1.

The pressure on the top surface of an aeroplane wing is 0.7xx10^(3)Pa and pressure on the bottom surface is 0.75xx10^(3)Pa. If the srea of each surfac is 50m^(2), the dynamic lift on the wing is

Answer»

`25xx10^(4)N`
`0.5XX10^(4)N`
`5xx10^(4)N`
`0.25xx10^(4)N`

ANSWER :D


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