Fluid Mechanics
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air is streaming past a horizontal airplane wing with 120 m/s over upper part and 90 m/s at the lower part. air density= 1.3kg/m^3. wing 10m long and 2m wide. What is the pressure difference between two sides of the wing??
The Preasure difference would be p*delta( v)
p=1.3
delta v=30
so the preasure difference is 39N/m^2