Aerospace Engineering > GATE 2022 > Lift Calculation
Consider a circulation distribution over a finite wing given by the equation below.
The wingspan b is 10 m, the maximum circulation Γ0 is 20 m2/s, the density of air is 1.2 kg/m3 and the free stream speed is 80 m/s. The lift over the wing is _______ N. (rounded off to the nearest integer)
Correct : 9500 to 9800
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