Dynamics Modeling and Application for Flexible Wing Based on Collaborative Simulation
基于协同仿真的柔性机翼动力学建模及应用

Using multidisciplinary collaboration simulation,applying aeroelastic theory and method,structural modeling with FEM was set up,structural dynamics and vibration mode were analyzed,and then problem of gust load alleviation for a large flexible wing was discussed.The simulation verified the approach available and effective.