Step-by-Step Tutorial Session 1 - Front Wing Design Study (Part 1)

About this project

For your homework, your task is to investigate the behavior of drag and lift and determine the stall zone for two different front wing flap angles: 6 degrees (standard) and 18 degrees (high downforce) considering a constant inlet velocity of 20 m/s. The step-by-step tutorial below contains all of the steps for setting up the simulation in SimScale and visualizing the results.