1.

The flow speeds of air on the lower and upper surfaces of the wing of an aeroplane are v and √2v respectively. The density of air is ρ and surface area of wing is A. The dynamic lift on the wing is:

Answer»

The flow speeds of air on the lower and upper surfaces of the wing of an aeroplane are v and 2v respectively. The density of air is ρ and surface area of wing is A. The dynamic lift on the wing is:



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