Chapter 5: Problem 2
Show that \(\nabla \times \mathbf{V}=0\) when \(\mathbf{V}\) is the gradient of a scalar function of position, \(\mathbf{V}=\nabla \phi\).
Chapter 5: Problem 2
Show that \(\nabla \times \mathbf{V}=0\) when \(\mathbf{V}\) is the gradient of a scalar function of position, \(\mathbf{V}=\nabla \phi\).
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Get started for freeShow that the sound wave specified by $$ p(\mathbf{r}, t)=p_{m} \exp i(\mathbf{x} \cdot \mathbf{r}-\omega t) $$ satisfies the wave equation (5.3.1) and constitutes a plane wave traveling in the direction of the vector wave number \(\kappa\). Find an expression for the particle displacement \(\boldsymbol{\rho}\) and velocity \(\dot{e}\) in the wave. Verify that the wave is irrotational by computing \(\nabla \times\) e. Justify the use of the term "longitudinal" in referring to a plane sound wave, such as (5.3.20).
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.
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?
Construct a table similar to Table \(5.3\) for a diatomic gas for which \(\gamma=1.4\).
A satellite passes across the sky sending out radio signals at a constant but inaccurately known frequency \(\omega_{s}\). Assume that the satellite altitude is small compared to the earth's radius and hence that the trajectory can be considered to be a straight line at constant altitude above a flat earth. By beating the signals against a known standard frequency and measuring the difference frequency, an observer on the earth can accurately measure the received frequency, with its Doppler shift, as a function of time, with \(\cos \theta_{s}\) in \((5.8 .3)\) [or \((5.8 .5)\), with \(\gamma=1\), since \(v \ll c]\) ranging from 1 to \(-1\). Show how the observations can be made to yield a value of \(v\), the velocity of the satellite, and a value of \(D\), the closest distance of approach of the satellite. \(\dagger\)
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