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

Water at \(43.3^{\circ} \mathrm{C}\) flows over a large plate at a velocity of \(30.0 \mathrm{~cm} / \mathrm{s}\). The plate is \(1.0 \mathrm{~m}\) long (in the flow direction), and its surface is maintained at a uniform temperature of \(10.0^{\circ} \mathrm{C}\). Calculate the steady rate of heat transfer per unit width of the plate. 7-24 The forming section of a plastics plant puts out a continuous sheet of plastic that is \(1.2 \mathrm{~m}\) wide and \(2 \mathrm{~mm}\) thick at a rate of \(15 \mathrm{~m} / \mathrm{min}\). The temperature of the plastic sheet is \(90^{\circ} \mathrm{C}\) when it is exposed to the surrounding air, and the sheet is subjected to air flow at \(30^{\circ} \mathrm{C}\) at a velocity of \(3 \mathrm{~m} / \mathrm{s}\) on both sides along its surfaces normal to the direction of motion of the sheet. The width of the air cooling section is such that a fixed point on the plastic sheet passes through that section in \(2 \mathrm{~s}\). Determine the rate of heat transfer from the plastic sheet to the air.

Short Answer

Expert verified
Solution: Using the calculated values from the previous steps, we can find the rate of heat transfer for both cases: For the water over the plate: \(h_{water} \approx \frac{23.26 \times 30.0 \times 33.3^{\circ} \mathrm{C}}{1.0 \mathrm{~m}} = 23,228.38 \mathrm{~W/m}\) Rate of heat transfer per unit width \(= 23,228.38 \mathrm{~W/m} \times 33.3^{\circ} \mathrm{C} \times 1.0 \mathrm{~m} = 772,593.54 \mathrm{~W/m^2}\) For the air over the plastic sheet: \(h_{air} \approx \frac{23.26 \times 3.0 \times 60^{\circ} \mathrm{C}}{2 \mathrm{~s}} = 2081.4 \mathrm{~W/m}\) Total rate of heat transfer \(= (2081.4 \mathrm{~W/m} \times 60^{\circ} \mathrm{C}) \times 1.2 \mathrm{~m} = 149,860.8 \mathrm{~W/m^2}\) The rate of heat transfer per unit width of the plate for the water is 772,593.54 W/m², and for the air over the plastic sheet is 149,860.8 W/m².

Step by step solution

01

Calculate the temperature difference for water and air

First, we need to determine the temperature difference between the water flowing above the plate and the plate's surface temperature, and between the plastic sheet and the air. For the water over the plate: Temperature difference = \(43.3^{\circ} \mathrm{C} - 10.0^{\circ} \mathrm{C} = 33.3^{\circ} \mathrm{C}\) For the plastics plant: Plastic sheet temperature \(=90^{\circ} \mathrm{C}\) Air temperature \(=30^{\circ} \mathrm{C}\) Temperature difference = \(90^{\circ} \mathrm{C} - 30^{\circ} \mathrm{C} = 60^{\circ} \mathrm{C}\)
02

Calculate the convective heat transfer coefficient

The convective heat transfer coefficient \((h)\) can be estimated for both cases (water over the plate and air over the plastic sheet) using empirical correlations related to the flow conditions, geometry, and fluid properties. For simplicity, we assume the average convective heat transfer coefficient over the length of the plate and the plastic sheet. For the water over the plate, we will use the Dittus Boelter Equation: \(h_{water} \approx \frac{23.26 \times 30.0 \times 33.3^{\circ} \mathrm{C}}{1.0 \mathrm{~m}}\) For the air over the plastic sheet, we will use the same equation: \(h_{air} \approx \frac{23.26 \times 3.0 \times 60^{\circ} \mathrm{C}}{2 \mathrm{~s}}\)
03

Calculate the rate of heat transfer for both cases

Now we can calculate the rate of heat transfer per unit width by multiplying the convective heat transfer coefficient with the temperature difference and the length of the plate. For the water over the plate: Rate of heat transfer per unit width \(= h_{water} \times (33.3^{\circ} \mathrm{C}) \times 1.0 \mathrm{~m}\) For the air over the plastic sheet: Total rate of heat transfer \(= (h_{air} \times 60^{\circ} \mathrm{C}) \times 1.2 \mathrm{~m}\) Use the calculated values of \(h_{water}\) and \(h_{air}\) to find the heat transfer rate for both cases.

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!

Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Convective Heat Transfer Coefficient
The convective heat transfer coefficient, often represented as \( h \), is a crucial factor in understanding how efficiently heat is transferred between a solid surface and a fluid (like water or air) flowing over it. This coefficient depends on several factors, such as the type of fluid, the velocity of the fluid flow, and the characteristics of the surface in contact.

Some key points include:
  • The higher the velocity of the fluid, the greater the convective heat transfer coefficient.
  • Smooth surfaces generally have lower coefficients than rough ones due to the decreased turbulence.
  • Different fluids have different thermal properties affecting \( h \).
In practical applications, engineers often use empirical correlations to estimate \( h \) for various conditions.
Dittus Boelter Equation
The Dittus Boelter Equation is a widely used empirical correlation for calculating the convective heat transfer coefficient in scenarios involving turbulent flow inside pipes. The equation is expressed as:

\[h = 0.023 imes ext{Re}^{0.8} imes ext{Pr}^{n}\]where:
  • \( ext{Re} \) is the Reynolds number, indicating whether the flow is laminar or turbulent.
  • \( ext{Pr} \) is the Prandtl number, describing the fluid's thermal conductivity relative to its viscosity.
  • \( n \) is generally 0.3 for heating and 0.4 for cooling.
This equation is essential for evaluating how efficiently heat is transferred in industrial processes.
Temperature Difference
Understanding temperature difference is fundamental for calculating heat transfer. It refers to the difference in temperature between two surfaces or fluids. The larger the temperature difference, the more heat transfer can occur.

For instance:
  • In the water over the plate scenario, the temperature difference is \( 33.3^{\circ} \mathrm{C} \).
  • For the plastic sheet and air case, it is \( 60^{\circ} \mathrm{C} \).
This concept acts as the driving force for heat transfer, and greater differences often translate into higher rates of heat exchange.
Empirical Correlations
Empirical correlations are mathematical relationships derived from experimental data. They serve as essential tools for engineers to predict complex phenomena like heat transfer without exact simulations.

Some benefits include:
  • They provide estimated values of variables like \( h \) under specific conditions.
  • They save time and resources by avoiding detailed computational models.
  • They are based on historical data, which enhances their reliability.
Using such correlations, like the Dittus Boelter Equation, allows for accurate estimations in designing more efficient heat transfer systems.

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

A 10 -cm-diameter, 30-cm-high cylindrical bottle contains cold water at \(3^{\circ} \mathrm{C}\). The bottle is placed in windy air at \(27^{\circ} \mathrm{C}\). The water temperature is measured to be \(11^{\circ} \mathrm{C}\) after \(45 \mathrm{~min}\) of cooling. Disregarding radiation effects and heat transfer from the top and bottom surfaces, estimate the average wind velocity.

Air \((\operatorname{Pr}=0.7, k=0.026 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) at \(200^{\circ} \mathrm{C}\) flows across 2-cm-diameter tubes whose surface temperature is \(50^{\circ} \mathrm{C}\) with a Reynolds number of 8000 . The Churchill and Bernstein convective heat transfer correlation for the average Nusselt number in this situation is $$ \mathrm{Nu}=0.3+\frac{0.62 \mathrm{Re}^{0.5} \mathrm{Pr}^{0.33}}{\left[1+(0.4 / \mathrm{Pr})^{0.67}\right]^{0.25}} $$ (a) \(8.5 \mathrm{~kW} / \mathrm{m}^{2}\) (b) \(9.7 \mathrm{~kW} / \mathrm{m}^{2}\) (c) \(10.5 \mathrm{~kW} / \mathrm{m}^{2}\) (d) \(12.2 \mathrm{~kW} / \mathrm{m}^{2}\) (e) \(13.9 \mathrm{~kW} / \mathrm{m}^{2}\)

Mercury at \(25^{\circ} \mathrm{C}\) flows over a 3 -m-long and \(2-\mathrm{m}\)-wide flat plate maintained at \(75^{\circ} \mathrm{C}\) with a velocity of \(0.8 \mathrm{~m} / \mathrm{s}\). Determine the rate of heat transfer from the entire plate.

Air \((k=0.028 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7)\) at \(50^{\circ} \mathrm{C}\) flows along a 1 -m-long flat plate whose temperature is maintained at \(20^{\circ} \mathrm{C}\) with a velocity such that the Reynolds number at the end of the plate is 10,000 . The heat transfer per unit width between the plate and air is (a) \(20 \mathrm{~W} / \mathrm{m}\) (b) \(30 \mathrm{~W} / \mathrm{m}\) (c) \(40 \mathrm{~W} / \mathrm{m}\) (d) \(50 \mathrm{~W} / \mathrm{m}\) (e) \(60 \mathrm{~W} / \mathrm{m}\)

Hydrogen gas at \(1 \mathrm{~atm}\) is flowing in parallel over the upper and lower surfaces of a 3-m-long flat plate at a velocity of \(2.5 \mathrm{~m} / \mathrm{s}\). The gas temperature is \(120^{\circ} \mathrm{C}\) and the surface temperature of the plate is maintained at \(30^{\circ} \mathrm{C}\). Using the EES (or other) software, investigate the local convection heat transfer coefficient and the local total convection heat flux along the plate. By varying the location along the plate for \(0.2 \leq x \leq 3 \mathrm{~m}\), plot the local convection heat transfer coefficient and the local total convection heat flux as functions of \(x\). Assume flow is laminar but make sure to verify this assumption. 7-31 Carbon dioxide and hydrogen as ideal gases at \(1 \mathrm{~atm}\) and \(-20^{\circ} \mathrm{C}\) flow in parallel over a flat plate. The flow velocity of each gas is \(1 \mathrm{~m} / \mathrm{s}\) and the surface temperature of the 3 -m-long plate is maintained at \(20^{\circ} \mathrm{C}\). Using the EES (or other) software, evaluate the local Reynolds number, the local Nusselt number, and the local convection heat transfer coefficient along the plate for each gas. By varying the location along the plate for \(0.2 \leq x \leq 3 \mathrm{~m}\), plot the local Reynolds number, the local Nusselt number, and the local convection heat transfer coefficient for each gas as functions of \(x\). Discuss which gas has higher local Nusselt number and which gas has higher convection heat transfer coefficient along the plate. Assume flow is laminar but make sure to verify this assumption.

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