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 $\rho $ and surface area of wing is $A$ . The dynamic lift on the wing is
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 $\rho $ and surface area of wing is $A$ . The dynamic lift on the wing is
- A
$\frac{1}{2}\rho {v^2}\,A$
- B
$\rho {v^2}\,A$
- C
$\frac{3}{2}\rho {v^2}\,A$
- D
$2\rho {v^2}\,A$
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- [JEE MAIN 2024]