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Doing the Analysis wing of fixed wing UAV

A Snap fit. Statically modeled with friction-less contact.

The engineering challenge is to predict how well the finished product will perform under real-world working conditions.
This involves considering stresses and deformation as well as a range of failure criteria. 
honeycomb Core is used in many applications like aircraft, buildings, etc.  in this particular simulation a honeycomb core is simulated against static structural by applying a load, pressure on different faces with different conditions such as cantilever or fixed beam.  
A most important analysis of this simulation is finding out of plane elastic modulus. Out of Plane analysis is done by applying load in a particular direction and finding deformation, stress, and strain in that particular direction.  Therefore three different times load is applied in x, y, and z-direction to simulate out plane analysis.  I here have taken two conditions first cantilever beam and the second is a fixed beam.
 It was very easy and interesting to simulate here and the time consumed was even less as compared to other software.

Engergie cinétique d'un volant d'inertie.

In this project a static analysis of a shaft subjected to a user defined rotation and a cyclic boundary condition is demonstrated. The objective is to evaluate a shaft consisted of a single part against a shaft split in half.

Calculation of the displacement of cantilever beam. Learning new platform for simulating the things

FEA- Offshore reel hose- case 1 testing Tension, Torsional & Bending Load

To find the stress, strain and deflections at various points in a layer of the pavement.

FEA Offshore Reeling Hose Helical Spring-Basecase

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

Stress adding of foldable helmet, optimising materials

This project acts as the demonstration template for the FEA professional training of the SimScale Academy - https://www.simscale-academy.com

Demo Project for the SimScale Professional Training - https://www.simscale-academy.com/

This challenge is about designing your own lightweight design along with amazing renderings. The objective function is to reduce the weight of the wing without exceeding the maximum allowable deflection (+y direction) of 1 meter!

Video about the challenge: https://bit.ly/2TE3HPr

Strain analysis of a spinal rod with various thickness of adhesive

Ver como el reforzamiento afecta a los resultados

FEA calculation with used the symmetry. The geometry of the barrel with inside pressure.

Demostracion de metodo analitico para hallar la deformacion de una viga de perfil variable e incluso material variable

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