Q. Air is streaming past a horizontal airplane's wing such that its speed is $120 \,ms ^{-1}$ over the upper surface and $90\, ms ^{-1}$ at the lower surface. If the density of air is $1.3\, kgm ^{-3}$ 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 is
Mechanical Properties of Fluids
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