《Quantum Chemistry》章末总结2

第二章,在讲薛定谔方程之前先讲了一些经典波动方程的铺垫。

Chapter 2 The Classical Wave Equation

We learned in Chapter Ⅰ that matter can behave as a wave, so it’s not surprising that the Schrödinger equation (sometimes called the Schrödinger wave equation) describes wavelike behavior.

Not only does the classical wave equation provide a physical background to the Schrodinger equation, but, in addition, the mathematics involved in solving the
classical wave equation are central to any discussion of quantum mechanics.

Because most students of physical chemistry have little experience with classical wave equations, this chapter discusses this topic.

这一章可以算作物理基础的部分,不过嘛,考虑到我的数理水平,有必要写一写。

2.1 The One-Dimensional Wave Equation Describes the Motion of a Vibrating String

Consider a uniform string stretched between two fixed points, as shown in Figure 2.1. The maximum displacement of the string from its equilibrium horizontal position is called its amplitude. If we let u(x,t)u(x,t) be the displacement of the string, then u(x,t)u(x,t) satisfies the equation:

2ux2=1v22ut2\frac {\partial^2u}{\partial x^2}=\frac 1{v^2} \frac {\partial^2 u}{\partial t^2}

QC-fig2.1

where vv is the speed with which a disturbance moves along the string. The equation is the classical wave equation.

In addition to having to satisfy Equation, the displacement u(x,t)u(x,t) must satisfy certain physical conditions as well. Because the ends of the string are held fixed, the displacement at these two points is always zero, and so we have the requirement that:

u(0,t)=0andu(l,t)=0(for all t)u(0,t)=0 \quad and \quad u(l,t)=0 \quad (for\ all\ t)

These two conditions are called boundary conditions because they specify the behavior of u(x,t)u(x,t) at the boundaries. Generally, a partial differential equation must be solved subject to certain boundary conditions, the nature of which will be apparent on physical grounds.

边界条件是非常重要的条件,对于解方程来说很重要,同时一般具有明确的物理意义。

2.2 The Wave Equation Can Be Solved by the Method of Separation of Variables

The classical wave equation, as well as the Schrodinger equation and many other partial differential equations that arise in physical chemistry, can be solved readily by a method called separation of variables. We shall use the problem of a vibrating string to illustrate this method.

The key step in the method of separation of variables is to assume that u(x,t)u(x,t) factors into a function of xx, X(x)X(x), times a function of tt, T(t)T(t), or that:

u(x,t)=X(x)T(t)u(x,t)=X(x)T(t)

We can obtain:

1X(x)d2X(x)dx2=1v2T(t)d2T(t)dt2\frac 1{X(x)}\frac {d^2X(x)}{dx^2}=\frac 1{v^2T(t)}\frac {d^2T(t)}{dt^2}

The only way for the equality of the two sides to be preserved under any variation of xx and tt is for each side to be equal to a constant. If we let this constant be KK, we can write:

1X(x)d2X(x)dx2=K\frac 1{X(x)}\frac {d^2X(x)}{dx^2} = K

and

1v2T(t)d2T(t)dt2=K\frac 1{v^2T(t)}\frac {d^2T(t)}{dt^2}=K

where KK is called the separation constant and will be determined later.

We do not know right now whether KK is positive, negative, or even zero. Let’s first assume that K=0K=0. In this case, equations can be integrated immediately to find:

X(x)=a1x+b1T(t)=a2t+b2X(x)=a_1x+b_1 \\ T(t)=a_2t+b_2

In terms of X(x)X(x) and T(t)T(t), the boundary conditions are:

u(0,t)=X(0)T(t)=0andu(l,t)=X(l)T(t)=0u(0,t)=X(0)T(t)=0 \quad and \quad u(l,t)=X(l)T(t)=0

Because T(t)T(t) certainly does not vanish for all tt, we must have that:

X(0)=0andX(l)=0X(0)=0\quad and \quad X(l)=0

we conclude that the only way to satisfy equations is for a1=b1=0a_1=b_1=0, which means that X(x)=0X(x)=0 and that u(x,t)=0u(x,t)=0 for all xx. This is called a trivial solution to The equation and is of no physical interest. Not that every solution to the equation is physically acceptable.

Now let’s assume that K>0K>0. To this end, write KK as k2k^2, where kk is real. This assures that KK is positive because it is the square of a real number.

d2X(x)dx2k2X(x)=0\frac {d^2X(x)}{dx^2}-k^2X(x)=0

Experience shows that solutions to a linear differential equation with constant coefficients whose right side is equal to zero are of the form X(x)=eαxX(x)=e^{\alpha x}, where α\alpha is a constant to be determined.

这里的“经验”来自于高等数学的学习XD

We now look for a solution:

α=±k\alpha =\pm k

Applying the boundary conditions:

c1+c2=0andc1ekl+c2ekl=0c_1+c_2=0 \quad and \quad c_1e^{kl}+c_2e^{-kl}=0

The only way to satisfy these conditions is with c1=c2=0c_1=c_2=0, and so once again, we find only a trivial solution.

2.3 Some Differential Equations Have Oscillatory Solutions

Let’s hope that assuming KK to be negative gives us something interesting. If we set K=β2K=-\beta^2, then KK is negative if β\beta is real.

d2X(x)dx2+β2X(x)=0\frac {d^2X(x)}{dx^2} + \beta^2X(x)=0

The general solution is:

X(x)=c1eiβx+c2eiβxX(x)=c_1e^{i\beta x}+c_2e^{-i\beta x}

It is sometimes more convenient to rewrite expressions using Euler’s formula:

X(x)=(c1+c2)cosβx+(ic1ic2)sinβx=c3eiβx+c4eiβxX(x)=(c_1+c_2)cos\beta x + (ic_1-ic_2)sin\beta x = c_3e^{i\beta x}+c_4e^{-i\beta x}

We see that the general solution to equation can be written as:

X(x)=Acosβx+BsinβxX(x)=Acos\beta x+Bsin\beta x

The condition at the boundary says that:

X(l)=Bsinβl=0X(l)=Bsin\beta l=0

So:

βl=nπn=1,2,3,\beta l=n\pi \quad n=1,2,3,\cdots

Where we have omitted the n=0n=0 case because it leads to β=0\beta=0, and a trivial solution. So far, then, we have that:

X(x)=BsinnπxlX(x)=Bsin\frac {n\pi x}l

这个形式虽然是从经典波动方程中推出的,但是很快我们就会在量子力学的势箱中再次遇到这种形式。

2.4 The General Solution to the Wave Equation Is a Superposition of Normal Modes

Remember the equation:

d2T(t)dt2+β2v2T(t)=0\frac {d^2T(t)}{dt^2}+\beta^2v^2T(t)=0

The general solution to equation is:

T(t)=Dcosωnt+EsinωntT(t)=Dcos\omega_nt+Esin\omega_nt

Where ωn=βv=nπv/l\omega_n=\beta v=n\pi v/l. We have no conditions to specify D and E, so the amplitude is:

u(x,t)=X(x)T(t)=(Bsinnπxl)(Dcosωnt+Esinωnt)=(Fcosωnt+Gsinωnt)sinnπxln=1,2,3,\begin{aligned} u(x,t) &=X(x)T(t)=(Bsin\frac {n\pi x}l)(Dcos\omega_nt+Esin\omega_nt) \\[3mm] &=(Fcos\omega_nt+Gsin\omega_nt)sin\frac {n\pi x}l \quad n=1,2,3,\cdots \end{aligned}

Because there is a u(x,t)u(x,t) for each integer nn and because the values of FF and GG may depend on nn, we should write u(x,t)u(x,t) as:

un(x,t)=(Fncosωnt+Gnsinωnt)sinnπxln=1,2,u_n(x,t)=(F_ncos\omega_nt+G_nsin\omega_nt)sin\frac {n\pi x}l \quad n=1,2,\cdots

Because each un(x,t)u_n(x,t) is a solution to the linear differential equation, their sum is also a solution and is, in fact, the general solution. Therefore, we have:

u(x,t)=n=1(Fncosωnt+Gnsinωnt)sinnπxln=1,2,u(x,t)=\sum_{n=1}^{\infin}(F_ncos\omega_nt+G_nsin\omega_nt)sin\frac {n\pi x}l \quad n=1,2,\cdots

Fcosωt+GsinωtFcos\omega t+Gsin\omega t can be written in the equivalent form, Acos(ωnt+ϕn)Acos(\omega_nt+\phi_n), where AA and are constants expressible in terms of FF and GG. The quantity AA is the amplitude of the wave and ϕ\phi is called the phase angle.

u(x,t)=n=1Ancos(ωnt+ϕn)sinnπxl=n=1un(x,t)u(x,t)=\sum_{n=1}^{\infin}A_ncos(\omega_nt+\phi_n)sin\frac {n\pi x}l=\sum_{n=1}^{\infin}u_n(x,t)

The equation has a nice physical interpretation. Each un(x,t)u_n(x,t) is called a normal mode, and the time dependence of each normal mode represents harmonic motion of frequency.

νn=ωn2π=νn2π\nu_n=\frac {\omega_n}{2\pi}=\frac {\nu n}{2\pi}

The waves shown in Figure 2.2 are called standing waves because the positions of the nodes are fixed in time. Between the nodes, the string oscillates up and down.

QC-fig2.2

It is easy to continue and show that the number of nodes is equal to n1n-1.

波动方程的通解是一系列特解的叠加,每一个特解在物理学中称为简正模,因此一般振动其实是一系列简正模的线性组合。

2.5 A Vibrating Membrane Is Described by a Two-Dimensional Wave Equation

The generalization of wave equation to two dimensions is:

2ux2+2uy2=1v22ut2\frac {\partial^2u}{\partial x^2}+\frac {\partial^2u}{\partial y^2}=\frac {1}{v^2}\frac {\partial^2u}{\partial t^2}

We will apply this equation to a rectangular membrane whose entire perimeter is clamped. By referring to the geometry in Figure 2.3, we see that the boundary conditions that u(x,y,t)u(x,y,t) must satisfy (because its four edges are clamped) are:

u(0,y)=u(a,y)=0andu(x,0)=u(x,b)=0(for all t)u(0,y)=u(a,y)=0 \quad and \quad u(x,0)=u(x,b)=0 \quad (for\ all\ t)

QC-fig2.3

By applying the method of separation of variables to equation, we assume that u(x,y,t)u(x,y,t) can be written as the product of a spatial part and a temporal part or that:

u(x,y,t)=F(x,y)T(t)u(x,y,t)=F(x,y)T(t)

We can find:

1v2T(t)d2Tdt2=1F(x,y)(2Fx2+2Fy2)\frac 1{v^2T(t)}\frac {d^2T}{dt^2}=\frac 1{F(x,y)}(\frac {\partial^2 F}{\partial x^2}+\frac {\partial^2F}{\partial y^2})

Anticipating that the separation constant will be negative, as it was in the previous sections, we write it as β2-\beta^2 and obtain the two separate equations:

d2Tdt2+v2β2T(t)=0\frac {d^2T}{dt^2}+v^2\beta^2T(t)=0

and

2Fx2+2Fy2+β2F(x,y)=0\frac {\partial^2F}{\partial x^2}+\frac {\partial^2F}{\partial y^2}+\beta^2F(x,y)=0

We once again use separation of variables. Substitute F(x,y)=X(x)Y(y)F(x,y)=X(x)Y(y) into equation and divide both sides by X(x)Y(y)X(x)Y(y) to obtain:

1X(x)d2Xdx2+1Y(y)d2Ydy2+β2=0\frac 1{X(x)}\frac {d^2X}{dx^2}+\frac 1{Y(y)}\frac {d^2Y}{dy^2}+\beta^2=0

Again we argue that because xx and yy are independent variables, the only way this equation can be valid is that:

1X(x)d2Xdx2=p2and1Y(y)d2Ydy2=q2\frac 1{X(x)}\frac {d^2X}{dx^2}=-p^2 \quad and \quad \frac 1{Y(y)}\frac {d^2Y}{dy^2}=-q^2

p2+q2=β2p^2+q^2=\beta^2

The solutions:

X(x)=Acospx+BsinpxY(y)=Ccosqy+DsinqyX(x)=Acospx+Bsinpx \quad Y(y)=Ccosqy+Dsinqy

The boundary conditions imply that:

X(0)=X(a)=0Y(0)=Y(b)=0X(0)=X(a)=0 \quad Y(0)=Y(b)=0

So that:

Xn(x)=Bsinnπxan=1,2,X_n(x)=Bsin\frac {n\pi x}{a} \quad n=1,2,\cdots

Ym(y)=Dsinnπybm=1,2,Y_m(y)=Dsin\frac {n\pi y}{b} \quad m=1,2,\cdots

Recalling that p2+q2=β2p^2+q^2=\beta^2, we see that:

βnm=π(n2a2+m2b2)1/2m=n=1,2,\beta_{nm}=\pi \left(\frac {n^2}{a^2}+\frac {m^2}{b^2} \right)^{1/2} \quad m=n=1,2,\cdots

Now we solve the equation for the time dependence:

Tnm(t)=Enmcosωnmt+Fnmsinωnmt=Gnmcos(ωnmt+ϕ)T_{nm}(t)=E_{nm}cos\omega_{nm}t+F_{nm}sin\omega_{nm}t=G_{nm}cos(\omega_{nm}t+\phi)

One solution to equation is given by the product unm(x,y,t)=Xn(x)Ym(y)Tnm(t)u_{nm}(x,y,t)=X_n(x)Y_m(y)T_{nm}(t),and the general solution is given by:

u(x,y,t)=n=1m=1unm(x,y,t)u(x,y,t)=\sum_{n=1}^{\infin}\sum_{m=1}^{\infin}u_{nm}(x,y,t)

As in the one-dimensional case of a vibrating string, we see that the general vibrational motion of a rectangular drum can be expressed as a superposition of normal modes, unm(x,y,t)u_{nm}(x,y,t). Some of these modes are shown in Figure 2.4.

QC-fig2.4

Note that in this two-dimensional problem we obtain nodal lines. In two-dimensional problems, the nodes are lines, as compared with points in one-dimensional problems.

Figure 2.4 shows the normal modes for a case in which aba\ne b. The case in which a=ba=b is an interesting one.

When a=ba=b:

ωnm=νβnm=νπa(n2+m2)1/2\omega_{nm}=\nu\beta_{nm}=\frac {\nu\pi}{a} \left(n^2+m^2 \right)^{1/2}

We see that ω12=ω21=5νπ/a\omega_{12}=\omega_{21}=\sqrt5\nu\pi/a in this case; yet the normal modes u12(x,y,t)u_{12}(x,y,t) and u21(x,y,t)u_{21}(x,y,t) are not the same, as seen from Figure 2.5. This is an example of a degeneracy, and we say that the frequency ω12=ω21\omega_{12}=\omega_{21} is doubly degenerate or two-fold degenerate.

QC-fig2.5

Note that the phenomenon of degeneracy arises because of the symmetry introduced when a=ba=b. There will be at least a two-fold degeneracy when mnm\ne n because m2+n2=n2+m2m^2+n^2=n^2+m^2. We will see that the concept of degeneracy arises in quantum mechanics also.

2.6 A Characteristic Property of Waves Is That They Lead to Interference

We saw in Section 2.4 that a traveling wave can be expressed as a superposition of standing waves. To see this more explicitly, start with this:

u(x,t)=cosω1tsinπxlu(x,t)=cos\omega_1tsin\frac {\pi x}{l}

Now use the trigonometric identity to write u(x,t)u(x,t) in the form:

u(x,t)=12sin[πt(x+vt)]+12sin[πl(xvt)]u(x,t)=\frac 12sin \left[\frac {\pi}t(x+vt) \right]+\frac 12sin \left[\frac {\pi}l(x-vt) \right]

Note that the shape does not change with time; the curve simply moves uniformly to the right. In fact, the speed with which it moves is vv, which you can see by setting π(xvt)/l=constant\pi(x-vt)/l=constant, and then differentiating with respect to tt to find that dx/dt=vdx/dt=v.

Introduce the angular frequency ω=2πν\omega=2\pi \nu (radians per second) and k=2π/λk=2\pi/\lambda to write the expression:

f(x,t)=sin(ktωt)f(x,t)=sin(kt-\omega t)

The equation expresses a traveling wave in very common notation. The quantity kk is called the wave vector. In one dimension, kk is just a scalar, but in two or three dimensions kk is a vector that describes the direction of propagation of the wave. When dealing with traveling waves, it is usually more convenient to use a complex exponential notation and to express f(x,t)f(x,t) above as:

f(x,t)=ei(kxωt)f(x,t)=e^{i(kx-\omega t)}

A wave of the form described by the equation is called a plane wave because it is uniform in the y-z plane.

Let’s use the equation to derive the interference pattern of a two-slit experiment like that discussed in Section 1.13.

QC-fig2.6

If we let x0x_0 be the distance S1PS_1P in Figure 2.6, we can write the electric field at the point P as:

E(θ)=E0ei(kx0ωt)+E0ei(k(x0+dsinθ)ωt)=E0ei(kx0ωt)(1+eikdsinθ)=E0(1+eikdsinθ)ei(kx0ωt)=A(θ)ei(kx0ωt)\begin{aligned} E(\theta) &=E_0e^{i(kx_0-\omega t)}+E_0e^{i(k(x_0+dsin\theta)-\omega t)} \\ &=E_0e^{i(kx_0-\omega t)}(1+e^{ikdsin\theta}) \\ &=E_0(1+e^{ikdsin\theta})e^{i(kx_0-\omega t)} \\ &=A(\theta)e^{i(kx_0-\omega t)} \end{aligned}

Where A(θ)A(\theta) is the amplitude of ei(kx0ωt)e^{i(kx_0-\omega t)} We have written EE and AA as E(θ)E(\theta) and A(θ)A(\theta) to emphasize their dependence on the angle θ\theta. The intensity of the radiation is given by:

I(θ)=A(θ)A(θ)I(\theta)=A^*(\theta)A(\theta)

I(θ)=2E02[1+cos(kdsinθ)]I(\theta)=2E_0^2 \left[1+cos(kdsin\theta) \right]

Using the k=2π/λk=2\pi/\lambda and trigonometric identity to write this as:

I(θ)=4E02cos2πdsinθλI(\theta)=4E_0^2cos^2\frac {\pi dsin\theta}{\lambda}

Note that I(θ)I(\theta) achieves maximum values when cos2(πdsinθ/λ)cos^2(\pi dsin\theta/\lambda), or when:

πdsinθλ=nπn=0,±1,±2,\frac {\pi d sin\theta}{\lambda}=n\pi \quad n=0,\pm1,\pm2,\cdots

Note that this is just the relation (dsinθ=nλdsin\theta=n\lambda) that we derived in Section 1.13.

QC-fig2.7

This chapter has presented a discussion of the wave equation and its solutions. In Chapter 3, we will use the mathematical methods developed here.

总结

本章作为物理基础,或者说是物理复习其实是很重要的,因为下一章在向经典理论中引入量子力学的过程中,仍会用到这一章涉及的方法和概念,如线性变分法等。作为一本化学书,本章的内容也是充分考虑到读者的物理水平,讲解还是很细致的。

这章花的时间比我预计的长了不少,主要是需要编辑不少LaTeX\LaTeX.


《Quantum Chemistry》章末总结2
http://argon-gas.top/p/15101.html
作者
Sun
发布于
2024年1月18日
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