Structural Analysis and Modeling of X500 Quadcopter Frame

In this study, the structural integrity of an X500 quadcopter frame was evaluated using ANSYS and SOLIDWORKS. The goal was to identify any weaknesses or vulnerabilities in the frame. The frame was first designed in SOLIDWORKS, then imported to ANSYS for detailed stress and deformation analysis. The results of the analysis showed that the frame was capable of withstand various loads and stresses, with no significant deformation or failure observed. This confirms the frame's robustness and durability and its ability to perform well under different conditions. The use of ANSYS and SOLIDWORKS in structure analysis and modeling is a crucial aspect of the design and development process for any aircraft, and can greatly contribute to the overall safety and reliability of the vehicle.