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The laminar boundary layer for a thin airfoil is maximum at_____(a) Leading edge(b) Trailing edge(c) Quarter-chord(d) We can’t say without calculatingI had been asked this question by my school principal while I was bunking the class.This interesting question is from Laminar Flow in section Incompressible Flow over Airfoils of Aerodynamics |
Answer» The correct choice is (b) Trailing edge |
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