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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?
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?