Air of density 1.05 kg/m^3 flows over a planes wing at 111.0 m/s and below the wing at 80.0 m/s. If the area of the wing is 100.0 m^2 what is the upward force (dynamic lift) on the plane’s wing?
SOLUTION:
= 1.05 kg/m3
= 111 m/s = Over velocity
= below velocity
A= area = 100 m2
Lets the upward force is = F
The upward force is = 310852.5 N
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