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0 Geometries
0 Meshes
0 Simulation setups
0 ResultsThe objective of this project is to design and evaluate a drone landing pad capable of providing a stable and safe landing surface for unmanned aerial vehicles (UAVs). The landing pad is modelled using computer-aided design (CAD) techniques and analysed using finite element analysis (FEA) to assess its structural performance under the load exerted by a drone during landing. The structural analysis is carried out using SimScale to determine the distribution of stress and deformation within the landing pad. Appropriate material properties, boundary conditions, and loading conditions are defined to simulate real operating conditions. The analysis helps identify critical regions that experience maximum stress and displacement, ensuring that the design remains within the allowable limits of the selected material. The results obtained from the simulation are used to evaluate the structural integrity, stability, and safety of the landing pad. Based on the analysis, the suitability of the design for practical drone landing applications is assessed. This project demonstrates the application of computer-aided engineering (CAE) tools in designing reliable aerospace support structures while improving understanding of structural analysis and engineering design principles.
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by slilbaekslilbaek
shaashwatbajpa created this project
about 2 months ago
0 Geometries 0 Meshes 0 Simulation setups 0 ResultsThe objective of this project is to design and evaluate a drone landing pad capable of providing a stable and safe landing surface for unmanned aerial vehicles (UAVs). The landing pad is modelled using computer-aided design (CAD) techniques and analysed using finite element analysis (FEA) to assess its structural performance under the load exerted by a drone during landing. The structural analysis is carried out using SimScale to determine the distribution of stress and deformation within the landing pad. Appropriate material properties, boundary conditions, and loading conditions are defined to simulate real operating conditions. The analysis helps identify critical regions that experience maximum stress and displacement, ensuring that the design remains within the allowable limits of the selected material. The results obtained from the simulation are used to evaluate the structural integrity, stability, and safety of the landing pad. Based on the analysis, the suitability of the design for practical drone landing applications is assessed. This project demonstrates the application of computer-aided engineering (CAE) tools in designing reliable aerospace support structures while improving understanding of structural analysis and engineering design principles.
