Fluid MechanicsMedium
Question
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 :
Options
A.ρv2A
B.√2ρv2A
C.(1/2)ρv2A
D.2ρv2A
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