Catia

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Measurement of the lift coefficient and drag coefficient at a certain angle of attack.

Simulating flow around BE105 profile wing

This project aims to develop a bioclimatic design for energy efficiency and thermal comfort in tropical regions like Indonesia. Some important building parameters such as building geometry and the envelope, HVAC, system, daylighting, natural ventilation, occupation, etc will be studied and optimized.
In this project, we will use the thermal comfort simulation, HVAC system, etc

Assessing the distribution of heat within the rear compartment

Simulate many geometries and find the aerodynamic coefficients for use in atmospheric reentry simulations

In this simulation, it is aimed to calculate the drag coefficient of an experimental rocket. Although the rocket geometry used is representative, the drag coefficient can be calculated for realistic models by following the simulation steps. K-w SST turbulence model was used for simulation. For the experimental rocket, the speed was taken 270 m / s and a ninety-degree (not realistic) flight angle assumption was made.

flow analysis in wind tunnel using finite element methods

Condotto inclinato a tenaglia plus OBSOLETO

Simulation de T20 avec le radiateur et les roues

Voir la variation de température du fluide entre l'entrée et la sortie

Comparison between balsa wood and spruce wood spar for a KFm3  4 meter span wing made of XPS blue foam for remote controlled aircraft.

Analysis of the aerodynamic drag of a monopole aircraft antenna

Pour l'Avant Projet ISAT Formula Team 2020

Catia | SimScale Project Library | Page 87