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Question

An aeroplane of mass 5000 kg is flying at an altitude of 3 km. If the area of the wings is 50 m2 and pressure at the lower surface of wings is 0.6×105Pa, the pressure on the upper surface of wings is?(in pascal) (g=10ms2)

A
59×103
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B
2×104
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C
6×103
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D
59
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Solution

The correct option is A 59×103
weight of the aero plane and upthrust of plane
mg=(P2P1)A
p1 is upper surface
p2 isw lower surface
A area cross sectional
500×10=(0.6×105P1)
P1=0.6×1055000050
59000PA
0.59×105Pa

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