Chapter 4: Problem 14
Prove that Eq. (4.4) is exact for all values of \(x\) if \(f(x)=\) \(a x^{2}+b x+c\).
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Chapter 4: Problem 14
Prove that Eq. (4.4) is exact for all values of \(x\) if \(f(x)=\) \(a x^{2}+b x+c\).
These are the key concepts you need to understand to accurately answer the question.
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Evaluate and interpret the condition numbers for (a) \(f(x)=\sqrt{|x-1|}+1 \quad\) for \(x=1.00001\) (b) \(f(x)=e^{-x}\) for \(x=10\) (c) \(f(x)=\sqrt{x^{2}+1}-x \quad\) for \(x=300\) (d) \(f(x)=\frac{e^{-x}-1}{x} \quad\) for \(x=0.001\) (e) \(f(x)=\frac{\sin x}{1+\cos x}\) for \(x=1.0001 \pi\)
Starting with the simplest version, \(\cos x=1,\) add terms one at a time to estimate \(\cos (\pi / 3) .\) After each new term is added, compute the true and approximate percent relative errors. Use your pocket calculator to determine the true value. Add terms until the absolute value of the approximate error estimate falls below an error criterion conforming to two significant figures.
The Stefan-Boltzmann law can be employed to estimate the rate of radiation of energy \(H\) from a surface, as in $$H=A e \sigma T^{4}$$,where \(H\) is in watts, \(A=\) the surface area \(\left(m^{2}\right), e=\) the emissivity that characterizes the emitting properties of the surface (dimensionless), \(\sigma=\) a universal constant called the Stefan-Boltzmann constant \(\left(=5.67 \times 10^{-8} \mathrm{W} \mathrm{m}^{-2} \mathrm{K}^{-4}\right),\) and \(T=\) absolute temperature (K). Determine the error of \(H\) for a steel plate with \(A=\) \(0.15 \mathrm{m}^{2}, e=0.90,\) and \(T=650 \pm 20 .\) Compare your results with the exact error. Repeat the computation but with \(T=650 \pm 40\) Interpret your results.
A missile leaves the ground with an initial velocity \(v_{0}\) forming an angle \(\phi_{0}\) with the vertical as shown in Fig. P4.17. The maximum desired altitude is \(\alpha R\) where \(R\) is the radius of the earth. The laws of mechanics can be used to show that $$\sin \phi_{0}=(1+\alpha) \sqrt{1-\frac{\alpha}{1+\alpha}\left(\frac{v_{e}}{v_{0}}\right)^{2}}$$ where \(v_{e}=\) the escape velocity of the missile. It is desired to fire the missile and reach the design maximum altitude within an accuracy of \(\pm 2 \%\). Determine the range of values for \(\phi_{0}\) if \(v_{e} / v_{0}=2\) and \(\alpha=0.25\).
Consider the function \(f(x)=x^{3}-2 x+4\) on the interval [-2,2] with \(h=0.25 .\) Use the forward, backward, and centered finite difference approximations for the first and second derivatives so as to graphically illustrate which approximation is most accurate. Graph all three first derivative finite difference approximations along with the theoretical, and do the same for the seco derivative as well.
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