An aeroplane of mass 3 x 104 kg and total wing
area of 120 m²is in a level flight at some height.
The difference in pressure between the upper and
lower surfaces of its wings in kilopascals is
(g=10m/s2)
(1) 2.5
(2) 5.0
(3) 10.0
(4) 12.5
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Explanation:
Given An Aero plane of mass 3 x 104 kg and total wing area of 120 m²is in a level flight at some height. The difference in pressure between the upper and lower surfaces of its wings in kilo pascals is
- We know that pressure will be both in upward as well as downward surface and will be mg.
- Let PA and PB be the pressure upward and downward directions.
- Given m = 3 x 10^4
- Area = 120 m^2
- g = 10 m/s^2
- So we know that
- (PB – PA) Area = mg
- Or PB – PA = mg / Area
- Or ΔP = 3 x 10^4 x 10 / 120
- = 1/40 x 10^5 N/m^2
- Or ΔP = 100 / 40 x 10^3 Pa
- = 2.5 K Pa
- The difference in pressure between the upper and
- lower surfaces of its wings in kilo pascals is 2.5
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