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Experiments on a rough turbine blade surface indicate that the local Nusselt number is ???=0.044???0.78??1/3. (a)...

Experiments on a rough turbine blade surface indicate that the local Nusselt number is ???=0.044???0.78??1/3. (a) Calculate the form of the average Nusselt number (???̅̅̅̅̅̅). (b) What would be the form of the local and average friction coefficient? Hint: modified Reynolds analogy is appropriate here.

Engineering   Mechanical-Engineering   
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