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Development of a new frontwing that creates more downforce with high efficiency while following all of the regulations of the FSAE reglement. Results derived from the XLS New Wing Results (6000 timesteps): Downforce Frontwing: 199N Drag: 33N Reference Wing Results (6000 timesteps): Downforce Frontwing: 137 N Drag : 24N The Screenshots show in comparison with the 2nd homework a significant increase of the low pressure at the lower side of the frontwing. (The pictures were made with the same scale range.)
by simscalesimscale
pputin created this project
about 9 years ago