波与量子代写Waves and Quanta|PA1140 University of Leicester Assignment

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Waves and quanta are two fundamental concepts in physics that are closely related but also distinct.

A wave is a disturbance that travels through space and time, carrying energy without the transfer of matter. Waves can take many forms, including electromagnetic waves (such as light and radio waves), sound waves, and water waves. Waves are characterized by their wavelength, frequency, and amplitude, which determine their properties such as speed and energy.

On the other hand, a quantum is a discrete packet of energy that behaves both as a particle and as a wave. In the quantum world, particles can exhibit wave-like behavior, and waves can behave like particles. This duality is known as wave-particle duality. The behavior of quanta is described by quantum mechanics, a branch of physics that deals with the behavior of matter and energy at the atomic and subatomic level.

The relationship between waves and quanta is that waves can be thought of as a collection of quanta. For example, electromagnetic waves consist of a stream of photons, which are quanta of electromagnetic radiation. Similarly, matter waves, which describe the behavior of particles such as electrons, can be thought of as a collection of quanta.

Overall, waves and quanta are both fundamental concepts in physics that are used to explain and understand the behavior of matter and energy in our universe.

波与量子代写Waves and Quanta|PA1140 University of Leicester Assignment

问题 1.

A long, uniform taut string (mass per unit length $\rho$, tension $T$ ) along $-\infty<x<\infty$ is supported on an elastic foundation of stiffness $\alpha$, and a point mass $M$ is attached at $x=0$.
Suppose that a time-harmonic vertical force
$$
F \cos \Omega t
$$
is applied to the mass at $x=0$.
Determine the steady-state displacement response of the string for $-\infty<x<\infty$.

证明 .

The equation of motion for the string is given by the wave equation:

$\rho \frac{\partial^2 u}{\partial t^2}=T \frac{\partial^2 u}{\partial x^2}-\alpha u$

where $u(x,t)$ is the displacement of the string from its equilibrium position at point $x$ and time $t$. The first term on the right-hand side represents the tension in the string, and the second term represents the elastic foundation. We can assume a solution of the form:

$u(x, t)=U(x) e^{i \omega t}$

where $\omega = \Omega + i\beta$ is the complex frequency and $U(x)$ is the complex amplitude of the displacement.

Substituting this solution into the wave equation and simplifying, we get:

$\frac{d^2 U}{d x^2}+k^2 U=0$

where $k^2 = \frac{\omega^2 \rho}{T} – i\frac{\alpha}{T}$. This is a second-order homogeneous differential equation with constant coefficients, which has solutions of the form:

$U(x)=A e^{i k x}+B e^{-i k x}$

where $A$ and $B$ are complex constants to be determined by the boundary conditions.

At $x=0$, the displacement of the string must be equal to the displacement of the mass, which is given by:

$u(0, t)=U(0) e^{i \omega t}=\frac{F}{M} e^{i \omega t}$

Therefore, $U(0) = \frac{F}{M}$.

At $x=\pm \infty$, the string must be taut and have no displacement. Therefore, we can assume that $U(\pm \infty) = 0$.

Using these boundary conditions, we can solve for $A$ and $B$:

$A=-\frac{F}{2 M} e^{-i k x} \quad$ and $\quad B=\frac{F}{2 M} e^{i k x}$

Therefore, the displacement of the string is given by:

$u(x, t)=\frac{F}{2 M}\left(e^{i(k x-\omega t)}-e^{i(-k x-\omega t)}\right)$

Simplifying, we get:

$u(x, t)=\frac{F}{M} \sin (k x) \sin (\omega t)$

where $k = \sqrt{\frac{\omega^2 \rho}{T} – i\frac{\alpha}{T}}$. This is the steady-state displacement response of the string for $-\infty < x < \infty$.

问题 2.

The propagation of free uni-directional surface waves of small amplitude on moderately shallow water is governed by the equation
$$
\frac{\partial \eta}{\partial t}+c_0 \frac{\partial \eta}{\partial x}+\beta \frac{\partial^3 \eta}{\partial x^3}=0
$$
where $\eta(x, t)$ is the free-surface elevation and $c_0$ and $\beta$ are constants.
(a) Suppose that an external localized pressure disturbance traveling with constant speed $V$ acts on the free surface. Determine the wavenumber(s) of the excited steadystate radiating wave(s), depending on the forcing speed $V$. Sketch the position of these waves relative to the forcing. (Take $c_0>0$ and consider $\beta>0$ and $\beta<0$ as well as $V>0$ and $V<0$.)

证明 .

To determine the wavenumber(s) of the excited steady-state radiating wave(s), we start by assuming a solution of the form:

$\eta(x, t)=A e^{i(k x-\omega t)}$

where $A$ is the amplitude of the wave, $k$ is the wavenumber, and $\omega$ is the frequency. Substituting this solution into the given equation yields:

$-i \omega A+i c_0 k A-i \beta k^3 A=0$

Dividing through by $-iA$ and solving for $k$, we get:

$k^2=\frac{\omega}{c_0} \pm \sqrt{\left(\frac{\omega}{c_0}\right)^2-\frac{\beta}{c_0}}$

Now suppose that an external localized pressure disturbance traveling with constant speed $V$ acts on the free surface. This means that the phase velocity of the wave excited by the disturbance will be $V$, i.e. $\omega/k=V$. Substituting this into the above expression for $k^2$ yields:

$k^2=\frac{V^2}{c_0^2} \pm \sqrt{\left(\frac{V^2}{c_0^2}\right)^2-\frac{\beta}{c_0^3}}$

Depending on the sign of $\beta$, we have two cases to consider:

Case 1: $\beta>0$

In this case, there are two possible values of $k$ given by:

$k_1=\frac{V}{c_0}+\sqrt{\left(\frac{V}{c_0}\right)^2-\frac{\beta}{c_0^3}}, \quad k_2=\frac{V}{c_0}-\sqrt{\left(\frac{V}{c_0}\right)^2-\frac{\beta}{c_0^3}}$

The two corresponding frequencies are:

$\omega_1=c k_1=c_0\left(\frac{V}{c_0}+\sqrt{\left(\frac{V}{c_0}\right)^2-\frac{\beta}{c_0^3}}\right), \quad \omega_2=c_0 k_2=c_0\left(\frac{V}{c_0}-\sqrt{\left(\frac{V}{c_0}\right)^2-\frac{\beta}{c_0^3}}\right)$

where $c=\sqrt{c_0^2+\beta k^2}$ is the phase velocity of the wave.

Note that $k_1$ and $k_2$ have opposite signs, which means that the two waves have opposite directions of propagation. Furthermore, the two waves have different wavelengths and frequencies. The wave with wavenumber $k_1$ has a longer wavelength and a lower frequency than the wave with wavenumber $k_2$.

To sketch the position of these waves relative to the forcing, we note that the wave with wavenumber $k_1$ travels in the same direction as the external disturbance, while the wave with wavenumber $k_2$ travels in the opposite direction. The amplitude of the waves decreases with distance from the source, so the wave with wavenumber $k_1$ will be closer to the source than the wave with wavenumber $k_2$.

Case 2: $\beta<0$

In this case, there is only one possible value of $k$ given

问题 3.

(b) Suppose at $t=0$ a localized initial wave disturbance is introduced in the vicinity of $x=0$. Sketch qualitatively the time history of the response for $t>0$ at a fixed station $x=L>0$, far from the region of the initial disturbance. Sketch qualitatively a snapshot of the disturbance for $-\infty<x<\infty$ at time $t=T$, long after the initial excitation. Justify your answers. (Again, $c_0>0$ and consider $\beta>0$ and $\beta<0$.)

证明 .

To sketch qualitatively the time history of the response for $t>0$ at a fixed station $x=L>0$, we first need to find the solution to the given equation. We can use the method of characteristics to solve this equation.

Let $dx/dt=c_0$ and $d^2x/dt^2=0$, which gives $x=c_0t+x_0$ and $x_0=L$ for $t=0$. Then, we have

$\frac{d \eta}{d t}=-\beta \frac{\partial^3 \eta}{\partial x^3}$

We assume a solution of the form $\eta(x,t)=f(x-ct)$, where $c$ is the wave speed. Substituting this into the above equation and integrating three times with respect to $x$, we get

$\eta(x, t)=A e^{-k(x-c t)} \cos (k(x-c t)+\phi)$

where $k=\sqrt[3]{\beta/c_0}$, $A$ and $\phi$ are constants determined by the initial conditions.

Now, we can sketch the time history of the response for $t>0$ at a fixed station $x=L>0$. At $x=L$, the free surface elevation is given by

$\eta(L, t)=A e^{-k(L-c t)} \cos (k(L-c t)+\phi)$

As $t$ increases, the amplitude of the cosine function decays exponentially with a decay rate of $k(c t-L)$. Therefore, the free surface elevation decreases in amplitude and oscillates with a decreasing frequency as time progresses. The decay rate is faster for larger values of $k$ (i.e., for larger values of $\beta$ or smaller values of $c_0$). If $\beta<0$, then $k$ is imaginary, which means the wave amplitude decays exponentially without oscillation.

To sketch qualitatively a snapshot of the disturbance for $-\infty<x<\infty$ at time $t=T$, long after the initial excitation, we can use the same solution as above, but with $t=T$. Thus, we have

$\eta(x, T)=A e^{-k(x-c T)} \cos (k(x-c T)+\phi)$、

The cosine function represents a wave with wavelength $\lambda=2\pi/k$ and wave number $k$. The wave is propagating to the right if $c>c_0$, or to the left if $c<c_0$. The amplitude of the wave decreases exponentially as $x$ increases or decreases from the initial position of the disturbance. The decay rate is faster for larger values of $k$ (i.e., for larger values of $\beta$ or smaller values of $c_0$). If $\beta<0$, then $k$ is imaginary, which means the wave amplitude decays exponentially without oscillation. The phase velocity of the wave is given by $c/k$, which decreases as $k$ increases. If $\beta>0$, then the group velocity of the wave is given by $c-(2/3)k^2c_0$, which is smaller than the phase velocity. If $\beta<0$, then the group velocity is undefined because $k$ is imaginary.

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