Air is streaming past a horizontal airplane wing such that its speed is 120 m...
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Air is streaming past a horizontal airplane wing such that its speed is 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 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 O 4095 0 pascal O 409 50 pascal O 40 950 pascal 4 0950 pascal
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