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脉冲型天平高精度全自动校准系统 期刊论文
中国科学:物理学 力学 天文学, 2020, 卷号: 50, 期号: 06, 页码: 76-86
Authors:  汪运鹏;  李小刚;  姜宗林
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激波风洞  脉冲型天平  校准系统  全自动校准  
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  
大尺度高焓激波风洞喷管设计研究 期刊论文
中国科学:物理学 力学 天文学, 2019, 卷号: 49, 期号: 07, 页码: 63-72
Authors:  唐蓓;  汪运鹏;  姜宗林
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超高速高焓激波风洞  喷管设计  边界层修正  高温气体效应  CFD  
Aerodynamic Force Measurement in a Large-Scale Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
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Aerodynamic Force Measurement Techniques in JF12 Shock Tunnel 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
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)
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High-speed unsteady flows past two-body configurations 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 1, 页码: 54-64
Authors:  Xue XP;  Nishiyama Y;  Nakamura Y;  Mori K;  Wang YP(汪运鹏);  Wen CY
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Compressible flow  Shock/shock interaction  Two-body configurations  Unsteady flow  Wake/shock interaction  
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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超声速三维进气道内激波干扰的研究 期刊论文
推进技术, 2017, 期号: 12, 页码: 6
Authors:  项高翔;  王春;  汪运鹏;  姜宗林
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高超声速流动  箱式进气道  侧壁压缩进气道  波系结构  流场区域  
不同攻角下超声速降落伞伞绳的影响研究 期刊论文
航天返回与遥感, 2017, 卷号: 38, 期号: 04, 页码: 47-54
Authors:  薛晓鹏;  温志湧;  汪运鹏;  张德良
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超声速降落伞  伞绳  攻角  数值模拟  着陆  
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.
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Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel