SimScale simulation projects by antonio | Page 1

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Investigation of lift distribution on a low Re wing

Tutorial project for a stress analysis of a connecting rod. The project only provides the geometry to start with. See our tutorials section to have a look at the step-by-step instructions to set up the simulation.

Weight is one of the most critical parameters in aircraft design. In this challenge, you will be provided with a baseline design of an aluminum aircraft wing. Your objective is to reduce the weight of the wing without exceeding the maximum allowable deflection (+ y direction) of .90 meters.

In this project vibration analysis of jet engine is performed.

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.

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

This project involves the simulation of stress analysis of an aircraft wing. There are total 6 comparison configurations with 3 different models and two different load definition.

This project involves the simulation of ventilation in an aircraft cabin. There are 6 comparison configurations with 3 different inlets and 2 outlets.

Weight is one of the most critical parameters in aircraft design. In this exercise, you will be provided with a baseline design of an aluminum aircraft wing. Your objective is to reduce the weight of the wing without exceeding the yield stress and maximum allowable deflection

CFD of the motorbike Aprilia RSV4 to investigate pressure field and velocity field

Aerodynamic simulation of drone's propeller

Homework assinment 1. Linear analysis of stress in elastic field.

Structural analisys of a drone's arm depending on screws preload.

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