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An airplane has an effective wing surface area of 19.4 m2 that is generating the lift force. In level flight the air speed over the top of the wings is 67.0 m/s, while the air speed beneath the wings is 51.0 m/s. What is the weight of the plane?

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Answer:

W =23807.68 N

Step-by-step explanation:

given,

surface area of wing = 19.4 m²

speed over top wing = 67 m/s

speed under wing = 51 m/s

density of air = 1.3 kg/m³

weight of plane

From Bernoulli's principle


P_1 + (1)/(2)\rho v_1^2 = P_2 + (1)/(2)\rho_2^2

where 1 and 2 are two different locations at the same geo potential level

so if we call 1 the lower surface and 2 the upper surface,

we find the pressure differential, P₁ -P₂


\Delta P =(1)/(2)\rho (v_2^2-v_1^2)


\Delta P =(1)/(2)* 1.3 * (67^2-51^2)


\Delta P =1227.2\ N/m^2

then the force acting on the plane is

F=P A

F=1227.2 x 19.4

F =23807.68 N

weight of the plane

W =23807.68 N

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