 硕士生导师
中国科学院力学研究所 高温气体动力学国家重点实验室
邮箱:wangyunpeng@imech.ac.cn
座机:010-82543998
邮编:100190
地址:北京市北四环西路15号
个人详细信息

研究成果

20 1176 289
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[1] Liu YF,Wang YP,Yuan CK,et al. Aerodynamic Force And Moment Measurement Of 10° Half-angle Cone In Jf12 Shock Tunnel[J]. Chinese Journal Of Aeronautics,2017-06-01,30(3):983-987.
浏览/下载:95/21
[2] Wang YP,Hu ZM,Liu YF,et al. Starting Process In A Large-scale Shock Tunnel[C]. Aiaa Journal.Reston.Amer Inst Aeronautics Astronautics.2016-01-01.
浏览/下载:68/13
[3] Wang YP,Liu YF,Luo ZT,et al. Force Measurement Using Strain-gauge Balance In A Shock Tunnel With Long Test Duration[J]. Review Of Scientific Instruments,2016-01-01,87(5):55108.
浏览/下载:44/6
[4] Wang YP,Hu ZM,Liu YF,et al. Starting Process In A Large-scale Shock Tunnel[J]. Aiaa Journal,2016-04-01,54(5):1240-1249.
浏览/下载:37/13
[5] Wang YP,Liu YF,Jiang ZL. Design Of A Pulse-type Strain Gauge Balance For A Long-test-duration Hypersonic Shock Tunnel[J]. Shock Waves,2016-01-01,26(6):835-844.
浏览/下载:35/12
[6] Wang YP,Liu YF,Luo ZT,et al. Force Measurement In A Shock Tunnel With 100 Milliseconds Test Duration[C]. 34th Aiaa Applied Aerodynamics Conference.2016-01-01.
浏览/下载:30/11
[7] Wang YP,Hu ZM,Liu YF,et al. Numerical Investigation Of The Starting Process In A Long-test-duration Hypersonic Shock Tunnel[C]. 22nd Aiaa Computational Fluid Dynamics Conference.2015-01-01.
浏览/下载:11/3
[8] Wang YP,Liu YF,Luo ZT,et al. Force Test In A Large-scale Shock Tunnel[C]. 55th Aiaa Aerospace Sciences Meeting .Usa.American Institute Of Aeronautics And Astronautics Inc, Aiaa.2017-01-01.
浏览/下载:5/0
[9] 罗长童,汪运鹏,王春,等. 激波风洞气动力信号分离的波系适配法[C]. 高温气体动力学研究进展.2013-01-01,12-16.
浏览/下载:403/137
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研究主题

激波风洞[6] 动态校准[3] 气动力测量[3] 应变天平[3] 试验时间[2] 尖锥[2] 刚度特性[2] 信号分离[2] 测力[2] 试验需求[2] 波系结构[1] 数值模拟[1] 长试验时间[1] 高超声速气动力特性[1] 法向力[1]

成果统计

合作作者[TOP 5]

 

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