机械学代写Mechanics|PA1110 University of Leicester Assignment

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Assignment-daixieTM为您提供莱斯特大学University of Leicester PA1110 Mechanics机械学代写代考辅导服务!

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Classical mechanics is a fundamental part of physics that deals with the motion of macroscopic objects in the presence of forces. It is based on the laws of motion proposed by Sir Isaac Newton in the 17th century, which form the foundation of classical mechanics.

In classical mechanics, we use various quantities to describe the behavior of objects, including position, velocity, acceleration, force, work, energy, momentum, and angular momentum. These quantities are related through mathematical equations and principles that describe how objects move and interact with each other.

For example, the work-energy principle states that the work done on an object is equal to the change in its kinetic energy, while the law of conservation of momentum states that the total momentum of a closed system remains constant unless acted upon by an external force.

Classical mechanics is still widely used today in many fields of science and engineering, from astronomy to robotics, and it provides a solid foundation for understanding the behavior of objects at the macroscopic level.

机械学代写Mechanics|PA1110 University of Leicester Assignment

问题 1.

A runner travels along the $\mathrm{x}$-axis, and at time $t=0$ is at the origin. The $x$-component of the runner’s position with respect to the origin is given by: $$ x(t)=b t^2 $$ where $b$ is a positive constant. (Part a) What are the units of the constant $b$ ? Express your answer in terms of $\mathrm{m}$ for meter and $\mathrm{s}$ for seconds. (Part b) Find $v(t)$, the $x$-component of the runner’s velocity as a function of time.

证明 .

a) The units of the constant $b$ can be obtained by looking at the units of $x(t)$. We have $x(t)=[b][t^2]$, where $[b]$ denotes the units of $b$ and $[t]$ denotes the units of $t$. Since $x(t)$ has units of length (meters), we have $[b]=\mathrm{m}/\mathrm{s}^2$.

b) The velocity of the runner is given by the derivative of the position function with respect to time:

$v(t)=\frac{d x}{d t}=\frac{d}{d t}\left(b t^2\right)=2 b t$.

Therefore, the $x$-component of the runner’s velocity as a function of time is $v(t) = 2bt$.

问题 2.

(Part c) Find $a(t)$, the $x$-component of the runner’s acceleration as a function of time.

证明 .

c) The acceleration of the runner is given by the second derivative of the position function with respect to time:

$a(t)=\frac{d^2 x}{d t^2}=\frac{d}{d t}(2 b t)=2 b$

Therefore, the $x$-component of the runner’s acceleration as a function of time is constant and given by $a(t) = 2b$.

问题 3.

At time $t=0$, a car moving along the $+x$-axis passes through $x=0$ with a constant velocity of magnitude $v_0$. At some time later, $t_1$, it starts to slow down. The acceleration of the car as a function of time is given by:
$$
a(t)= \begin{cases}0 & 0 \leq t \leq t_1 \ -c\left(t-t_1\right) & t_1<t \leq t_2\end{cases}
$$
where $c$ is a positive constants in $\mathrm{Sl}$ units, and $t_1<t \leq t_2$ is the given time interval for which the car is slowing down. The goal of the problem is to find the car’s position as a function of time between $t_1<t<t_2$. Express your answer in terms of $\mathrm{v}{-} 0$ for $v_0$, t 1 for $t_1, \mathrm{t} 2$ for $t_2$, and $c$ as needed.
(Part a). What is $v(t)$, the velocity of the car as a function of time during the time interval $0 \leq t \leq t_1$ ?

证明 .

Since the acceleration of the car is zero during the time interval $0 \leq t \leq t_1$, the car’s velocity remains constant during this time interval. Therefore, the velocity of the car as a function of time during the time interval $0 \leq t \leq t_1$ is given by:

$$v(t) = v_0 \qquad \text{for } 0 \leq t \leq t_1$$

where $v_0$ is the constant velocity of the car at $t=0$.

这是一份2023年的莱斯特大学University of Leicester PA1110数学物理代写的成功案例




















数学物理代写Mathematics for Physicists I|PH-132 Swansea University Assignment

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Assignment-daixieTM为您提供斯旺西大学Swansea University PH-132 Mathematics for Physicists I数学物理代写代考辅导服务!

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数学物理代写Mathematics for Physicists I|PH-132 Swansea University Assignment

问题 1.

Let $\left{f_j\right}$ be a sequence of functions in $L^2(\mathbb{R})$. We say $f_j \rightarrow f$ strongly in $L^2$ if there exists $f \in L^2(\mathbb{R})$ such that
$$
\left|f_j-f\right|_{L^2(\mathbb{R})} \rightarrow 0
$$
Give an example of a sequence $\left{f_j\right}$ and a function $f$ such that $f_j \rightarrow f$ strongly in $L^2$ but $f_j$ does not converge to $f$ pointwise. Prove both of these facts about your example.

证明 .

Consider the sequence of functions $\left{f_j\right}$ defined as follows:

$f_j(x)= \begin{cases}j, & \text { if } x \in\left[0, \frac{1}{j}\right] \ 0, & \text { otherwise }\end{cases}$

for $j\geq 1$.

Note that each $f_j$ is in $L^2(\mathbb{R})$ since

$\int_{-\infty}^{\infty}\left|f_j(x)\right|^2 d x=\int_0^{1 / j} j^2 d x=\frac{1}{j} \rightarrow 0 \quad$ as $j \rightarrow \infty$

Also, $f_j$ converges to $0$ pointwise everywhere on $\mathbb{R}$ since $\frac{1}{j}<x$ implies $f_j(x)=0$ for all $j\geq 1$.

To show that $f_j$ converges strongly to $0$ in $L^2(\mathbb{R})$, we calculate \begin{align*} \left|f_j-0\right|{L^2(\mathbb{R})}^2 &= \int{-\infty}^{\infty}|f_j(x)|^2dx\ &=\int_{0}^{1/j}j^2dx\ &=\frac{1}{j} \rightarrow 0 \quad \text{as }j\rightarrow \infty. \end{align*} Therefore, $f_j$ converges strongly to $0$ in $L^2(\mathbb{R})$.

However, $f_j$ does not converge pointwise to $0$ since, for example, $f_1(x)=1$ for $x\in[0,1]$ and $f_j(x)=0$ for $x\in[0,1/j]$ when $j\geq 2$.

Therefore, we have shown that $f_j$ converges strongly to $0$ in $L^2(\mathbb{R})$ but $f_j$ does not converge pointwise to $0$.

问题 2.

Let $X, Y$ be $n \times n$ matrices such that $X^3=Y^3$ and $X^2 Y=Y^2 X$. What are necessary and sufficient conditions on $X$ and $Y$ such that $X^2+Y^2$ is invertible?

证明 .

$X^3=Y^3$ and $X^2 Y=Y^2 X$ taken together allow us to write
$$
\left(X^2+Y^2\right) X=X^3+Y^2 X=Y^3+X^2 Y=\left(X^2+Y^2\right) Y \text {. }
$$
Notice that if $X \neq Y$ then $X^2+Y^2$ cannot be invertible. Thus, a necessary condition is that $X=Y$.

问题 3.

Let $T: \mathbb{R}^3 \rightarrow \mathbb{R}^2$ and $S: \mathbb{R}^3 \rightarrow \mathbb{R}^3$ correspond to the transformations
$$
T(x, y, z)=(x, y) ; S(x, y, z)=(-x,-y,-z) .
$$
Notice that $T S$ is a well defined linear transformation. Find a matrix representation for $S$, $T$, and $T S$ using the basis ${(1,0,0),(1,1,0),(1,1,1)}$ for $\mathbb{R}^3$ and the basis ${(1,0),(1,-1)}$ for $\mathbb{R}^2$.

证明 .

First note that $T(1,0,0)=(1,0)=1 \cdot(1,0)+0 \cdot(1,-1) ; \quad T(1,1,0)=$ $(1,1)=2 \cdot(1,0)-1 \cdot(1,-1) ; \quad T(1,1,1)=(1,1)=2 \cdot(1,0)-1 \cdot(1,-1)$ and thus the matrix for $T$ in these bases is
$$
\left(\begin{array}{ccc}
1 & 2 & 2 \
0 & -1 & -1
\end{array}\right)
$$
To find the matrix for $S$ we perform the same process:
$$
\begin{aligned}
& S(1,0,0)=(-1,0,0)=-1 \cdot(1,0,0)+0 \cdot(1,1,0)+0 \cdot(1,1,1) \
& S(1,1,0)=(-1,-1,0)=0 \cdot(1,0,0)-1 \cdot(1,1,0)+0 \cdot(1,1,1) \
& S(1,1,1)=(-1,-1,-1)=0 \cdot(1,0,0)+0 \cdot(1,1,0)-1 \cdot(1,1,1)
\end{aligned}
$$
Thus the matrix for this transformation is
$$
\left(\begin{array}{ccc}
-1 & 0 & 0 \
0 & -1 & 0 \
0 & 0 & -1
\end{array}\right)
$$

Thus we find the matrix for $T S$ by multiplication:
$$
\left(\begin{array}{ccc}
1 & 2 & 2 \
0 & -1 & -1
\end{array}\right)\left(\begin{array}{ccc}
-1 & 0 & 0 \
0 & -1 & 0 \
0 & 0 & -1
\end{array}\right)=\left(\begin{array}{ccc}
-1 & -2 & -2 \
0 & 1 & 1
\end{array}\right)
$$

这是一份2023年的斯旺西大学Swansea University PH-132数学物理代写的成功案例




















天文学和宇宙学代写Astronomy and Cosmology|PH-104 Swansea University Assignment

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Assignment-daixieTM为您提供斯旺西大学Swansea University PH-100  Astronomy and Cosmology天文学和宇宙学代写代考辅导服务!

Instructions:

Observational astronomy and cosmology are fascinating fields that allow us to explore and understand the vast universe around us. I’m sure students will find it inspiring to learn about the different techniques used to study celestial objects, such as telescopes and spectroscopy. Practical observations can also be a fun way to apply theoretical concepts and gain a deeper understanding of astronomical phenomena. I hope students enjoy the module and are motivated to pursue further studies in these areas.

天文学和宇宙学代写Astronomy and Cosmology|PH-104 Swansea University Assignment

问题 1.

A spectrum is taken of a single star (i.e., one not in a binary), Among the observed spectral lines is one from oxygen whose rest wavelength is $5007 \mathrm{~A}$. The Doppler shifted oxygen line from this star is observed to be at a wavelength of $5012 \mathrm{~A}$. The star is also observed to have a proper motion, $\mu$, of 1 arc second per year (which corresponds to $\sim 1.5 \times$ $10^{-13}$ radians per second of time). It is located at a distance of $60 \mathrm{pc}$ from the Earth.
What is the 3 dimensional velocity of the star?

证明 .

$\begin{aligned} & V_r=\frac{\Delta \lambda}{\lambda} c=\frac{5}{5000} c=300 \mathrm{~km} / \mathrm{s} \ & V_T=1.5 \times 10^{-13} \times D=\dot{\theta} D=\mu D=277 \mathrm{~km} / \mathrm{s}\end{aligned}$

问题 2.

What parallax would be measured for this star?

证明 .

parallax $=\frac{1^{\prime \prime}}{60}$

问题 3.

A candle has a power in the visual band of -3 Watts. When this candle is placed at a distance of $3 \mathrm{~km}$ it has the same apparent brightness as a certain star. Assume that this star has the same luminosity as the Sun in the visual band $\left(\sim 10^{26}\right.$ Watts). How far away is the star?

证明 .

\begin{aligned}
& \text { Sane } f \text { lux } \Rightarrow \frac{3}{(3 \mathrm{~km})^2}=\frac{10^{26}}{d^2} \
& d=10^{13} \times \frac{3}{\sqrt{3}}=1.7 \times 10^{13} \mathrm{~km} \
& d=0.56 \mathrm{pc} \
&
\end{aligned}

这是一份2023年的斯旺西大学Swansea University PH-104天文学和宇宙学代写的成功案例




















动力学 震荡和波浪代写Dynamics, Oscillations and Waves|PH-100 Swansea University Assignment

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Assignment-daixieTM为您提供斯旺西大学Swansea University PH-100  Dynamics, Oscillations and Waves动力学 震荡和波浪代写代考辅导服务!

Instructions:

Dynamics is the branch of physics that deals with the study of motion and its causes, including force, energy, momentum, and angular momentum. In classical mechanics, which is the study of motion of macroscopic objects at low speeds, dynamics plays a central role in describing how objects move and how forces affect their motion.

Oscillations are a type of motion that involves the repetitive back-and-forth motion of an object around a central position, such as a pendulum swinging back and forth or a spring vibrating up and down. Oscillations are characterized by their amplitude, frequency, and period.

Waves are a type of disturbance that propagates through a medium or space, carrying energy and momentum without necessarily transporting matter. Waves can take many different forms, such as sound waves, light waves, and water waves. Waves are characterized by their wavelength, frequency, amplitude, and velocity.

动力学 震荡和波浪代写Dynamics, Oscillations and Waves|PH-100 Swansea University Assignment

问题 1.

A man rows a hoat across a river of width u occupying the region $0<x<u$ in the $x, y$. plane, always rowing towards a fixed point un uut bank say ‘ 0,0$)$. He rows at constant speed $u$ relative to the water. and the river flows at constant speed $v$. Show that $$ \dot{r}-\frac{-u x}{\left(x^2+y^2\right)^{1 / 2}} \quad \quad \dot{i}-v-\frac{u \eta}{\left(x^2+y^2\right)^{1 / 2}} $$ where $(x, y)$ are the conrdinates of the hoat. Show that the phase trajectories are given by $$ y+\left(x^2+y^2\right)^{1 / 2}-C x^{1-\alpha}, $$ where $\alpha-v / u$. Sketch the phase diagram for $\alpha<1$ and interpret it. What kind of point is the origin? What happens to the boat if $\alpha>1$ ?

证明 .

To derive the equations of motion for the boat, we note that the velocity of the boat relative to the river is given by $(u, v)$. Therefore, the velocity of the boat in the $x$-direction is $u\cos\theta$, where $\theta$ is the angle between the boat’s direction and the $x$-axis. Similarly, the velocity of the boat in the $y$-direction is $u\sin\theta$. The angle $\theta$ is determined by the condition that the boat is always rowing towards the fixed point $(0,0)$ on the opposite bank. Therefore,

$\tan \theta=\frac{y}{x-u}$

Taking the time derivative of $x$ and $y$ gives

$\dot{x}=u \cos \theta-\frac{u x}{\sqrt{x^2+y^2}}, \quad \dot{y}=u \sin \theta-v-\frac{u y}{\sqrt{x^2+y^2}}$.

Using the identity $\cos^2\theta+\sin^2\theta=1$, we can write $\cos\theta=\sqrt{1-\sin^2\theta}$ and substitute for $\cos\theta$ in the expression for $\dot{x}$, giving

$\dot{x}=u \sqrt{1-\frac{y^2}{(x-u)^2}}-\frac{u x}{\sqrt{x^2+y^2}}$.

We can simplify this expression by multiplying both the numerator and denominator of the first term by $(x-u)^2$, giving

$\dot{x}=u \frac{x-u}{\sqrt{x^2+y^2}}-\frac{u x}{\sqrt{x^2+y^2}}=\frac{u}{\sqrt{x^2+y^2}}\left(-u x+\sqrt{x^2+y^2}\right)$.

Similarly, we can substitute for $\sin\theta$ in the expression for $\dot{y}$, giving

$\dot{y}=u \frac{y}{\sqrt{(x-u)^2+y^2}}-v-\frac{u y}{\sqrt{x^2+y^2}}=\frac{u}{\sqrt{x^2+y^2}}\left(-v+(x-u) \frac{y}{\sqrt{(x-u)^2+y^2}}\right)$.

Defining $r=\sqrt{x^2+y^2}$ and $\eta=y/x$, we obtain the desired equations of motion,

$\dot{r}-\frac{-u x}{\left(x^2+y^2\right)^{1 / 2}}=\frac{u}{r}(r-u), \quad \dot{\eta}-v-\frac{u \eta}{\left(x^2+y^2\right)^{1 / 2}}=\frac{u}{r} \eta\left(\frac{r-u}{x}\right)$.

To obtain the phase trajectories, we can eliminate time between these two equations by differentiating the second equation with respect to $x$ and substituting for $\dot{r}$ from the first equation. This gives

$\frac{d}{d x}\left(\frac{\dot{\eta}+v}{\eta}\right)=\frac{u}{r}\left(1-\frac{u}{r}\right)$.

Integrating this expression gives

$\ln |\eta+\dot{\eta}+v|=u \ln \left|\frac{r}{u}-1\right|+C_1$,

where $C_1$ is a constant

问题 2.

Consider the system governed by
$$
\ddot{x}+\mu \sin \dot{x}+x-0
$$
(a) Construct several trajectories and show that more than one limit cycle exists
(You may find it useful to use the computer for this purpose.’,

证明 .

As an AI language model, I can provide the steps to find the limit cycles but I can’t plot the trajectories directly. However, I can help you set up the equations and provide guidance on how to find the limit cycles using a numerical method.

To begin, we can rewrite the given system as a set of first-order differential equations:

$\begin{aligned} & \dot{x}=y \ & \dot{y}=-\mu \sin (y)-x\end{aligned}$

We can use the Poincaré-Bendixson theorem to determine the existence of limit cycles. The theorem states that if a solution is bounded and does not approach a fixed point or a periodic orbit, then it must approach a limit cycle.

To find the limit cycles, we can use numerical methods such as the Runge-Kutta method to solve the system of equations and plot the trajectories. We can start by choosing different initial conditions and simulating the system for a sufficiently long time to ensure that the trajectory has converged to a limit cycle or has become unbounded.

Here are the steps to find the limit cycles:

  1. Choose a set of initial conditions $(x_0, y_0)$
  2. Solve the system of differential equations numerically using a numerical method such as the Runge-Kutta method.
  3. Plot the trajectory $(x(t), y(t))$ for a sufficiently long time.
  4. Repeat steps 1-3 for different initial conditions.
  5. Look for closed trajectories that do not approach a fixed point or a periodic orbit.
  6. If there are multiple closed trajectories, then there are multiple limit cycles.

Using a numerical method to find limit cycles can be computationally intensive and requires some experience with numerical methods. However, it can be a powerful tool to understand the dynamics of a system when analytical solutions are not available.

问题 3.

‘b) Some limit cycles are stable while others are unstable. How can me determine the stability of the various limit cycles by examining the trajectories in the phase plane?

证明 .

To determine the stability of the limit cycles, we can examine the trajectories in the phase plane near the limit cycles. Specifically, we can look at the behavior of nearby trajectories relative to the limit cycle.

Let’s assume that we have found a closed trajectory (i.e., a limit cycle) in the phase plane. We can then consider a nearby trajectory that starts at a point slightly displaced from the limit cycle. As time passes, this trajectory will either approach the limit cycle or move away from it.

If nearby trajectories that start on one side of the limit cycle move towards the limit cycle as time goes on, then the limit cycle is stable. On the other hand, if nearby trajectories that start on one side of the limit cycle move away from the limit cycle as time goes on, then the limit cycle is unstable.

More formally, we can use the concept of linear stability to determine the stability of the limit cycle. Linear stability analysis involves linearizing the system of equations around the limit cycle and examining the eigenvalues of the resulting linearized system. If all eigenvalues have negative real parts, then the limit cycle is stable. If at least one eigenvalue has a positive real part, then the limit cycle is unstable.

However, in the absence of an analytical solution, we can examine the trajectories in the phase plane to get an idea of the stability of the limit cycles. By examining the direction of the nearby trajectories relative to the limit cycle, we can infer whether the limit cycle is stable or unstable.

If the nearby trajectories spiral towards the limit cycle, then the limit cycle is stable. If the nearby trajectories spiral away from the limit cycle, then the limit cycle is unstable. The direction of the spiral can be determined by the sign of the eigenvalues of the linearized system.

It is important to note that this method of determining stability is not always accurate and can be subjective. However, it can provide a qualitative understanding of the stability of the limit cycles.

这是一份2023年的斯旺西大学Swansea University PH-100动力学 震荡和波浪代写的成功案例




















物理统计学 Statistical Physics II|PHYS7722 Boston College Assignment

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Assignment-daixieTM为您提供波士顿学院Boston College PHYS7722 Statistical Physics II物理统计学代写代考辅导服务!





Instructions:

Statistical physics is a branch of physics that studies the behavior of large collections of particles, such as atoms or molecules, using statistical methods. It aims to explain macroscopic properties of matter, such as temperature, pressure, and entropy, in terms of the microscopic properties of the constituent particles and the interactions between them.

Statistical physics is based on the principles of probability and statistics, and it provides a framework for understanding complex systems that cannot be analyzed through classical physics. It also provides a link between the microscopic world of quantum mechanics and the macroscopic world of classical mechanics.

物理统计学 Statistical Physics II|PHYS7722 Boston College Assignment

问题 1.

The partition function for an ideal gas of $N$ distinguishable particles where particle $k$ has mass $m_k$ can be written as
$$
Z=\frac{1}{h^{3 N}} \int_V d^3 \mathbf{q}1 \int{\text {all } \mathbf{p}} d^3 \mathbf{p}1 \cdots \int_V d^3 \mathbf{q}_N \int{\text {all } \mathbf{p}} d^3 \mathbf{p}N \exp \left(-\frac{1}{k_B T} \sum{k=1}^N \frac{\mathbf{p}_k^2}{2 m_k}\right) .,
$$
where $V$ is the volume of the system.
(a) Evaluate all the integrals in Eq.(40) and write the final result in terms of $T, V, N$ and the set of masses $m_1, m_2, \ldots, m_N$ (and physical constants).

证明 .

We can evaluate the integrals by using the fact that they represent the phase space integral for each particle. The integral $\int{d^3\mathbf{q}_k} \int{\text{all } \mathbf{p}_k}d^3\mathbf{p}_k$ represents the phase space integral for the $k$th particle. We can perform this integral by changing to spherical coordinates for the momentum integral and making use of the fact that the volume element $d^3 \mathbf{p}$ is $4\pi p^2dp$, where $p$ is the magnitude of the momentum vector. Thus, we have

$\int d^3 \mathbf{q}_k \int$ all $\mathbf{p}_k d^3 \mathbf{p}_k=V \int_0^{\infty} 4 \pi p_k^2 d p_k=\frac{4}{3} \pi V\left(\frac{2 \pi m_k k_B T}{h^2}\right)^{3 / 2}$

Using this result, we can evaluate the integral over all particles in the partition function: \begin{align*} Z &= \frac{1}{h^{3N}} \prod_{k=1}^N \int{d^3\mathbf{q}_k} \int{\text{all } \mathbf{p}k}d^3\mathbf{p}k \exp \left(-\frac{1}{k_B T} \sum{k=1}^N \frac{\mathbf{p}k^2}{2m_k}\right)\ &= \frac{1}{h^{3N}} \prod{k=1}^N \frac{4}{3} \pi V \left(\frac{2\pi m_k k_B T}{h^2}\right)^{3/2} \exp \left(-\frac{1}{k_B T} \frac{\mathbf{p}k^2}{2m_k}\right)\ &= \frac{1}{N! h^{3N}} V^N \prod{k=1}^N \left(\frac{2\pi m_k k_B T}{h^2}\right)^{3/2} \exp \left(-\frac{1}{k_B T} \frac{\mathbf{p}k^2}{2m_k}\right)\ &= \frac{1}{N!} \left(\frac{V}{v_N}\right)^N \prod{k=1}^N \left(\frac{mk_B T}{2\pi\hbar^2}\right)^{3/2}, \end{align*} where $v_N$ is the volume occupied by a single particle, defined by $v_N = \frac{4}{3}\pi\left(\frac{\hbar}{\sqrt{2\pi mk_B T}}\right)^3$ and $m$ is the average mass of a particle, defined by $m = \frac{1}{N}\sum{k=1}^N m_k$. The result is written in terms of physical constants and the set of masses $m_1, m_2, \ldots, m_N$.

问题 2. What is the free energy of this system written in terms of $T, V, N$ and the set of masses $m_1, m_2, \ldots, m_N$ (and physical constants).

证明 .

(b) Given the partition function $Z$ of a system, the free energy is
$$
F=-k_B T \ln Z
$$
Therefore, the free energy of this ideal gas system is
$$
\begin{aligned}
F & =-k_B T \ln \left[\frac{V^N}{h^{3 N}}\left(2 \pi k_B T\right)^{3 N / 2} \prod_{k=1}^N \sqrt{m_k^3}\right] \
& =-k_B T \ln \left[V^N\left(\frac{2 \pi k_B T}{h^2}\right)^{3 N / 2} \prod_{k=1}^N m_k^{3 / 2}\right] \
& =-k_B T\left[N \ln V+\frac{3 N}{2} \ln \frac{2 \pi k_B T}{h^2}+\frac{3}{2} \sum_{k=1}^N \ln m_k\right] .
\end{aligned}
$$

问题 3.

(c) Given that pressure is the negative of the volume partial derivative of the free energy, derive the relationship between pressure $P$, number of particles $N$, volume $V$ and temperature $T$ for this system.

证明 .

(c) The pressure of an ideal gas system is given by
$$
P=-\frac{\partial F}{\partial V}
$$
Computing the pressure from Eq.(45), we find
$\begin{aligned} P & =-\frac{\partial}{\partial V}\left{-k_B T\left[N \ln V+\frac{3 N}{2} \ln \frac{2 \pi k_B T}{h^2}+\frac{3}{2} \sum_{k=1}^N \ln m_k\right]\right} \ & =k_B T \frac{\partial}{\partial V} N \ln V=k_B T N \frac{1}{V},\end{aligned}$
where in the second line we dropped all terms which were independent of $V$. Therefore, we have
$$
P=\frac{N k_B T}{V}
$$
which is the standard ideal gas law for identical particles. Therefore, we see that the ideal gas law does not change when the particles are not identical.

这是一份2023年的波士顿学院Boston College PHYS7722 物理统计学代写的成功案例




















统计物理学 Statistical Physics I|PHYS7721Boston College Assignment

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Assignment-daixieTM为您提供波士顿学院Boston College PHYS7721 Statistical Physics I 统计物理学代写代考辅导服务!





Instructions:

Statistical physics is a branch of physics that uses statistical methods to explain the behavior of systems made up of many interacting particles. It seeks to understand the collective behavior of these particles in terms of the laws of physics and probability theory.

In statistical physics, the properties of a macroscopic system, such as temperature, pressure, and entropy, are derived from the statistical properties of the individual particles that make up the system. This approach is based on the assumption that the particles are in thermal equilibrium and that their interactions can be treated statistically.

One of the central concepts in statistical physics is the partition function, which is used to calculate the thermodynamic properties of a system. The partition function is a sum over all possible states of the system, weighted by their probability.

Statistical physics has many applications in fields such as condensed matter physics, astrophysics, and biophysics. It is also used in the study of phase transitions, critical phenomena, and the behavior of complex systems.

统计物理学 Statistical Physics I|PHYS7721Boston College Assignment

问题 1.

For a particular model of a gene in a cell, the probability density that said gene produces a concentration $x$ of proteins during the cell cycle is given by
$$
p(x)=A\left(\frac{x}{b}\right)^N e^{-x / b},
$$
where $b$ is a biological constant with units of concentration, $N$ is a physical constant, and $A$ is a normalization parameter.
(a) The concentration of proteins that can be produced ranges from zero to infinite. What must $A$ be in order for Eq.(1) to be normalized?

证明 .

(a) Given the range of possible protein production, $x$ can go from 0 to $\infty$. Therefore, for $p(x)$ to be normalized, we must obtain 1 when we integrate the function over this entire domain:
$$
\int_0^{\infty} d x p(x)=1 .
$$
From the definition of the probability density we have
$$
\begin{aligned}
1 & =\int_0^{\infty} d x A\left(\frac{x}{b}\right)^N e^{-x / b} \
& =A \int_0^{\infty} d x\left(\frac{x}{b}\right)^N e^{-x / b} \
& =A \int_0^{\infty} d u b u^N e^{-u} \
& =A b \int_0^{\infty} d u u^N e^{-u},
\end{aligned}
$$
where we changed variables with $u=x / b$ in the third line, and factored the $u$-independent constant out of the integral in the final line. By the integral definition of factorial, we have
$$
N !=\int_0^{\infty} d u u^N e^{-u} .
$$
Therefore, the final line of Eq.(4) becomes
$$
1=A b N !,
$$
and we can conclude
$$
A=\frac{1}{b N !} .
$$

The normalized probability density is therefore
$$
p(x)=\frac{1}{b N !}\left(\frac{x}{b}\right)^N e^{-x / b} .
$$

问题 2. (b)What is the mean of the normalized probability density?

证明 .

(b) The mean of a random variable defined by the probability density $p(x)$ (which has a nonzero domain for $x \in[0, \infty)$ ) is
$$
\langle x\rangle=\int_0^{\infty} d x \operatorname{xp}(x) .
$$
Using Eq.(8) to compute this value, we obtain
$$
\begin{aligned}
\langle x\rangle & =\int_0^{\infty} d x x \frac{1}{b N !}\left(\frac{x}{b}\right)^N e^{-x / b} \
& =\frac{1}{N !} \int_0^{\infty} d x\left(\frac{x}{b}\right)^{N+1} e^{-x / b} \
& =\frac{1}{N !} \int_0^{\infty} d u b u^{N+1} e^{-u} \
& =b \frac{(N+1) !}{N !}
\end{aligned}
$$
where in the third line we performed a change of variables with $u=x / b$ and in the final line we used Eq. By the definition of factorial, we ultimately find
$$
\langle x\rangle=b(N+1)
$$

问题 3.

(c) For this probability distribution, compute the average
$$
\left\langle e^{x / a}\right\rangle,
$$
and write the result in terms of an infinite sum over a binomial coefficient. (Note that $e^x=$ $\sum_{j=0}^{\infty} x^j / j !$.)

证明 .

(c) We now seek to compute the average of $e^{x / a}$. Noting the Taylor series definition of the exponential
$$
e^{x / a}=\sum_{j=0}^{\infty} \frac{(x / a)^j}{j !},
$$
we have
$$
\begin{aligned}
\left\langle e^{x / a}\right\rangle & =\left\langle\sum_{j=0}^{\infty} \frac{(x / a)^j}{j !}\right\rangle \
& =\sum_{j=0}^{\infty} \frac{1}{j !} \frac{1}{a^j}\left\langle x^j\right\rangle .
\end{aligned}
$$
Computing $\left\langle x^j\right\rangle$ yields
$$
\begin{aligned}
\left\langle x^j\right\rangle & =\int_0^{\infty} d x x^j \frac{1}{b N !}\left(\frac{x}{b}\right)^N e^{-x / b} \
& =\frac{b^j}{b N !} \int_0^{\infty} d x\left(\frac{x}{b}\right)^{N+j} e^{-x / b} \
& =\frac{b^j}{b N !} \int_0^{\infty} d u b u^{N+j} e^{-u}
\end{aligned}
$$

$$
=b^j \frac{(N+j) !}{N !}
$$
where in the second line we multiplied the numerator and the denominator by $b^j$, in the third line we performed a change of variables $u=x / b$, and in the final line we used Eq.(5). Inserting this result into Eq.(13), we find
$$
\left\langle e^{x / a}\right\rangle=\sum \sum_{j=0}^{\infty} \frac{1}{j !} \frac{1}{a^j} b^j \frac{(N+j) !}{N !}=\sum_{j=0}^{\infty} \frac{(N+j) !}{j ! N !}\left(\frac{b}{a}\right)^j,
$$
or
$$
\left\langle e^{x / a}\right\rangle=\sum_{j=0}^{\infty}\left(\begin{array}{c}
N+j \
j
\end{array}\right)\left(\frac{b}{a}\right)^j
$$
We note that we could evaluate $\left\langle e^{x / a}\right\rangle$ directly using a change of variables in the argument of the exponential of the distribution. The result would be
$$
\begin{aligned}
\left\langle e^{x / a}\right\rangle & =\frac{1}{b N !} \int_0^{\infty} d x e^{x / a}\left(\frac{x}{b}\right)^N e^{-x / b} \
& =\frac{1}{b N !} \int_0^{\infty} d x\left(\frac{x}{b}\right)^N e^{-(1 / b-1 / a) x} \
& =\frac{1}{b N !} \int_0^{\infty} d u \frac{a b}{a-b}\left(\frac{a u}{a-b}\right)^N e^{-u} \
& =\frac{1}{N !}\left(\frac{a}{a-b}\right)^{N+1} \int_0^{\infty} d u u^N e^{-u} \
& =\frac{1}{(1-b / a)^{N+1}},
\end{aligned}
$$
where in the second line we made the change of variables $u=x(a-b) / a b$. Considering Eq.(16), the result Eq.(17) implies
$$
\sum_{j=0}^{\infty}\left(\begin{array}{c}
N+j \
j
\end{array}\right) q^j=\frac{1}{(1-q)^{N+1}}
$$

这是一份2023年的波士顿学院Boston College PHYS7721统计物理学代写的成功案例




















经典力学 Classical Mechanics|PHYS7711Boston College Assignment

0

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Instructions:

Classical mechanics is a branch of physics that deals with the motion of objects under the influence of forces. It provides a framework for describing and predicting the behavior of physical systems ranging from the motion of planets and satellites to the behavior of atoms and molecules.

Classical mechanics is based on three fundamental laws of motion, known as Newton’s laws. The first law states that an object at rest will remain at rest, and an object in motion will continue to move in a straight line with constant velocity, unless acted upon by an external force. The second law relates the force acting on an object to its acceleration: F = ma, where F is the force, m is the mass of the object, and a is its acceleration. The third law states that for every action, there is an equal and opposite reaction.

In addition to these laws, classical mechanics also includes the concept of energy, both kinetic and potential. Kinetic energy is the energy possessed by an object due to its motion, while potential energy is the energy associated with the position or configuration of an object.

Classical mechanics is essential for understanding many areas of science and technology, including astronomy, engineering, and mechanics. It forms the foundation for many other branches of physics, such as thermodynamics, electromagnetism, and quantum mechanics.

经典力学 Classical Mechanics|PHYS7711Boston College Assignment

问题 1.

Consider the motion of an object close to the surface of the Earth moving under the influence of Earth’s gravity.
a) The gravitational force law
$$
\vec{F}=-\frac{G M m}{r^2} \hat{r}
$$
reduces to
$$
\vec{F}=-g m \hat{z}
$$
at the surface with $z$ pointing away from the center of the Earth (i.e., “up”). Express $g$ in terms of $G$, $M_{\oplus}$ and $R_{\oplus}$. Compute $g$ in SI units.

证明 .

At the surface of the Earth, the distance $r$ from the center of the Earth to the object is equal to the radius of the Earth, $R_{\oplus}$. Thus, we have

$\vec{F}=-\frac{G M_{\oplus} m}{R_{\oplus}^2} \hat{r} \approx-\frac{G M_{\oplus} m}{R_{\oplus}^2} \hat{z}$

where we have approximated $\hat{r}$ by $\hat{z}$ because the surface of the Earth is approximately a plane perpendicular to the $z$-axis.

The magnitude of the force is given by

$F=|\vec{F}|=\frac{G M_{\oplus} m}{R_{\oplus}^2}$

By Newton’s second law, the force is related to the object’s mass $m$ and acceleration $a$ via

$\vec{F}=m \vec{a}$

Since the object is moving only vertically, we have $\vec{a}=a\hat{z}$ and $|\vec{a}|=a$. Therefore,

F=ma=mg

where $g=|\vec{a}|$ is the acceleration due to gravity. Combining these equations, we obtain

$m g=\frac{G M_{\oplus} m}{R_{\oplus}^2}$

which can be solved for $g$ to give

$g=\frac{G M_{\oplus}}{R_{\oplus}^2}$

Substituting the values for $G$, $M_{\oplus}$, and $R_{\oplus}$ in SI units, we have

$g=\frac{\left(6.674 \times 10^{-11} \mathrm{~m}^3 \mathrm{~kg}^{-1} \mathrm{~s}^{-2}\right) \times\left(5.9722 \times 10^{24} \mathrm{~kg}\right)}{\left(6.371 \times 10^6 \mathrm{~m}\right)^2} \approx 9.81 \mathrm{~m} / \mathrm{s}^2$

Therefore, the acceleration due to gravity at the surface of the Earth is approximately $9.81 ,\mathrm{m/s^2}$.

问题 2. Consider the motion of an object close to the surface of the Earth moving under the influence of Earth’s gravity. b) For a cannonball fired at velocity $v_o$ and angle $\theta$ above the horizon on the Moon, find the range; the distance from the cannon at which the cannonball hits the surface of the Moon. (You will need to recompute $g$ for the Moon, but the lack of air on the Moon makes this calculation much easier there than on Earth.)

证明 .

The range, $R$, of a projectile launched at an angle $\theta$ above the horizon with initial velocity $v_0$ is given by:

$$R = \frac{v_0^2\sin(2\theta)}{g},$$

where $g$ is the acceleration due to gravity.

On the Moon, the acceleration due to gravity is $g_{\text{Moon}} = 1.62 \text{ m/s}^2$. Therefore, the range of a cannonball fired at velocity $v_0$ and angle $\theta$ above the horizon on the Moon is:

$$R = \frac{v_0^2\sin(2\theta)}{g_{\text{Moon}}}.$$

Note that since there is no air on the Moon, we do not need to worry about air resistance affecting the motion of the cannonball.

问题 3.

Hooke’s law for a spring of constant $k$ is $F=-k x$. A mass $m$ is pushed from position $x_o$ with velocity $v_o$ at $t=0$. Find the subsequent motion, $x(t)$.

证明 .

The equation of motion for a mass on a spring is given by Newton’s second law: $F = ma$, where $F$ is the force exerted by the spring, $m$ is the mass of the object attached to the spring, and $a$ is its acceleration. In this case, the force exerted by the spring is given by Hooke’s law, $F = -kx$, where $x$ is the displacement of the mass from its equilibrium position.

Assuming that the mass is only moving along the $x$-axis, we can write the equation of motion as:

ma=−kx

Since $a = \frac{d^2x}{dt^2}$, we can rewrite this as:

$m \frac{d^2 x}{d t^2}=-k x$

This is a second-order ordinary differential equation, which we can solve using the characteristic equation method. We assume that the solution takes the form:

$x(t)=A \cos (\omega t)+B \sin (\omega t)$

where $A$ and $B$ are constants that depend on the initial conditions, and $\omega$ is the angular frequency of the oscillation. Substituting this into the differential equation, we get:

$-\omega^2 m(A \cos (\omega t)+B \sin (\omega t))=-k(A \cos (\omega t)+B \sin (\omega t))$

Dividing both sides by $A\cos(\omega t) + B\sin(\omega t)$, we get:

$-\omega^2 m=-k \Rightarrow \omega=\sqrt{\frac{k}{m}}$

So the general solution is:

$x(t)=A \cos \left(\sqrt{\frac{k}{m}} t\right)+B \sin \left(\sqrt{\frac{k}{m}} t\right)$

To find the constants $A$ and $B$, we use the initial conditions. At $t=0$, the mass is at position $x_0$ with velocity $v_0$. So we have:

$x(0)=x_0 \Rightarrow A=x_0$

and

$v(0)=\left.\frac{d x}{d t}\right|_{t=0}=v_0=-\sqrt{\frac{k}{m}} x_0+B \sqrt{\frac{k}{m}}$

Solving for $B$, we get:

$B=\frac{v_0+\sqrt{\frac{k}{m}} x_0}{\sqrt{\frac{k}{m}}}$

Therefore, the solution for $x(t)$ is:

$x(t)=x_0 \cos \left(\sqrt{\frac{k}{m}} t\right)+\frac{v_0}{\sqrt{\frac{k}{m}}} \sin \left(\sqrt{\frac{k}{m}} t\right)$

This is the position of the mass as a function of time, given its initial position and velocity.

这是一份2023年的波士顿学院Boston College PHYS7711 经典力学代写的成功案例