For turbulent boundary layer flow over a flat plate, the thickness of the laminar sublayer δ' is given by

1
\(\frac{\nu}{u^*}\)
2
\(5(\frac{\nu}{u^*})\)
3
\(11.6(\frac{\nu}{u^*})\)
4
\(2300(\frac{\nu}{u^*})\)

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