Air is streaming past a horizontal air plane wing such that its speed in 120 m/s over the upper surface and 90 m/s at the lower surface. If the density of air is 1.3 kg per metre3 and the wing is 10 m long and has an average width of 2 m, then the difference of the pressure on the two sides of the wing of
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a
4095.0 Pascal
b
409.50 Pascal
c
40.950 Pascal
d
4.0950 Pascal
answer is A.
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Detailed Solution
From the Bernoulli's theoremP1−P2=12ρ(v22−v12)=12×1.3×[(120)2−(90)2]=4095 N/m2 or Pascal
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Air is streaming past a horizontal air plane wing such that its speed in 120 m/s over the upper surface and 90 m/s at the lower surface. If the density of air is 1.3 kg per metre3 and the wing is 10 m long and has an average width of 2 m, then the difference of the pressure on the two sides of the wing of