SimScale simulation projects by owirtanen | Page 1

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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.

This project simulates air flow around an Aircraft at low sub-sonic compressible flow regime.

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

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.

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