Lift !!! (airplanes) Hello, I am writing a research paper about the lift generated by the wings of an airplane. It is about the extent to which the Bernoulli effect and Newton's laws each contribute to creating lift. I planned on calculating the actual value of the lift generated by each, using data on the wing profiles of airplanes. But so far, I have only managed to get stuck. Any ideas on how I should go about doing this? PS Does anybody know where I can get detailed data/measurements of airplane wing profiles?