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Hello, this question is about lift in fixed wing flight (airplanes).
Is it possible to calculate separately the lift generated by:
- Newton's laws (wings deflecting air particles)
- Bernoulli effect (difference in air pressure above and below the wings caused by the shape of the wings(?))
Any suggestions on how to do this?
Is it possible to calculate separately the lift generated by:
- Newton's laws (wings deflecting air particles)
- Bernoulli effect (difference in air pressure above and below the wings caused by the shape of the wings(?))
Any suggestions on how to do this?