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A small jet airplane has a total wing area of 77.5 m2 and a mass of 7.23 104 kg. (a) If this jet is in horizontal flight, determine the pressure difference between the lower and upper surfaces of the wings.

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To solve this problem we must simply resort to Newton's second law as well as the relationship between pressure and force as a physical unit applied in a given area.

In mathematical terms the Weight can be expressed as


F_w = mg

Where,

m = mass

g = Gravitational Acceleration

We have the mass and the gravitational acceleration therefore the Weight is


m = 7.23*10^4Kg


g = 9.8m/s^2

Replacing we have


F_w = (7.23*10^4)(9.8)


F_w = 708540 N

In this way the pressure exerted according to the active Area is,


P = (F)/(A)


P = (708540)/(77.5)


P = 9142.45Pa

Therefore the pressure difference between the lower and upper surface of the wings is 9.14kPa

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