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Is lift over each wing segment is correspond?

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in Aerodynamics by (773k points)
Is lift over each wing segment is correspond?

(a) False

(b) True

The question was posed to me in my homework.

Question is from The Lifting Surface Theory in chapter Flow over Airfoils over Finite Wing of Aerodynamics

1 Answer

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Best answer
Correct answer is (a) False

The best I can explain: On a three dimensional, finite wing, lift over each wing segment does not correspond simply to what two-dimensional analysis predicts. Instead, this local amount of lift is strongly affected by the lift generated at neighboring wing section.

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