SimScale simulation projects by Lt2Adnan | Page 1

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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.

Study of the flow of air from a Airbitat duct across a human body representation. This is to prove the existence of the Coanda effect.

This project demonstrates the usage of rotating zones

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.

In this project vibration analysis of jet engine is performed.

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

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

Simulation of airflow around a model airplane at different angles of attack (AOA)

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

Analysis of the stress forces on a custom pitot tube mount under pressure forces induced by a cruise speed of 30m/s

Pressure Driven Laminar Flow across a 1m long, 0.01m (10mm) diameter pipe

Investigation of Couette flow between two plates that are moving relative to each other

Simulation of airflow over a custom mount designed for a hobby grade pitot tube

2D Breathing using tet-dominant mesh as a test

Analysis of loading on drone arm (Drone Design Workshop Homework 2)

Analyzing how arm density affects a drop test of a drone (Drone Workshop Homework 3)

CFD simulation of 2D Breathing with a N95 Mask

Analysis of quadrotor blade angle of attack (Simscale Drone Workshop Homework 1)

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

Investigation of the stress and deflections in a wing due to wind pressure

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