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In turbulent flow, one can estimate the Nusselt number using the analogy between heat and momentum transfer (Colburn analogy). This analogy relates the Nusselt number to the coefficient of friction, \(C_{p}\) as (a) \(\mathrm{Nu}=0.5 C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) (c) \(\mathrm{Nu}=C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) (e) \(\mathrm{Nu}=C_{f} \operatorname{Re}^{1 / 2} \operatorname{Pr}^{1 / 3}\) (d) \(\mathrm{Nu}=C_{f} \operatorname{Re} P r^{2 / 3}\)

Short Answer

Expert verified
Answer: (e) Nu=Cf Re^(1/2) Pr^(1/3)

Step by step solution

01

(Understand the given formulas)

First, let's break down the given formulas for Nusselt number estimation based on the Colburn Analogy. (a) \(\mathrm{Nu}=0.5 C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) (c) \(\mathrm{Nu}=C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) (e) \(\mathrm{Nu}=C_{f} \operatorname{Re}^{1 / 2} \operatorname{Pr}^{1 / 3}\) (d) \(\mathrm{Nu}=C_{f} \operatorname{Re} P r^{2 / 3}\) All of these formulas have the same variables: Nusselt number (Nu), coefficient of friction (\(C_f\)), Reynolds number (Re), and Prandtl number (Pr). However, they have different coefficients and exponents.
02

(Colburn Analogy)

The Colburn analogy is a useful method for estimating heat transfer in turbulent flows because it relates the Nusselt number to the coefficient of friction, Reynolds number, and Prandtl number. The correct formula for the Nusselt number using the Colburn analogy is: $$ \mathrm{Nu}=0.0296 C_{f} \operatorname{Re}^{4/5} \operatorname{Pr}^{1 / 3} $$ Now, compare the correct Colburn analogy formula with each of the given formulas to see which one is the most accurate representation.
03

(Comparing formulas)

Comparing each of the given formulas to the correct Colburn analogy formula: (a) \(\mathrm{Nu}=0.5 C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) - This formula has different coefficients and Re exponents compared to the correct Colburn analogy formula. (c) \(\mathrm{Nu}=C_{f} \operatorname{Re} \mathrm{Pr}^{1 / 3}\) - This formula has different coefficients and Re exponents compared to the correct Colburn analogy formula. (e) \(\mathrm{Nu}=C_{f} \operatorname{Re}^{1 / 2} \operatorname{Pr}^{1 / 3}\) - This formula has the correct Pr exponent but a different coefficient and Re exponent compared to the correct Colburn analogy formula. (d) \(\mathrm{Nu}=C_{f} \operatorname{Re} P r^{2 / 3}\) - This formula has different coefficients and exponents for both Re and Pr compared to the correct Colburn analogy formula.
04

(Selecting the most accurate representation)

None of the given formulas exactly matches the correct Colburn analogy formula for estimating Nusselt number in turbulent flow. However, selecting the closest representation: $$ \textbf{(e) }\mathrm{Nu}=C_{f} \operatorname{Re}^{1 / 2} \operatorname{Pr}^{1 / 3} $$ Formula (e) has the correct Pr exponent and a relatively similar Reynolds number exponent compared to the correct Colburn analogy formula, making it the most accurate representation among the given choices.

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Most popular questions from this chapter

The upper surface of a \(1-\mathrm{m} \times 1-\mathrm{m}\) ASTM B 152 copper plate is being cooled by air at \(20^{\circ} \mathrm{C}\). The air is flowing parallel over the plate surface at a velocity of $0.5 \mathrm{~m} / \mathrm{s}$. The local convection heat transfer coefficient along the plate surface is correlated with the correlation \(h_{x}=1.36 x^{-0.5}\), where \(h_{x}\) and \(x\) have the units \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(\mathrm{m}\), respectively. The maximum use temperature for the ASTM B152 copper plate is \(260^{\circ} \mathrm{C}\) (ASME Code for Process Piping, ASME B31.3-2014, Table A-1M). Evaluate the average convection heat transfer coefficient \(h\) for the entire plate. If the rate of convection heat transfer from the plate surface is \(700 \mathrm{~W}\), would the use of ASTM B152 plate be in compliance with the ASME Code for Process Piping?

Under what conditions can a curved surface be treated as a flat plate in fluid flow and convection analysis?

What is the physical significance of the Reynolds number? How is it defined for external flow over a plate of length \(L\) ?

What is the no-slip condition? What causes it?

Air at \(1 \mathrm{~atm}\) is flowing over a flat plate with a free stream velocity of \(70 \mathrm{~m} / \mathrm{s}\). If the convection heat transfer coefficient can be correlated by $\mathrm{Nu}_{x}=0.03 \operatorname{Re}_{x}^{08} \operatorname{Pr}^{1 / 3}$, determine the friction coefficient and wall shear stress at a location \(2 \mathrm{~m}\) from the leading edge. Evaluate air properties at \(20^{\circ} \mathrm{C}\) and $1 \mathrm{~atm}$.

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