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 $metre^3 $ 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 ....... $Pascal$ 
  • A$4095.0$
  • B$409.50$
  • C$ 40.950 $
  • D$4.0950 $
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