- #1
Jeviah
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Homework Statement
hello, i have been given a piece of homework which is determining the characteristics on an aerofoils boundary layer. In the brief the following statement is made with no context “Aerofoil is flying in chord Reynolds number 0.2x10^6” am i correct in saying that is the point at which the boundary layer transitions from laminar to turbulant or would i use this reynolds number to determine the free flow velocity (Um)?
Homework Equations
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The Attempt at a Solution
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