Static

This analysis type is used to determine the displacements and stresses in structures or components caused by the applied constraints and steady loads - inertia and damping effects are ignored. A Static analysis can be either linear or nonlinear. | Page 4

compresion ciclica (ahuellamiento une 12697 - 25) - Copy - Copy - Copy - Copy

This project demonstrates the static stress analysis of three aircraft engine bearing bracket models considering both linear and nonlinear material definition. The models are tested with horizontal and vertical loading conditions as provided on the challenge page of GrabCAD.

This piece acts as part of the support of a motor engine

Compare stress in solid vs. lattice-structured implants.
Geometry:
•	Implant dimensions: 0.15 m × 0.02 m (diameter).
•	Lattice structure: Gyroid (50% porosity).
Material: Titanium (E = 110 GPa, ν = 0.33).
Boundary Conditions:
•	1 kN compressive load simulating body weight.
•	Fixed support at the distal end.
Analysis Steps (SimScale):
1.	Static structural analysis.
2.	Homogenize lattice properties (simplified model).
3.	Compare stress and weight reduction.
Deliverables:
•	Stress distribution in lattice vs. solid.
•	Weight reduction percentage.
Validation: Compare with experimental data on lattice compression.

ボルトナットの締結シミュレーション

Tutorial project for linear static analysis of a crane - Copy - Copy - Copy

Testing the modelling of an interference fit with a very simple geometry

This project demonstrates the static stress analysis of three aircraft engine bearing bracket models considering both linear and nonlinear material definition. The models are tested with horizontal and vertical loading conditions as provided on the challenge page of GrabCAD. - Copy

This project focuses on designing, analyzing, and testing a CubeSat for potential space missions. The CubeSat is a small, modular satellite that follows the 1U (10x10x10 cm) standard, designed for scientific research and technological experiments in low Earth orbit (LEO).

The main Goal of this study is to find the final max forces that a design of a robotic arm will be able to withstand.  
What is the highest stress point on the assembly design