Electronic plug-in is an important part of aircraft,and its structural design needs to meet the requirements of stiffness and strength under dynamic load environment for example of random vibration and impact vibration.In this paper,random vibration and impact of electronic plug-in is studied based on the extracted dynamic load.The theoretical basis and simulation flow of the analysis are described.The results show that the electronic plug-in meets the design requirements.
electronic plug-inrandom vibrationshock vibrationdynamicsfinite element
万方数据
维普
