How do we work out where the distance from the leading edge the laminar boundary layer would turn into a turbulent boundary layer? Assuming we have been given the length of the plate, speed, dynamic viscosity of air and the Reynolds number?
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For help with homework problems, always show what you have tried so far. Otherwise you come across as asking people to do your homework for you, which I assume is not what you wish. – Organic Marble Jul 15 '21 at 01:33
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Related: Is airflow ever laminar in the boundary layer, near the wing leading edge? – mins Jul 17 '21 at 20:04