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Question

An aeroplane of mass 6000 kg is flying at an altitude of 3 km. If the area of the wings is 30 m2 and the pressure at the lower surface of wings is 0.6×105 pa, the pressure on the upper surface of wings is : ( in pascal) ( g=10 ms2)

A
5.8×104
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B
6.8×104
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C
7.8×104
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D
8.8×104
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Solution

The correct option is D 5.8×104
Pressure at lower surface of wing=0.6×105Pa
Let pressure at upper surface of wing=p
Weight of the airplane =5×104N
For equilibrium, Weight =upthrust due to air

5×104=(0.6×105p)×50
103=0.6×105p
p=0.6×105103
p=59×103Pa

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