IGN PeculiarRequest SolgaleoDeposited Spearow M lvl 8 Message Please Trade Pokmon with me . Thanks in advance <| sep |> Probably will be sub . 500 on Friday as well . Very likely to lose that game imo unless the lakers can move the ball well and hit their shots . So this is technically correct . <| sep |> It ' s an over simplification , but the Bernoulli principle is at least partially valid . You ' re right there are many things it doesn ' t consider , and you ' d really need an experimentally or CFD derived coefficient of lift vs angle of attack curve to figure out total lift or downforce based on the projected area of the aerofoil . Ideally , you ' d select a wing profile , aspect ratio length vs width and angle of attack with the most favorable lift to drag ratio but it varies on application . At least from my understanding based on an undergrad mechanical engineering level . I ' m not breaking out the Navier Stokes equation because I don ' t fully understand it yet , but all aerodynamic theory stems from that pretty much . Anyways , my original point was that having a clean undisturbed airflow over the bottom of a car ' s wing makes it more effective because you ' re avoiding the turbulence created by the mounting points and struts . Is that part correct at least ?