/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 15 An electric resistance heater is... [FREE SOLUTION] | 91Ó°ÊÓ

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An electric resistance heater is embedded in a lony cylinder of diameter \(30 \mathrm{~mm}\). When water with a temperature of \(25^{\circ} \mathrm{C}\) and velocity of \(1 \mathrm{~m} / \mathrm{s}\) flows crosswise over the cylinder, the power per unit length required to maintain the surface at a uniform temperature of \(90^{\circ} \mathrm{C}\) is \(28 \mathrm{~kW} / \mathrm{m}\). When air, also at \(25^{\circ} \mathrm{C}\), but with a velocity of \(10 \mathrm{~m} / \mathrm{s}\) is flowing, the power per unit length required to maintain the same surface temperature is \(400 \mathrm{~W} / \mathrm{m}\). Calculate and compare the convection coefficients for the flows of water and air.

Short Answer

Expert verified
Water has a significantly higher convection coefficient (4624.2 W/m²⋅K) than air (65.8 W/m²⋅K), indicating more efficient heat transfer.

Step by step solution

01

Understand the Problem

We need to find the convection coefficients (h) of water and air when they flow at given conditions over a cylinder that is maintained at a certain surface temperature. The power per unit length for water and air is provided as 28 kW/m and 400 W/m, respectively.
02

Use Newton's Law of Cooling

Newton's law of cooling is expressed as:\[ q' = h imes A_s imes (T_s - T_{ ext{fluid}}) \]where:* \( q' \) is the heat transfer per unit length,* \( h \) is the convection heat transfer coefficient,* \( A_s \) is the surface area per unit length (circumference of the cylinder),* \( T_s \) is the surface temperature,* \( T_{\text{fluid}} \) is the fluid temperature.Apply this formula to both water and air to find the convection coefficients.
03

Calculate Surface Area per Unit Length

The cylinder has a diameter \( D = 0.03 \text{ m} \). The surface area per unit length \( A_s \) (circumference) is given by:\[ A_s = \pi imes D = \pi imes 0.03 = 0.0942 \text{ m} \]
04

Calculate Convection Coefficient for Water

For water:\[ q'_w = 28000 \text{ W/m}, \; T_s = 90^{\circ} \text{C}, \; T_{\text{water}} = 25^{\circ} \text{C} \]Substitute into Newton's law:\[ 28000 = h_w imes 0.0942 imes (90 - 25) \]Solve for \( h_w \):\[ h_w = \frac{28000}{0.0942 imes 65} \approx 4624.2 \text{ W/m}^2 \cdot \text{K} \]
05

Calculate Convection Coefficient for Air

For air:\[ q'_a = 400 \text{ W/m}, \; T_s = 90^{\circ} \text{C}, \; T_{\text{air}} = 25^{\circ} \text{C} \]Substitute into Newton's law:\[ 400 = h_a imes 0.0942 imes (90 - 25) \]Solve for \( h_a \):\[ h_a = \frac{400}{0.0942 imes 65} \approx 65.8 \text{ W/m}^2 \cdot \text{K} \]
06

Compare Convection Coefficients

The convection coefficient for water \( h_w = 4624.2 \) W/m²⋅K is significantly higher than that for air \( h_a = 65.8 \) W/m²⋅K. This indicates that water, being a denser fluid with better heat transfer properties, transfers heat more efficiently than air does.

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Key Concepts

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

Newton's Law of Cooling
Newton's Law of Cooling is a fundamental principle in the field of heat transfer. It states that the rate of heat transfer between a solid surface and a fluid flowing past it is directly proportional to the difference in temperature between the surface and the fluid. Mathematically, this is represented as:\[ q' = h \times A_s \times (T_s - T_{fluid}) \]Here,
  • \( q' \) is the heat transfer per unit length,
  • \( h \) is the convection heat transfer coefficient,
  • \( A_s \) is the surface area per unit length of the object,
  • \( T_s \) is the surface temperature, and
  • \( T_{fluid} \) is the fluid temperature.
This law is important because it allows engineers to design systems that efficiently manage heat transfer, such as cooling systems in engines or electronic devices. In the example given, it helps determine how much heat must be added or removed to maintain a specific surface temperature as fluids like water or air pass over a cylinder.
Convection Coefficient
The convection heat transfer coefficient \(h\) is a critical factor in understanding how effectively a fluid can transfer heat to or from a surface. A higher coefficient indicates more efficient heat transfer. This coefficient depends on several factors:
  • The properties of the fluid involved, including viscosity, density, and thermal conductivity.
  • The velocity of the fluid moving across the surface.
  • The nature of the surface, for example, its roughness and shape.
In the context of the exercise, we calculated the convection coefficients for water and air passing over the same cylindrical surface. The calculated value for water was approximately 4624.2 W/m² ⋅ K, considerably higher compared to air's 65.8 W/m² ⋅ K. The reason water has a higher heat transfer efficiency is due to its higher density and better thermal conductivity compared to air.
Cylinder Heat Transfer
When considering heat transfer involving cylindrical objects, like the one in the exercise, the geometry plays a significant role in determining how heat is exchanged between the surface and the fluid. The geometry affects both the surface area available for heat transfer and how the fluid flows around the object.In a cylinder, the surface area per unit length \( A_s \) is determined by its circumference, calculated as:\[ A_s = \pi \times D \]where \( D \) is the diameter of the cylinder.
In the given problem, the cylinder of diameter 0.03 m provides a particular surface over which heat transfer can occur.
This area is crucial as it influences both the heat transfer coefficient \( h \) and the heat transfer rate \( q' \).
Cylindrical heat transfer problems often illustrate how geometry and fluid characteristics define heat exchange efficiency, helping design thermally effective systems or devices.

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Most popular questions from this chapter

The clectrical-substitation radiometer shown schematically determines the optical (radiant) power of a beam by measuring the electrical power required to heat the receiver to the same temperature. With a beam, such as a luser of optical power \(P_{\text {epv }}\) incident on the receiver, its temperature, \(T_{p}\) increases above that of the chamber walls held al a uniform temperature, \(T_{\text {we }}=77 \mathrm{~K}\), With the optical beam blocked, the heater on the hackside of the receiver is encrgized and the electrical power, \(P_{\text {eine: }}\) required to reach the same value of \(T_{\text {, is measured. The }}\) purpose of your analysis is to determine the relationship tetween the clectrical and optical power, considering heat transfer processes experienced by the receiver. Consider a radiomeler with a \(15-\mathrm{mm}\)-diameter receiver having a blackened surface with an emissivity of \(0.95\) and an absorptivity of \(0.98\) for the optical beam. When operating in the optical mode, conduction heat losses from the backside of the receiver are negligible. In the electricul mode, the loss amounts to \(5 \%\) of the electrical power. What is the optical power of a beam when the indicated electrical power is \(20.64 \mathrm{~mW}\) ? What is the corresponding recciver temperature?

The thermal conductivity of a sheet of rigid, extruded insulation is reported to be \(k=0.029 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The measured temperature difference across a 20 -mm-thick sheet of the material is \(T_{1}-T_{2}=10^{F} \mathrm{C}\). (a) What is the heat flux through a \(2 \mathrm{~m} \times 2 \mathrm{~m}\) shect of the insulation? (b) What is the rate of heat transfer through the sheet of insulation?

A square isothermal chip is of width \(w=5 \mathrm{~mm}\) on a side and is mounted in a substrate such that its side and bock surfaces are well insulated, while the front surface is exposed to the flow of a coolant at \(T_{w}=15^{\circ} \mathrm{C}\). From reliatility considerations, the chip temperature must not cxceed \(T=85^{\circ} \mathrm{C}\). Coclart \(\longrightarrow T_{m} h\) If the coolant is air and the corresponding convection coefficient is \(h=200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), what is the maximum allowable chip power? If the coolant is a dielectric liequid for which \(h=3000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}^{\mathrm{K}}\), what is the maximam allowable power?

An instrumentation package has a spherical outer surface of diameter \(D=100 \mathrm{~nm}\) and emissivity \(c=0.25\). The package is placed in a large space simulation chamber whose walls are maintained at \(77 \mathrm{~K}\). If operation of the electronic components is restricted to the lemperature range \(40 \leq 7 \leq 85^{\circ} \mathrm{C}\), what is the range of acceptable power dissipation for the package? Display your results graphically, showing also the effect of variations in the emissivity by censidering values of \(0.20\) and \(0.30\).

A vacuum system, as used in sputiering electrically conducting thin films on microcircuits, is comprised of a buseplate maintained by an electrical heater at \(300 \mathrm{~K}\) and a shroud within the enclosure maintained at \(77 \mathrm{~K}\) by a liquid-nitrogen coolant loop. The circular baseplate, insulated on the lower side, is \(0.3 \mathrm{~m}\) in diameter and has an emissivity of \(0.25\). (a) How much clectrical power must be provided to the baseplate heater? (b) At what rate must liquid nitrogen be supplied to the shiroud if its heat of vaporization is \(125 \mathrm{~kJ} / \mathrm{kg}\) ? (c) To reduce the liquid-nitrogen consumption, it is proposed to bond a thin sheet of aluminura foil \((\varepsilon=0.09)\) to the baseplate. Will this have the desfred effect?

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