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An aeroplane of mass 5000 kg is flying at an altitude of 3 km. If the area of wings is 50 m^2 and pressure at the lower surface of wings is 60000 PA,the pressure on the upper surface of wings is

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Apply P1-P2=½P(V1²-V2²)
The answer is 59×10³.

Sashank 9th Class....

Can you give a bit detailed response
Thanku

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