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Q.

An aeroplane of mass 5000kg is flying at an altitude of 3km. If the area of the wings is 50m2 and pressure at the lower surface of wings is 0.6 × 105 Pa, then the pressure on the upper surface of wings is (in pascal) (g=10ms-2)

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a

59×103

b

6×103

c

2×104

d

59

answer is A.

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Detailed Solution

mg=Pdown-Pup×A

Pup=Pdown-mgA=0.6×105-5000×1050=59×103 Pa

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