1.
Three Degree-of-freedom Forced Vibration Method for Identification of Aerodynamic Derivatives of Bridge Decks;
桥梁断面气动导数识别的三自由度强迫振动法
2.
Theoretical and Experiment Study on Identification of Aerodynamic Derivatives of Bridge Decks;
桥梁结构气动导数识别的理论和试验研究
3.
An improved stochastic subspace identification method for flutter derivatives of bridge decks
桥梁断面气动导数识别的改进随机子空间法
4.
The Research on Three Degree-of-freedom Forced Vibration Method for Identification of Aerodynamic Derivatives and Flutter Mechanism;
气动导数识别的三自由度强迫振动法及颤振机理研究
5.
SUBSECTION EXTENDED ORDER ITERATIVE LEAST SQUARE METHOD FOR AERODYNAMIC DERIVATIVE IDENTIFICATIONS OF ECCENTRIC BRIDGE SECTION MODELS
有偏心桥梁断面气动导数识别的分段扩阶最小二乘迭代法
6.
Identification of aerodynamic derivatives for bridge sections by LSCE method
利用LSCE方法识别桥梁气动导数研究
7.
Identification Method of Free Coupled Vibration for Aerodynamic Derivatives of Bridge Decks;
桥梁断面气动导数自由耦合振动识别方法研究
8.
Estimation of aerodynamic admittance functions of long-span bridges by the relationships among aerodynamic parameters
基于气动参数之间关系的桥梁断面气动导纳识别
9.
Parameter identification and simulation analysis of the rolling guide-way
滚动导轨结合面参数识别及仿真分析
10.
Experimental Recognition of Aerodynamic Admittance of ∏-Shape Main Girder Cross Section of Long Span Bridge
大跨桥∏形主梁断面气动导纳的试验识别
11.
Aerodynamic Admittance Identification for Non-streamline Section by Method of Zero-separation
非流线型截面气动导纳识别的零点分离法
12.
Automatic Number Identification
自动数字码识别器自动数字识别
13.
The Identification of Flutter Derivatives for Long-span Bridges Applying the Forced Vibration Method;
大跨桥梁颤振导数识别的强迫振动法研究
14.
Identification of Aerodynamic Parameters of Bridge Section Using Artificial Neural Network;
桥梁断面气动参数的人工神经网络识别
15.
Study on Aerodynamic Parameter Identification and Wind-Induced Responses of Long-Span Arch Bridges;
大跨度拱桥气动参数识别及风致响应研究
16.
Discussion on Aerodynamic Admittance of Flat Double-Girder Bridge Decks through Cross-Correlation Spectrum Recognition
扁平双边肋主梁桥梁断面气动导纳互功率谱识别方法探讨
17.
dynamic parameter recognition of machinery
机械的动力学参数识别
18.
Simulation for Identification of Flutter Derivatives for Aerofoil Using Forced Vibration Method and Its Application
机翼节段颤振导数的强迫振动仿真识别及其应用