Chapter 5: Problem 2
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.
Chapter 5: Problem 2
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.
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Get started for freeShow 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
Show that \(\nabla \times \mathbf{V}=0\) when \(\mathbf{V}\) is the gradient of a scalar function of position, \(\mathbf{V}=\nabla \phi\).
Investigate the radially symmetric standing waves in a rigid spherical container of radius \(R\) filled with a gas in which the velocity of sound is \(c\). In particular find an expression giving the frequency of the fundamental and its overtones.
What boundary condition must the velocity potential satisfy \((a)\) at a rigid boundary; \((b)\) at a free surface of a fluid; \((c)\) at a plane interface between two different fluids?
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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