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Force measurement using strain-gauge balance in shock tunnel based on deep learning 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53
Authors:  Nie SJ(聂少军);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2346Kb)  |  Favorite  |  View/Download：60/11  |  Submit date：2024/02/26
Convolutional neural net-works  Deep learning  Frequency domain analysis  Force measurement  Time domain analysis  Recurrent neural networks  
Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文
SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2149Kb)  |  Favorite  |  View/Download：194/56  |  Submit date：2020/12/28
artificial intelligence  BALANCE SYSTEM  deep learning  DESIGN  dynamic calibration  FLOWS  force-measurement system  strain-gauge balance  
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)
View  |  Adobe PDF(2227Kb)  |  Favorite  |  View/Download：275/67  |  Submit date：2019/10/21
Aerodynamic force measurement  Dynamic system  Impact response  Cross-validation  System identification  
Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
Authors:  Meng BQ(孟宝清);  Han GL(韩桂来);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1937Kb)  |  Favorite  |  View/Download：270/87  |  Submit date：2018/10/30
Hypersonic  Shock tunnel  Start-up process  Impulse force  Vibration  
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：525/130  |  Submit date：2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
Wave system fitting: A new method for force measurements in shock tunnels with long test duration 期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2015, 卷号: 62-63, 页码: 2841-2848
Authors:  Luo CT(罗长童);  Wang YP(汪云鹏);  Wang C(王春);  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1074Kb)  |  Favorite  |  View/Download：359/101  |  Submit date：2016/01/07
Aerodynamic Force Measurements  Strain Gauge Balance  Inertia Compensation  Signal Decomposition  Accelerometer-free  Shock Tunnels