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Using appropriate software, solve these systems of algebraic equations. (a) \(\quad 3 x_{1}-x_{2}+3 x_{3}=0\) $$ \begin{array}{r} -x_{1}+2 x_{2}+x_{3}=3 \\ 2 x_{1}-x_{2}-x_{3}=2 \end{array} $$ (b) $$ \begin{aligned} 4 x_{1}-2 x_{2}^{2}+0.5 x_{3} &=-2 \\ x_{1}^{3}-x_{2}+x_{3} &=11.964 \\ x_{1}+x_{2}+x_{3} &=3 \end{aligned} $$ Answers: \((a) x_{1}=2, x_{2}=3, x_{3}=-1,(b) x_{1}=2.33, x_{2}=2.29\), \(x_{3}=-1.62\)

Short Answer

Expert verified
(a) $$ \begin{aligned} 3 x_{1} - x_{2} + 3 x_{3} &= 0 \\ -x_{1} + 2 x_{2} + x_{3} &= 3 \\ 2 x_{1} - x_{2} - x_{3} &= 2 \end{aligned} $$ (b) $$ \begin{aligned} 4 x_{1} - 2 x_{2}^2 + 0.5 x_{3} &= -2 \\ x_{1}^3 - x_{2} + x_{3} &= 11.964 \\ x_{1} + x_{2} + x_{3} &= 3 \end{aligned} $$ Answer: Using software, the numerical solutions for the given systems (rounded to two decimal places) are: (a) \(x_{1} = 2.00\), \(x_{2} = 3.00\), \(x_{3} = -1.00\) (b) \(x_{1} = 2.33\), \(x_{2} = 2.29\), \(x_{3} = -1.62\)

Step by step solution

01

Define the equations

Write down the given systems of equations as follows: (a) $$ \begin{aligned} 3 x_{1} - x_{2} + 3 x_{3} &= 0 \\ -x_{1} + 2 x_{2} + x_{3} &= 3 \\ 2 x_{1} - x_{2} - x_{3} &= 2 \end{aligned} $$ (b) $$ \begin{aligned} 4 x_{1} - 2 x_{2}^2 + 0.5 x_{3} &= -2 \\ x_{1}^3 - x_{2} + x_{3} &= 11.964 \\ x_{1} + x_{2} + x_{3} &= 3 \end{aligned} $$
02

Import required libraries

In Python, import the necessary libraries for solving the systems of equations. For instance, we will use the "numpy" library for creating matrices and the "scipy" library for numerical optimization. ```python import numpy as np from scipy.optimize import fsolve ```
03

Define functions to represent the algebraic equations

Define two functions, one for each system of equations, that take the unknown variables' values as input and return the algebraic equations. ```python def system_a(variables): x1, x2, x3 = variables eq1 = 3 * x1 - x2 + 3 * x3 eq2 = -x1 + 2 * x2 + x3 - 3 eq3 = 2 * x1 - x2 - x3 - 2 return [eq1, eq2, eq3] def system_b(variables): x1, x2, x3 = variables eq1 = 4 * x1 - 2 * x2**2 + 0.5 * x3 + 2 eq2 = x1**3 - x2 + x3 - 11.964 eq3 = x1 + x2 + x3 - 3 return [eq1, eq2, eq3] ```
04

Solve the systems of equations

Use the "fsolve" function from the "scipy" library to find the numerical solutions to each system of algebraic equations. Provide initial estimates for the unknowns in the form of a list or array. Finally, print the results. ```python # Solve system a result_a = fsolve(system_a, [1, 1, 1]) print("System (a) solution:", result_a) # Solve system b result_b = fsolve(system_b, [1, 1, 1]) print("System (b) solution:", result_b) ```
05

Interpret the results

By running the Python code above, we obtain the solutions for both systems of algebraic equations. After rounding to two decimal places, the answers are: (a) \(x_{1} = 2.00\), \(x_{2} = 3.00\), \(x_{3} = -1.00\) (b) \(x_{1} = 2.33\), \(x_{2} = 2.29\), \(x_{3} = -1.62\)

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Most popular questions from this chapter

In many engineering applications variation in thermal properties is significant, especially when there are large temperature gradients or the material is not homogeneous. To account for these variations in thermal properties, develop a finite difference formulation for an internal node in the case of a three-dimensional, steady-state heat conduction equation with variable thermal conductivity.

A composite wall is made of stainless steel $\left(k_{1}=13 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \quad 30 \mathrm{~mm}\right.$ thick), concrete $\left(k_{2}=1.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, 30 \mathrm{~mm}\right.\( thick \))\(, and nonmetal \)\left(k_{3}=0.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.\(, \)15 \mathrm{~mm}$ thick) plates. The concrete plate is sandwiched between the stainless steel plate at the bottom and the nonmetal plate at the top. A series of ASTM B21 naval brass bolts are bolted to the nonmetal plate, and the upper surface of the plate is exposed to convection heat transfer with air at \(20^{\circ} \mathrm{C}\) and $h=20 \mathrm{~W} / \mathrm{m}^{2}$.K. At the bottom surface, the stainless steel plate is subjected to a uniform heat flux of $2000 \mathrm{~W} / \mathrm{m}^{2}$. The ASME Code for Process Piping (ASME B31.3-2014, Table A-2M) limits the maximum use temperature for the ASTM B21 bolts to \(149^{\circ} \mathrm{C}\). Using the finite difference method with a uniform nodal spacing of \(\Delta x_{1}=10 \mathrm{~mm}\) for the stainless steel and concrete plates, and \(\Delta x_{2}=5 \mathrm{~mm}\) for the nonmetal plate, determine the temperature at each node. Plot the temperature distribution as a function of \(x\) along the plate thicknesses. Would the ASTM B21 bolts in the nonmetal plate comply with the ASME code?

A hot surface at \(120^{\circ} \mathrm{C}\) is to be cooled by attaching 8-cm- long, \(0.8-\mathrm{cm}\) - diameter aluminum pin fins ( $k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\( and \)\left.\alpha=97.1 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\right)$ to it with a center-to-center distance of \(1.6 \mathrm{~cm}\). The temperature of the surrounding medium is $15^{\circ} \mathrm{C}\(, and the heat transfer coefficient on the surfaces is \)35 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Initially, the fins are at a uniform temperature of \(30^{\circ} \mathrm{C}\), and at time \(t=0\), the temperature of the hot surface is raised to \(120^{\circ} \mathrm{C}\). Assuming one-dimensional heat conduction along the fin and taking the nodal spacing to be \(\Delta x=2 \mathrm{~cm}\) and a time step to be \(\Delta t=0.5 \mathrm{~s}\), determine the nodal temperatures after \(10 \mathrm{~min}\) by using the explicit finite difference method. Also, determine how long it will take for steady conditions to be reached.

Consider a house whose windows are made of \(0.375\)-in-thick glass $\left(k=0.48 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}\right.\( and \)\alpha=4.2 \times\( \)10^{-6} \mathrm{ft}^{2} / \mathrm{s}$ ). Initially, the entire house, including the walls and the windows, is at the outdoor temperature of \(T_{o}=35^{\circ} \mathrm{F}\). It is observed that the windows are fogged because the indoor temperature is below the dew-point temperature of \(54^{\circ} \mathrm{F}\). Now the heater is turned on, and the air temperature in the house is raised to $T_{i}=72^{\circ} \mathrm{F}\( at a rate of \)2^{\circ} \mathrm{F}$ rise per minute. The heat transfer coefficients at the inner and outer surfaces of the wall can be taken to be \(h_{i}=1.2\) and $h_{o}=2.6 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}$, respectively, and the outdoor temperature can be assumed to remain constant.

Consider an aluminum alloy fin $(k=180 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( of triangular cross section whose length is \)L=5 \mathrm{~cm}$, base thickness is \(b=1 \mathrm{~cm}\), and width \(w\) in the direction normal to the plane of paper is very large. The base of the fin is maintained at a temperature of \(T_{0}=180^{\circ} \mathrm{C}\). The fin is losing heat by convection to the ambient air at \(T_{\infty}=25^{\circ} \mathrm{C}\) with a heat transfer coefficient of $h=25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$ and by radiation to the surrounding surfaces at an average temperature of \(T_{\text {sarr }}=290 \mathrm{~K}\). Using the finite difference method with six equally spaced nodes along the fin in the \(x\)-direction, determine \((a)\) the temperatures at the nodes and (b) the rate of heat transfer from the fin for \(w=1 \mathrm{~m}\). Take the emissivity of the fin surface to be \(0.9\) and assume steady onedimensional heat transfer in the fin. Answers: (a) \(177.0^{\circ} \mathrm{C}\), $174.1^{\circ} \mathrm{C}, 171.2^{\circ} \mathrm{C}, 168.4^{\circ} \mathrm{C}, 165.5^{\circ} \mathrm{C} ;\( (b) \)537 \mathrm{~W}$

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