An aeroplane of mass 6000kg is flying at an altitude of 3km. If the area of the wings is 30m2 and the pressure at the lower surface of wings is 0.6×105pa, the pressure on the upper surface of wings is : ( in pascal) ( g=10ms−2)
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 D5.8×104 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=(0.6×105−p)×50 ⇒103=0.6×105−p ⇒p=0.6×105−103 ⇒p=59×103Pa