Analysis of a UAV structure
Meshing and the analysis results\\nThe entire UAV structure is meshed using shell and beam elements\\n Masses are assigned o these locations using OD mass element. Air loads, particularly lift forces are applied on the lower wing skin. To constrain the aircraft on air, an unique methodology of inertia relief was considered.NASTRAN automatically assigns an opposite inertia at the CG point and constraints the model. This is essential for airborne flight load analysis of structure.
About Me
I am here for jobs related to Mechanical Engineering. Problem solving and design are my areas of interest. All kind of jobs in this fields are welcomed. I looking for work to sharpen my skills specially in the field of Finite Element Analysis and 3D modelling. I have hands-on experience using Msc NASTRAN and PATRAN to perform FEA. Modelling & Drafting will be done in Creo & AutoCAD respectively.
