Derive the formula for critical velocity
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Step-by-step explanation:
If the Reynold's number is not given, you can calculate it using the formula: Nr = ρ_V_D/µ. Laminar flow is represented by a Reynold's number of less than 2,320, and turbulent flow is represented by a Reynold's number of greater than 4,000. Plug in the values for each of the variables of the Reynold's number equation.
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