SimScale simulation projects by vineet | Page 1

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The project simulates 2 cases of aircraft wings to compare the aerodynamic effects.

The effect of numerics on the simulation quality and convergence time.

This project demonstrates the static stress analysis of three aircraft engine bearing bracket models considering both linear and nonlinear material definition. The models used in this analysis are taken from GrabCAD users who were the winners of GrabCAD 'Airplane Bearing Bracket Challenge'. The models are tested with horizontal and vertical loading conditions as provided on the challenge page of GrabCAD.

CFD analysis to verify the experimental results carried out on NACA 64015A Swpetback wing at AoA zero degree and Sweep angle 20 degrees.

Reference:  http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19980227185.pdf

This project contains resources for Session 1 of the F1 Workshop

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