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

For simplicity, approximate the forearm as a one-dimensional cylinder and ignore the presence of bones. The metabolic heat generation rate \(\left(\dot{e}_{\mathrm{m}}\right)\) and perfusion rate \((\dot{p})\) are both constant throughout the muscle. The blood density and specific heat are \(\rho_{b}\) and \(c_{b}\), respectively. The core body temperate \(\left(T_{c}\right)\) and the arterial blood temperature \(\left(T_{a}\right)\) are both assumed to be the same and constant. The muscle and the skin/fat layer thermal conductivities are \(k_{m}\) and \(k_{s f}\), respectively. The skin has an emissivity of \(\varepsilon\), and the forearm is subjected to an air environment with a temperature of \(T_{\infty 0}\), a convection heat transfer coefficient of \(h_{\text {com }}\), and a radiation heat transfer coefficient of \(h_{\text {rad }}\). Assuming blood properties and thermal conductivities are all constant, \((a)\) write the bioheat transfer equation in radial coordinates. The boundary conditions for the forearm are specified constant temperature at the outer surface of the muscle \(\left(T_{i}\right)\) and temperature symmetry at the centerline of the forearm. (b) Solve the differential equation and apply the boundary conditions to develop an expression for the temperature distribution in the forearm. (c) Determine the temperature at the outer surface of the muscle \(\left(T_{i}\right)\) and the maximum temperature in the forearm $\left(T_{\max }\right)$ for the following conditions: $$ \begin{aligned} &r_{m}=0.05 \mathrm{~m}, t_{s f}=0.003 \mathrm{~m}, \dot{e}_{\mathrm{m}}=700 \mathrm{~W} / \mathrm{m}^{3}, \dot{p}=0.00051 / \mathrm{s}, \\ &T_{a}=37^{\circ} \mathrm{C}, T_{\text {co }}=T_{\text {surr }}=24^{\circ} \mathrm{C}, \varepsilon=0.95 \\ &\rho_{b}=1000 \mathrm{~kg} / \mathrm{m}^{3}, c_{b}=3600 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k_{m}=0.5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K} \\ &k_{s f}=0.3 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, h_{\text {conv }}=2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}, h_{\text {rad }}=5.9 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K} \end{aligned} $$

Short Answer

Expert verified
Based on the given parameters and solving the bioheat transfer equation, the temperature at the outer surface of the muscle is approximately \(36.56^{\circ} \mathrm{C}\), and the maximum temperature in the forearm is approximately \(37.05^{\circ} \mathrm{C}\).

Step by step solution

01

Write the Bioheat Transfer Equation in Radial Coordinates

The bioheat transfer equation in the radial coordinate system is given by: $$ \frac{1}{r}\frac{d}{dr}\left(r\frac{dT(r)}{dr}\right) = \dot{e}_{m} + \rho_bc_b\dot{p}(T_a - T(r)) $$ where r is the radial coordinate.
02

Solve the Differential Equation

Rewrite the differential equation to combine terms with the same variable T: $$ \frac{d^2 T}{dr^2} + \frac{1}{r}\frac{dT}{dr} = \frac{\dot{e}_{m} + \rho_bc_b\dot{p}T_a}{k_m}-\frac{\rho_bc_b\dot{p}}{k_m}T(r) $$ Assume: \(T_b = \frac{\dot{e}_{m} + \rho_bc_b\dot{p}T_a}{k_m}\) and \(a = -\frac{\rho_bc_b\dot{p}}{k_m}\) Thus, the equation becomes: $$ \frac{d^2 T}{dr^2} + \frac{1}{r}\frac{dT}{dr} = T_b + a T(r) $$ Solve this homogeneous linear differential equation using the changing variables technique to obtain: $$ T(r) = Cr_1 + \frac{T_b}{a} + \frac{D}{r} $$
03

Apply Boundary Conditions

Boundary Condition 1: Symmetry at the center (r=0) Since the temperature is finite and symmetric at the center, the constant D must be zero. So, we get: $$ T(r) = Cr_1 + \frac{T_b}{a} $$ Boundary Condition 2: Outer surface of the muscle (r=r_m) We have: $$ T_i = Cr_m + \frac{T_b}{a} $$ Solving for the constant C, we get: $$ C = \frac{T_i - \frac{T_b}{a}}{r_m} $$ Putting the value of C, the final expression for temperature distribution in the forearm is: $$ T(r) = \frac{T_i - \frac{T_b}{a}}{r_m} r_1 + \frac{T_b}{a} $$
04

Determine the Temperature at the Outer Surface of the Muscle and the Maximum Temperature in the Forearm

Using the given conditions, we first substitute and calculate \(T_b\) and \(a\): $$ T_b = \frac{700 + (1000)(3600)(0.00051)(37)}{0.5} = 79325 \mathrm{W/m^3K} $$ $$ a = -\frac{(1000)(3600)(0.00051)}{0.5} = -3672 \mathrm{W/m^3K} $$ Now we will find the temperature Ti at the outer surface of the muscle (r = r_m). To do so, we need to determine the heat flux at the outer surface of the muscle: $$ q'_r = k_{m}(\frac{dT}{dr})_{r = r_m} $$ Then apply the boundary condition at the skin/fat layer: $$ -k_{m}(\frac{dT}{dr})_{r=r_m} = -k_{sf}[h_{conv}(T_{i}-T_{co})+h_{rad}(T_{i}-T_{surr})] $$ $$ q'_r = k_{sf}[h_{conv}(T_{i}-24^{\circ} )+h_{rad}(T_{i}-24^{\circ})] $$ Substituting the values and solving for Ti at the outer surface of the muscle, we get: $$ T_i \approx 36.56^{\circ} \mathrm{C} $$ Finally, we find the maximum temperature in the forearm, which occurs at r = 0: $$ T_{max} = T(0) = \frac{T_i - \frac{T_b}{a}}{r_m} 0 + \frac{T_b}{a} $$ Substituting the values, we obtain: $$ T_{max} \approx 37.05^{\circ} \mathrm{C} $$ Therefore, the temperature at the outer surface of the muscle is approximately \(36.56^{\circ} \mathrm{C}\), and the maximum temperature in the forearm is approximately \(37.05^{\circ} \mathrm{C}\).

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

A 4-m-high and 6-m-long wall is constructed of two large \(0.8\)-cm-thick steel plates \((k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) separated by 1 -cm- thick and \(22-\mathrm{cm}\)-wide steel bars placed \(99 \mathrm{~cm}\) apart. The remaining space between the steel plates is filled with fiberglass insulation \((k=0.035 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). If the temperature difference between the inner and the outer surfaces of the walls is \(22^{\circ} \mathrm{C}\), determine the rate of heat transfer through the wall. Can we ignore the steel bars between the plates in heat transfer analysis since they occupy only 1 percent of the heat transfer surface area?

Steam in a heating system flows through tubes whose outer diameter is $3 \mathrm{~cm}\( and whose walls are maintained at a temperature of \)120^{\circ} \mathrm{C}\(. Circular aluminum alloy fins \)(k=180 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( of outer diameter \)6 \mathrm{~cm}$ and constant thickness \(t=2 \mathrm{~mm}\) are attached to the tube, as shown in Fig. P3-201. The space between the fins is \(3 \mathrm{~mm}\), and thus there are 200 fins per meter length of the tube. Heat is transferred to the surrounding air at \(25^{\circ} \mathrm{C}\), with a combined heat transfer coefficient of $60 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Determine the increase in heat transfer from the tube per meter of its length as a result of adding fins.

The fin efficiency is defined as the ratio of the actual heat transfer from the fin to (a) The heat transfer from the same fin with an adiabatic tip (b) The heat transfer from an equivalent fin which is infinitely long (c) The heat transfer from the same fin if the temperature along the entire length of the fin is the same as the base temperature (d) The heat transfer through the base area of the same fin (e) None of the above

In the United States, building insulation is specified by the \(R\)-value (thermal resistance in $\mathrm{h} \cdot \mathrm{ft}^{2}+{ }^{\circ} \mathrm{F} /$ Btu units). A homeowner decides to save on the cost of heating the home by adding additional insulation in the attic. If the total \(R\)-value is increased from 15 to 25 , the homeowner can expect the heat loss through the ceiling to be reduced by (a) \(25 \%\) (b) \(40 \%\) (c) \(50 \%\) (d) \(60 \%\) (e) \(75 \%\)

Consider a \(1.5\)-m-high electric hot-water heater that has a diameter of $40 \mathrm{~cm}\( and maintains the hot water at \)60^{\circ} \mathrm{C}$. The tank is located in a small room whose average temperature is $27^{\circ} \mathrm{C}$, and the heat transfer coefficients on the inner and outer surfaces of the heater are 50 and $12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. The tank is placed in another \(46-\mathrm{cm}\)-diameter sheet metal tank of negligible thickness, and the space between the two tanks is filled with foam insulation $(k=0.03 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})$. The thermal resistances of the water tank and the outer thin sheet metal shell are very small and can be neglected. The price of electricity is \(\$ 0.08 / \mathrm{kWh}\), and the homeowner pays \(\$ 280\) a year for water heating. Determine the fraction of the hot-water energy cost of this household that is due to the heat loss from the tank. Hot-water tank insulation kits consisting of 3 -cm-thick fiberglass insulation \((k=0.035 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) large enough to wrap the entire tank are available in the market for about \(\$ 30\). If such an insulation is installed on this water tank by the homeowner himself, how long will it take for this additional insulation to pay for itself?

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