The pressure on the top surface of rhe aeroplan eis 0.8×10^5Pa ant the pressure at the bottom surface is 0.75×10^5 Pa .if the area of the surface is 50m^2 the dynamic lift of the wing is?
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Dynamic lift Force = (P1 - P2) * Area of surface
= (0.8 - 0.75) * 10⁵ * 50 N
= 250 kN
= (0.8 - 0.75) * 10⁵ * 50 N
= 250 kN
ashly2:
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