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Question: Air is streaming past a horizontal air plane wing such that its speed in 120 m/s over the upper surf...

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

A

4095.0 Pascal

B

409.50 Pascal

C

40.950 Pascal

D

4.0950 Pasca

Answer

4095.0 Pascal

Explanation

Solution

From the Bernoulli's theorem

=12×1.3×[(120)2(90)2]=4095 N/m2= \frac { 1 } { 2 } \times 1.3 \times \left[ ( 120 ) ^ { 2 } - ( 90 ) ^ { 2 } \right] = 4095 \mathrm {~N} / \mathrm { m } ^ { 2 } or Pasca