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Question

Air is streaming past a horizontal air plane wing such that its speed is 120m/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 is


A

4095.0 Pascal

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B

409.50 Pascal

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C

40.950 Pascal

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D

4.0950 Pascal

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Solution

The correct option is A

4095.0 Pascal


From the Bernoulli's theorem

P1P2=12ρ(v22v21)=12×1.3×[(120)2(90)2]

=4095 N/m2 or Pascal


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