Multiple Choice
A Boeing 737 airliner has a mass of 20 000 kg and the total area of both wings (top or bottom) is 100 m2. What is the pressure difference between the top and bottom surface of each wing when the airplane is in flight at a constant altitude?
A) 1 960 N/m2
B) 3 920 N/m2
C) 7 840 N/m2
D) 4 560 N/m2
E) 3 070 N/m2
Correct Answer:
Verified
Correct Answer:
Verified
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