An aeroplane of mass 3× 10 ^4 kg and total wing area of 120 m2 is in a level flight at some height the difference in pressure between the upper and lower surface of its wings in kilopascals in
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Answer:
Given,
m=3×10
4
kg
g=10m/s
2
A=120m
2
Upward force =mg=ΔP×A
ΔP=
A
mg
ΔP=
120
3×10
4
×10
ΔP=2.5kPa
Explanation:
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