Chapter 5: Problem 2
Construct a table similar to Table \(5.3\) for a diatomic gas for which \(\gamma=1.4\).
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Key Concepts
These are the key concepts you need to understand to accurately answer the question.
Chapter 5: Problem 2
Construct a table similar to Table \(5.3\) for a diatomic gas for which \(\gamma=1.4\).
These are the key concepts you need to understand to accurately answer the question.
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Get started for freeEach possible normal mode of oscillation of a distributed system constitutes a mechanical degree of freedom of the system. According to the classical equipartition-of-energy theorem, each oscillatory degree of freedom is to be assigned an average thermal energy of \(k T\), where \(k\) is Boltzmann's constant and \(T\) is the absolute temperature. Hence the internal thermal energy per unit volume of a monatomic gas should be \(E_{v}=n k T\), with \(n\) given by (5.7.11). For a mole of monatomic gas, kinetic theory tells us that the internal energy is \(E_{\mu}=\frac{3}{2} R T\), where \(R\) is the gas constant per mole. We can bring the two viewpoints into agreement by choosing a suitable value of \(\omega_{\max }\). Compute this value and show that the minimum wavelength is of the order of the mean spacing of the atoms in the gas.
Compute the velocity of sound in hydrogen, the lightest gas, and in UF \(_{6}\), a heavy gas, both at standard conditions. Assume \(\gamma=1.3\) for the latter gas.
Supply convincing symmetry arguments establishing that the reflected and refracted plane waves at a plane interface have vector wave numbers lying in the plane of incidence. Why must all three waves have the same frequency?
Show that Brewster's angle, the angle of incidence at which no reflection
occurs, is given by
$$
\cot ^{2}\left(\theta_{1}\right)_{\text {Brewster
}}=\frac{Z_{1}^{2}}{Z_{2}^{2}-Z_{1}^{2}} \frac{c_{1}^{2}-c_{2}^{2}}{c_{1}^{2}}
$$
Under what conditions is Brewster's angle real? Answer: \(1
If we view the shock front from a reference frame moving with the velocity of the front, gas approaches from the right with the velocity \(v_{0}=-c\), suffers a compression as it moves through the front, and leaves toward the left with the velocity \(v_{1}=-\left(c-u_{p}\right)\) Show that \(v_{0} v_{1}=\left(P_{1}-P_{0}\right) /\left(\rho_{1}-\rho_{0}\right)\), which is known as Prandtl's relation.
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