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MCAT Question of the Day
Q:
Airfoils can generate lower pressures on their top surfaces than their bottom surfaces which lie at atmospheric pressure. This helps air on the bottom push the airfoil upwards. For a flying 500kg airfoil with an area of 20 m
2
, what is the maximum pressure on its top surface? Assume air pressure is 100 kPa. 1 Pa = 1 N/m
2
A
0 Pa
B
250 Pa
C
75000 Pa
D
99750 Pa
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