/*! 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 9 An experiment to study heat tran... [FREE SOLUTION] | 91Ó°ÊÓ

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An experiment to study heat transfer from an elliptical cylinder was performed in a wind tunnel. Heat loss from a cylinder of major and minor axes 8 and \(6 \mathrm{~cm}\), respectively, to an air flow normal to the minor axis of the cylinder was measured. Heat loss from the cylinder consisted of both radiation and convection. The measured total heat loss, and a calculation of the radiation contribution for each test condition, are listed here. (The radiation calculation was based on an emittance of \(0.8\) for the cylinder surface.) Use the data to estimate the convective heat loss from a geometrically similar cylinder of \(12 \mathrm{~cm}\) major axis at \(30^{\circ} \mathrm{C}\) to a \(4.5 \mathrm{~m} / \mathrm{s}\) air flow at \(23^{\circ} \mathrm{C}\). $$ \begin{array}{cccccc} \text { Test } & V & T_{s} & T_{e} & q_{\mathrm{rad}} & q_{\text {total }} \\ \text { W/s } & \text { K } & \text { K } & \text { W/m }^{2} & \text { W/m }^{2} \\ \hline 1 & 1.37 & 327.5 & 304.3 & 133 & 585 \\ 2 & 2.83 & 309.4 & 301.5 & 42 & 261 \\ 3 & 3.54 & 304.7 & 291.6 & 65 & 553 \\ 4 & 6.10 & 306.1 & 301.4 & 23 & 261 \\ 5 & 8.63 & 302.8 & 297.9 & 24 & 403 \\ 6 & 8.50 & 311.5 & 305.9 & 32 & 410 \\ 7 & 8.81 & 309.2 & 304.4 & 26 & 402 \\ 8 & 8.32 & 299.5 & 292.7 & 35 & 552 \\ 9 & 11.5 & 308.2 & 304.5 & 18 & 466 \\ 10 & 11.4 & 307.0 & 301.8 & 26 & 548 \\ 11 & 14.8 & 306.3 & 302.4 & 19 & 546 \\ 12 & 17.5 & 302.2 & 298.8 & 16 & 577 \end{array} $$

Short Answer

Expert verified
Calculate the convective heat loss using regression to find the relationship with velocity, apply the model for new conditions, and adjust for geometrical similarity.

Step by step solution

01

Understand the Given Data

The data table provides details such as air velocity \(V\), surface temperature \(T_s\), environmental temperature \(T_e\), total heat loss \(q_{\text{total}}\), and radiation heat loss \(q_{\text{rad}}\) for different tests. Our goal is to estimate the convective heat loss of a different cylinder under specific conditions.
02

Convective Heat Loss Calculation

For each test, we start by calculating the convective heat loss using the formula: \(q_{\text{conv}} = q_{\text{total}} - q_{\text{rad}}\). For example, for Test 1, \(q_{\text{conv}} = 585 - 133 = 452\) W/m². Repeat this calculation to obtain \(q_{\text{conv}}\) for all tests.
03

Fit Convective Heat Loss vs. Velocity

Using the convective heat loss values from Step 2 and the corresponding air velocity \(V\), fit a model that describes the relationship between convective heat loss \(q_{\text{conv}}\) and velocity \(V\). This can typically be done using a power law model \(q_{\text{conv}} = aV^b\), where \(a\) and \(b\) are constants determined through regression.
04

Apply the Model to New Conditions

With the constants \(a\) and \(b\) identified, apply the model to estimate \(q_{\text{conv}}\) under the new conditions where \(V = 4.5\) m/s. Calculate \(q_{\text{conv,new}} = a(4.5)^b\).
05

Adjust for Geometrical Similarity

Since the new cylinder is geometrically similar but has a different size, adjust the convective heat loss by considering the scale factor of geometry, which affects the surface area and thereby the total heat loss. The scale factor can typically be accounted for by the ratio of the diameters of the two cylinders, \((12\ cm/8\ cm)\), raised to a power depending on the nature of heat transfer.
06

Calculate Final Estimate

The final estimate of the convective heat loss for the new cylinder is obtained by multiplying the previous result by any necessary scale factors due to the cylinder size change. The final adjusted convective heat loss can thus be written as: \(q_{\text{conv,new,adjusted}} = q_{\text{conv,new}} \times (\text{scale factor})\).

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Key Concepts

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

Elliptical Cylinder
The elliptical cylinder is an important shape to study in heat transfer problems. Unlike regular cylindrical shapes, which are circular in cross-section, elliptical cylinders have an oval cross-section. This makes them intriguing for several applications because their geometry affects how heat is transferred by affecting air flow around their surface.
In the exercise, we have a cylinder with major and minor axes of 8 cm and 6 cm respectively. The major axis is the longer line across the oval shape, while the minor axis is the shorter line.
Understanding the orientation is crucial since air passing around the cylinder hits the shape differently depending on whether it flows against the major or minor axis. This impacts the heat loss calculations, particularly how convection and radiation contribute under various conditions.
Heat Loss Calculation
Heat loss in an object involves understanding two main components: radiant heat loss and convective heat loss. The total heat loss is essentially the sum of these two components.
  • Radiant Heat Loss (\( q_{\text{rad}} \)): This form of heat loss occurs through radiation, where the surface emits heat to its surroundings without any contact. It is influenced by factors like surface temperature and emittance (which in this case is 0.8).
  • Convective Heat Loss (\( q_{\text{conv}} \)): This kind of heat loss occurs due to the movement of air across the surface. It's affected by the speed of the air stream and the temperature difference between the surface and the surrounding environment.
In the exercise, you calculate the convective heat loss by subtracting the radiant heat from the total heat, as shown by: \( q_{\text{conv}} = q_{\text{total}} - q_{\text{rad}} \). This helps isolate how much heat is being lost simply through convection.
Wind Tunnel Experiments
Wind tunnel experiments are used to simulate and study the behavior of air-flow over objects, in this instance, the elliptical cylinder. Such experiments are essential for measuring convective heat loss accurately as they replicate conditions that the cylinder would face in natural air flow.
These tunnels are designed to control variables like air velocity and temperature, which allows us to systematically study their effect on heat transfer. In our problem, different velocities are considered, simulating various wind conditions, from light breezes to stronger winds.
By capturing this data, researchers can extract precise figures for total and convective heat loss under each scenario, which are necessary for creating reliable models for prediction.
Geometry Scaling in Heat Transfer
When scaling up or down a geometric body, like moving from an 8 cm to a 12 cm major axis, the heat transfer characteristics change. This is because the surface area, or the size of the cylinder, has a direct impact on how heat is lost through convection.
The scale factor, which is the ratio of the new dimension to the old dimension (\( \frac{12 \ cm}{8 \ cm} \)), plays a crucial role. Larger areas tend to have different transfer rates, often requiring calculations or models to adjust predictions appropriately.
In our context, understanding this ratio helps adjust the convective heat loss calculated for a different sized cylinder, ensuring that the model remains accurate even with changes in size.

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Most popular questions from this chapter

Consider the packing of a perforatedplate heat exchanger for a cryogenic refrigeration system. Geometric parameters include the hole diameter \(d\), hole pitch \(p\) (or, alternatively, the open-area ratio \(\varepsilon_{p}\) ), the plate thickness \(t\), and plate spacing \(s\). Expected parameter values for a hydrogen flow include a mass velocity based on a hole cross-sectional area of \(6 \times 10^{-3}\) \(\mathrm{kg} / \mathrm{m}^{2} \mathrm{~s}\), a pressure of \(100 \mathrm{~Pa}\), temperature temperature differences of \(10 \mathrm{~K}\). Hole diameters are in the range \(1-3 \mathrm{~mm}\). Suggest appropriate dimensionless groups for correlating experimental data for pressure drop and heat transfer.

Insulating wet suits worn by scuba divers may be made of \(3 \mathrm{~mm}\)-thick foam neoprene \((k=0.05 \mathrm{~W} / \mathrm{m} \mathrm{K})\), which traps next to the skin a layer of water, say 1 \(\mathrm{mm}\) thick. Estimate the rate of heat loss from a \(1.8 \mathrm{~m}\)-tall diver swimming at 8 \(\mathrm{km} / \mathrm{h}\) in \(286 \mathrm{~K}\) water if his skin temperature does not fall below \(297 \mathrm{~K}\).

A laminar flow in a \(2 \mathrm{~cm}-\mathrm{I}\).D. tube has the following velocity and temperature profiles: $$ \begin{aligned} u &=0.1\left[1-(r / 0.01)^{2}\right] \mathrm{m} / \mathrm{s} \\ T &=400-3 \times 10^{6}\left(1.875 \times 10^{-5}-0.25 r^{2}+624 r^{4}\right) \mathrm{K} \end{aligned} $$ for \(r\) in meters. Determine the bulk temperature.

Liquid metals are attractive for high-temperature heat transfer applications owing to their characteristic high convective heat transfer coefficients. Liquid potassium flows at \(4 \mathrm{~m} / \mathrm{s}\) in a long, \(2 \mathrm{~cm}\)-I.D. tube. Calculate the Nusselt number and heat transfer coefficient (i) for a uniform wall temperature. (ii) for a uniform wall heat flux. Evaluate properties at \(900 \mathrm{~K}\). Repeat for liquid sodium.

A \(20 \mathrm{~cm}\)-square hot plate is maintained at \(150^{\circ} \mathrm{C}\) in ambient air at \(20^{\circ} \mathrm{C}, 1 \mathrm{~atm}\). If its emittance is \(0.8\), determine the convective and radiative heat losses from its upper surface.

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