The objective of the project was to see if a regular upper cambered wing (traditional wing) could produce more lift than the following six wings: Symmetrical Curved, Brick, Barn Door, Car-Foil, Right Triangle, and a Sideways
The results show that the Car-Foil Wing achieved the highest lift.
We conclude that the Traditional Wing didn#t produce the most lift after all. Instead two of our made up wings, the Car-Foil and the Sideways Figure-8 both got high lift at 10 to 30 degrees angle of attack. However the Traditional wing achieved consistent lift over all the angle of attacks, making this wing very suitable of passenger planes.
This project is to see which of the seven different airfoils, both standard designs and made-up designs, could produce the most lift at different angles of attack.