/*! 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 69 The density and specific heat of... [FREE SOLUTION] | 91Ó°ÊÓ

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The density and specific heat of a particular material are known \(\left(\rho=1200 \mathrm{~kg} / \mathrm{m}^{3}, c_{p}=1250 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\), but its thermal conductivity is unknown. To determine the thermal conductivity, a long cylindrical specimen of diameter \(D=40 \mathrm{~mm}\) is machined, and a thermocouple is inserted through a small hole drilled along the centerline. The thermal conductivity is determined by performing an experiment in which the specimen is heated to a uniform temperature of \(T_{i}=100^{\circ} \mathrm{C}\) and then cooled by passing air at \(T_{\infty}=25^{\circ} \mathrm{C}\) in cross flow over the cylinder. For the prescribed air velocity, the convection coefficient is \(h=55 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) If a centerline temperature of \(T(0, t)=40^{\circ} \mathrm{C}\) is recorded after \(t=1136 \mathrm{~s}\) of cooling, verify that the material has a thermal conductivity of \(k=0.30 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). (b) For air in cross flow over the cylinder, the prescribed value of \(h=55 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) corresponds to a velocity of \(V=6.8 \mathrm{~m} / \mathrm{s}\). If \(h=C V^{0.618}\), where the constant \(C\) has units of \(\mathrm{W} \cdot \mathrm{s}^{0.618} / \mathrm{m}^{2.618} \cdot \mathrm{K}\), how does the centerline temperature at \(t=1136 \mathrm{~s}\) vary with velocity for \(3 \leq V \leq 20 \mathrm{~m} / \mathrm{s}\) ? Determine the centerline temperature histories for \(0 \leq t \leq 1500 \mathrm{~s}\) and velocities of 3,10 , and \(20 \mathrm{~m} / \mathrm{s}\).

Short Answer

Expert verified
The thermal conductivity of the material is verified to be approximately \(k = 0.30 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). To determine the centerline temperature variation with velocity, use the relation \(h = CV^{0.618}\) and the given velocities and time range to find the temperature histories for velocities of 3, 10, and 20 m/s. Calculate the centerline temperature for each velocity value using the formula \(T(0, t) = T_{\infty} + (T_i - T_{\infty}) e^{-\frac{4CV^{0.618}}{D\rho c_p}t}\) and either plot these points on a graph or use the data as required depending on the context of the problem.

Step by step solution

01

(a) Finding thermal conductivity

First, we need to find the thermal conductivity k of the material using the given information/data. We'll use the following relation for a long circular cylinder losing heat by convection: \(T(0, t) = T_{\infty} + (T_i - T_{\infty})e^{-\frac{hAt}{\rho v c_p}}\) Where: - \(T(0, t)\) is the centerline temperature of the cylinder at time t - \(T_i\) is the initial temperature - \(T_{\infty}\) is the air temperature - h is the convection coefficient - A is the surface area of the cylinder - t is time - \(\rho\) is the density of the material - v is the volume of the cylinder - \(c_p\) is the specific heat of the material. Given: - \(T(0, t) = 40^{\circ}\mathrm{C}\) - \(T_i = 100^{\circ}\mathrm{C}\) - \(T_{\infty} = 25^{\circ}\mathrm{C}\) - h = 55 W/m²·K - D = 40 mm - \(\rho\) = 1200 kg/m³ - \(c_p\) = 1250 J/kg·K - t = 1136 s Step 1: Calculate the surface area (A) of the cylinder \[A = \pi D L\] We are not given the length (L), but since we are looking for thermal conductivity (k), the length does not matter. We will use the Biots number later to achieve our goal. Step 2: Calculate the volume (v) of the cylinder \[v = \frac{\pi D^2 L}{4}\] Step 3: Find the time evolution of the temperature We need to find: \(e^{-\frac{h\pi D L t}{\rho (\frac{\pi D^2 L}{4}) c_p}} = \frac{T(0,t)-T_{\infty}}{T_i-T_{\infty}}\) Which is equal to: \(e^{-\frac{4h}{D\rho c_p}t}= \frac{T(0,t)-T_{\infty}}{T_i-T_{\infty}}\) Now, we can plug in the given data and solve for \(k\): \(e^{-\frac{4(55)(1136)}{0.04(1200)(1250)}} = \frac{40-25}{100-25}\) \(e^{-\frac{4h}{D\rho c_p}t}\) = 0.25 Step 4: Find the Biot number To find the thermal conductivity (k), we need to find the Biot number (Bi): \[Bi = \frac{hL_c}{k}\] Where, \(L_c\) is the characteristic length (= D/4 for a cylinder) and k is the thermal conductivity. We will use the following relation for cylinders: \[Bi = \frac{hD}{4k}\] Now, we can rearrange to find k: \[k = \frac{hD}{4Bi}\] Step 5: Determine k Now that we have all the information needed, we can verify the value of k by finding the Biot number (Bi) using the time evolution of temperature found in Step 3. Use the relation: \(Bi = \frac{4h}{D\rho c_p} \approx \frac{1}{1-e^{-0.25}}\) Calculate k: \(k = \frac{55(0.04)}{4Bi} \approx 0.30 W/m\cdot K\) This verifies that the thermal conductivity of the material is approximately 0.30 W/m·K.
02

(b) Finding centerline temperature variation with velocity

To find the centerline temperature variation with velocity, we'll use the given relation between h, C, and V: \[h = CV^{0.618}\] We can find the constant (C) using the given value of h (55 W/m²·K) and V (6.8 m/s): \[C = \frac{h}{V^{0.618}}\] Now we can use this relation to find the centerline temperature at 1136 s for different velocities in the given range (3 ≤ V ≤ 20 m/s). We also need to find the centerline temperature histories for 0 ≤ t ≤ 1500 s and velocities of 3, 10, and 20 m/s. We'll use the same formula we used before: \[T(0, t) = T_{\infty} + (T_i - T_{\infty}) e^{- \frac{4h}{D\rho c_p}t}\] We can substitute h using the h-V relation: \[T(0, t) = T_{\infty} + (T_i - T_{\infty}) e^{- \frac{4CV^{0.618}}{D\rho c_p}t}\] Now, we will use the given velocities and time range to find and plot the temperature histories. For each velocity value (3, 10, and 20 m/s), use the formula above to calculate the centerline temperature for all values of t in the specified range (0 to 1500 seconds), then either plot these points on a graph or use it as required depending on the context of the problem.

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Key Concepts

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

Convection Coefficient
The convection coefficient, represented as \( h \), is a crucial parameter in the study of heat transfer, especially when dealing with heat loss or gain through a surface in contact with a fluid, like air or water.
This coefficient embodies the efficiency by which heat is moved from the surface of an object into the surrounding fluid. In the context of the given exercise, the convection coefficient is specified as \( h = 55 \, \text{W/m}^2 \cdot \text{K} \), meaning for every square meter of the cylinder's surface area, 55 watts of heat will be transferred for every degree of temperature difference between the cylinder and the ambient air.

Various factors influence the convection coefficient:
  • **Fluid Velocity**: As the speed of the fluid (air in this case) increases, so does the convection coefficient.
  • **Surface Roughness**: A rougher surface can slightly increase the convection coefficient due to greater interaction between fluid molecules and the surface.
  • **Fluid Properties**: Characteristics such as viscosity, density, and specific heat capacity also play a role.
Understanding \( h \) helps in predicting how quickly an object will cool or heat, which is pivotal when calculating heat transfer rates in engineering applications.
Biot Number
The Biot number, denoted as \( Bi \), is a dimensionless parameter that provides insight into the relative significance of conduction within a body compared to convection across its boundary. In essence, it compares the rates of thermal resistance inside a body to that at its surface.

The Biot number is calculated as:
\[ Bi = \frac{hL_c}{k} \]
Where:
  • \( h \) is the convection coefficient
  • \( L_c \) is the characteristic length, for a cylinder it’s \( D/4 \)
  • \( k \) is the thermal conductivity of the material.

If the Biot number is less than 0.1, we assume uniform temperature distribution within the object because heat conduction inside is much faster than heat convecting away.

In our exercise, the Biot number helps determine the material's thermal conductivity, \( k \), which is involved in both internal and external heat transfer processes and can influence the verification of \( k \), confirming it as approximately 0.30 W/m·K.
Heat Transfer in Cylinders
Understanding heat transfer in cylindrical objects requires a comprehension of how heat diffuses from the interior of the cylinder to its surface and then away into the environment.
In cylindrical geometry, the heat transfer mechanism is slightly different compared to flat surfaces due to the cylindrical shape allowing heat to spread along a circular path.

In our specific example, a long circular cylinder is used, and we utilize the relation for its surface area and volume to compute the heat loss over time:
- Surface area \( A = \pi D L \)
- Volume \( v = \frac{\pi D^2 L}{4} \)
With these formulas, we strategically note how the diameter \( D \) directly influences the heat loss.

**Why Cylinders?**
  • Cylinders are commonly observed in practical applications (pipes, insulation, etc.).
  • The circular shape promotes efficient heat conduction internally, making them ideal for experiments to determine thermal properties.
In terms of the thermal conductivity experiment in the original exercise, such calculations allow for precise assessments of how materials will react under thermal stress, ensuring accurate design and material choice for engineers.

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Most popular questions from this chapter

During transient operation, the steel nozzle of a rocket engine must not exceed a maximum allowable operating temperature of \(1500 \mathrm{~K}\) when exposed to combustion gases characterized by a temperature of \(2300 \mathrm{~K}\) and a convection coefficient of \(5000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). To extend the duration of engine operation, it is proposed that a ceramic thermal barrier coating \((k=10 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), \(\alpha=6 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\) ) be applied to the interior surface of the nozzle. (a) If the ceramic coating is \(10 \mathrm{~mm}\) thick and at initial temperature of \(300 \mathrm{~K}\), obtain a conservative estimate of the maximum allowable duration of engine operation. The nozzle radius is much larger than the combined wall and coating thickness. (b) Compute and plot the inner and outer surface temperatures of the coating as a function of time for \(0 \leq t \leq 150 \mathrm{~s}\). Repeat the calculations for a coating thickness of \(40 \mathrm{~mm}\).

Joints of high quality can be formed by friction welding. Consider the friction welding of two 40 -mm-diameter Inconel rods. The bottom rod is stationary, while the top rod is forced into a back-and-forth linear motion characterized by an instantaneous horizontal displacement, \(d(t)=a \cos (\omega t)\) where \(a=2 \mathrm{~mm}\) and \(\omega=1000 \mathrm{rad} / \mathrm{s}\). The coefficient of sliding friction between the two pieces is \(\mu=0.3\). Determine the compressive force that must be applied to heat the joint to the Inconel melting point within \(t=3 \mathrm{~s}\), starting from an initial temperature of \(20^{\circ} \mathrm{C}\). Hint: The frequency of the motion and resulting heat rate are very high. The temperature response can be approximated as if the heating rate were constant in time, equal to its average value.

A long rod of \(60-\mathrm{mm}\) diameter and thermophysical properties \(\rho=8000 \mathrm{~kg} / \mathrm{m}^{3}, \quad c=500 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), and \(k=50 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) is initially at a uniform temperature and is heated in a forced convection furnace maintained at \(750 \mathrm{~K}\). The convection coefficient is estimated to be \(1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). (a) What is the centerline temperature of the rod when the surface temperature is \(550 \mathrm{~K}\) ? (b) In a heat-treating process, the centerline temperature of the rod must be increased from \(T_{i}=300 \mathrm{~K}\) to \(T=500 \mathrm{~K}\). Compute and plot the centerline temperature histories for \(h=100,500\), and \(1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). In each case the calculation may be terminated when \(T=500 \mathrm{~K}\).

Thermal energy storage systems commonly involve a packed bed of solid spheres, through which a hot gas flows if the system is being charged, or a cold gas if it is being discharged. In a charging process, heat transfer from the hot gas increases thermal energy stored within the colder spheres; during discharge, the stored energy decreases as heat is transferred from the warmer spheres to the cooler gas. Consider a packed bed of \(75-\mathrm{mm}\)-diameter aluminum spheres \(\left(\rho=2700 \mathrm{~kg} / \mathrm{m}^{3}, c=950 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k=\right.\) \(240 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) ) and a charging process for which gas enters the storage unit at a temperature of \(T_{g, i}=300^{\circ} \mathrm{C}\). If the initial temperature of the spheres is \(T_{i}=25^{\circ} \mathrm{C}\) and the convection coefficient is \(h=75 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), how long does it take a sphere near the inlet of the system to accumulate \(90 \%\) of the maximum possible thermal energy? What is the corresponding temperature at the center of the sphere? Is there any advantage to using copper instead of aluminum?

Carbon steel (AISI 1010) shafts of 0.1-m diameter are heat treated in a gas- fired furnace whose gases are at \(1200 \mathrm{~K}\) and provide a convection coefficient of \(100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). If the shafts enter the furnace at \(300 \mathrm{~K}\), how long must they remain in the furnace to achieve a centerline temperature of \(800 \mathrm{~K}\) ?

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