Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

Consider turbulent forced convection in a circular tube. Will the heat flux be higher near the inlet of the tube or near the exit? Why?

Short Answer

Expert verified
Explain your reasoning. Answer: The heat flux will be higher near the inlet of the circular tube. This is because the thermal boundary layer, which is responsible for much of the heat transfer, is thinner at the inlet, leading to a steeper temperature gradient and a higher heat transfer rate. As the fluid moves along the tube, the boundary layer thickness increases, causing a decrease in the temperature gradient and a lower heat flux near the exit.

Step by step solution

01

Understanding turbulent forced convection

Turbulent forced convection is a heat transfer process in which a fluid moves through a conduit (like a circular tube in this exercise) and exchanges heat with the walls of the conduit. In this case, the fluid flow is turbulent, which indicates that the fluid particles move in an irregular and chaotic manner, leading to a higher mixing rate and, consequently, a higher heat transfer rate.
02

Factors affecting heat flux

Heat flux is the rate at which heat is transferred per unit area along the direction of heat transfer. There are several factors influencing the heat flux in the case of turbulent forced convection in a circular tube, including fluid properties, tube geometry, flow conditions, and temperature difference between the fluid and tube wall. Some of these factors, like flow velocity and fluid properties, change along the length of the tube, impacting the heat flux variation from the inlet to the exit.
03

The effect of thermal boundary layer on heat flux:

As the fluid flows through the circular tube, a thermal boundary layer develops near the tube wall. In this layer, the temperature gradient is steep, and much of the heat transfer occurs. The thickness of the boundary layer increases with distance along the flow direction, leading to a decrease in the temperature gradient and, consequently, a lower heat flux.
04

Conclusion

Considering the development of the thermal boundary layer and the decreasing temperature gradient along the flow direction, we can conclude that the heat flux will be higher near the inlet of the circular tube than near the exit. The reason for this is that the thermal boundary layer is thinner at the inlet, resulting in a steeper temperature gradient and, therefore, a higher heat transfer rate.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

The exhaust gases of an automotive engine leave the combustion chamber and enter an 8 -ft-long and 3.5-in-diameter thin-walled steel exhaust pipe at \(800^{\circ} \mathrm{F}\) and \(15.5 \mathrm{psia}\) at a rate of $0.05 \mathrm{lbm} / \mathrm{s}$. The surrounding ambient air is at a temperature of \(80^{\circ} \mathrm{F}\), and the heat transfer coefficient on the outer surface of the exhaust pipe is $3 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2},{ }^{\circ} \mathrm{F}$. Assuming the exhaust gases to have the properties of air, determine \((a)\) the velocity of the exhaust gases at the inlet of the exhaust pipe and \((b)\) the temperature at which the exhaust gases will leave the pipe and enter the air.

metal pipe $\left(k_{\text {pipe }}=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, D_{\text {, pipe }}=\right.\( \)5 \mathrm{~cm}, D_{o \text {, pipe }}=6 \mathrm{~cm}\(, and \)\left.L=10 \mathrm{~m}\right)$ situated in an engine room is used for transporting hot saturated water vapor at a flow rate of \(0.03 \mathrm{~kg} / \mathrm{s}\). The water vapor enters and exits the pipe at \(325^{\circ} \mathrm{C}\) and \(290^{\circ} \mathrm{C}\), respectively. Oil leakage can occur in the engine room, and when leaked oil comes in contact with hot spots above the oil's autoignition temperature, it can ignite spontaneously. To prevent any fire hazard caused by oil leakage on the hot surface of the pipe, determine the required insulation $\left(k_{\text {ins }}=0.95 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.$ ) layer thickness over the pipe for keeping the outer surface temperature below $180^{\circ} \mathrm{C}$.

A 4-m-long tube is subjected to uniform wall heat flux. The tube has an inside diameter of \(0.0149 \mathrm{~m}\) and a flow rate of $7.8 \times 10^{-5} \mathrm{~m}^{3} / \mathrm{s}$. The liquid flowing inside the tube is an ethylene glycol-distilled water mixture with a mass fraction of \(0.5\). Determine the apparent (developing) friction factor at the location \(x / D=20\) if the inlet configuration of the tube is: \((a)\) re-entrant and \((b)\) square- edged. At this location, the local Grashof number is Gr \(=24,000\), and the properties of the mixture of distilled water and ethylene glycol are: \(\operatorname{Pr}=20.9\), $\nu=2.33 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\(, and \)\mu_{y} / \mu_{s}=1.25$.

Water at $10^{\circ} \mathrm{C}\left(\rho=999.7 \mathrm{~kg} / \mathrm{m}^{3}\right.\( and \)\mu=1.307 \times\( \)10^{-3} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\( ) is flowing in a \)0.20-\mathrm{cm}$-diameter, 15 -m-long pipe steadily at an average velocity of $1.2 \mathrm{~m} / \mathrm{s}\(. Determine \)(a)\( the pressure drop and \)(b)$ the pumping power requirement to overcome this pressure drop. Assume flow is fully developed. Is this a good assumption? Answers: (a) \(188 \mathrm{kPa}\), (b) $0.71 \mathrm{~W}$

Liquid water flows in an ASTM B75 copper tube at a mass flow rate of $3.6 \mathrm{~g} / \mathrm{s}\(. The water enters the tube at \)40^{\circ} \mathrm{C}$, and the tube surface is subjected to a constant heat flux at a rate of \(1.8 \mathrm{~kW}\). The tube is circular with an inner diameter of $25 \mathrm{~mm}\( and a length of \)3 \mathrm{~m}$. The maximum use temperature for ASTM B75 copper tube is \(204^{\circ} \mathrm{C}\) (ASME Code for Process Piping, B31.3-2014, Table A-1M). Would the surface temperature of the tube exceed the maximum use temperature for the copper tube? If so, determine the axial location along the tube where the tube's surface temperature reaches \(204^{\circ} \mathrm{C}\). Evaluate the fluid properties at $100^{\circ} \mathrm{C}$. Is this an appropriate temperature at which to evaluate the fluid properties?

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free