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-rw-r--r--source/know/concept/bernoullis-theorem/index.md29
-rw-r--r--source/know/concept/central-limit-theorem/index.md26
-rw-r--r--source/know/concept/clausius-mossotti-relation/index.md27
-rw-r--r--source/know/concept/ehrenfests-theorem/index.md75
-rw-r--r--source/know/concept/ficks-laws/index.md54
-rw-r--r--source/know/concept/grad-shafranov-equation/index.md13
-rw-r--r--source/know/concept/holomorphic-function/index.md27
-rw-r--r--source/know/concept/larmor-precession/index.md26
-rw-r--r--source/know/concept/lubrication-theory/index.md67
-rw-r--r--source/know/concept/lyddane-sachs-teller-relation/index.md45
-rw-r--r--source/know/concept/prandtl-equations/index.md58
-rw-r--r--source/know/concept/probability-current/index.md66
-rw-r--r--source/know/concept/rabi-oscillation/index.md37
-rw-r--r--source/know/concept/time-dependent-perturbation-theory/index.md4
14 files changed, 277 insertions, 277 deletions
diff --git a/source/know/concept/bernoullis-theorem/index.md b/source/know/concept/bernoullis-theorem/index.md
index 867c443..2795f22 100644
--- a/source/know/concept/bernoullis-theorem/index.md
+++ b/source/know/concept/bernoullis-theorem/index.md
@@ -12,36 +12,21 @@ layout: "concept"
For inviscid fluids, **Bernouilli's theorem** states
that an increase in flow velocity $$\va{v}$$ is paired
with a decrease in pressure $$p$$ and/or potential energy.
-For a qualitative argument, look no further than
-one of the [Euler equations](/know/concept/euler-equations/),
-with a [material derivative](/know/concept/material-derivative/):
-
-$$\begin{aligned}
- \frac{\mathrm{D} \va{v}}{\mathrm{D} t}
- = \pdv{\va{v}}{t} + (\va{v} \cdot \nabla) \va{v}
- = \va{g} - \frac{\nabla p}{\rho}
-\end{aligned}$$
-
-Assuming that $$\va{v}$$ is constant in $$t$$,
-it becomes clear that a higher $$\va{v}$$ requires a lower $$p$$.
-
-
-## Simple form
-
-For an incompressible fluid
+Quantitatively, for an incompressible fluid
with a time-independent velocity field $$\va{v}$$ (i.e. **steady flow**),
-Bernoulli's theorem formally states that the
-**Bernoulli head** $$H$$ is constant along a streamline:
+Bernoulli's theorem states that
+the **Bernoulli head** $$H$$ is constant along every streamline:
$$\begin{aligned}
\boxed{
H
- = \frac{1}{2} \va{v}^2 + \Phi + \frac{p}{\rho}
+ \equiv \frac{1}{2} |\va{v}|^2 + \Phi + \frac{p}{\rho}
}
\end{aligned}$$
Where $$\Phi$$ is the gravitational potential, such that $$\va{g} = - \nabla \Phi$$.
-To prove this theorem, we take the material derivative of $$H$$:
+To prove this theorem, we take the
+[material derivative](/know/concept/material-derivative/) of $$H$$:
$$\begin{aligned}
\frac{\mathrm{D} H}{\mathrm{D} t}
@@ -50,7 +35,7 @@ $$\begin{aligned}
+ \frac{1}{\rho} \frac{\mathrm{D} p}{\mathrm{D} t}
\end{aligned}$$
-In the first term we insert the Euler equation,
+In the first term we insert the [Euler equation](/know/concept/euler-equations/),
and in the other two we expand the derivatives:
$$\begin{aligned}
diff --git a/source/know/concept/central-limit-theorem/index.md b/source/know/concept/central-limit-theorem/index.md
index 42bc05b..0ebad36 100644
--- a/source/know/concept/central-limit-theorem/index.md
+++ b/source/know/concept/central-limit-theorem/index.md
@@ -17,7 +17,8 @@ and calculating $$M$$ averages $$\mu_m$$ (which involves summing over $$N$$),
the resulting means $$\mu_m$$ are normally distributed
across the $$M$$ samples if $$N$$ is sufficiently large.
-More formally, for $$N$$ independent variables $$x_n$$ with probability distributions $$p(x_n)$$,
+More formally, for $$N$$ independent variables $$x_n$$
+with probability distributions $$p(x_n)$$,
we define the following totals of all variables, means and variances:
$$\begin{aligned}
@@ -39,9 +40,9 @@ $$\begin{aligned}
}
\end{aligned}$$
-We prove this below,
-but first we need to introduce some tools.
-Given a probability density $$p(x)$$, its [Fourier transform](/know/concept/fourier-transform/)
+We prove this below, but first we need to introduce some tools.
+Given a probability density $$p(x)$$,
+its [Fourier transform](/know/concept/fourier-transform/)
is called the **characteristic function** $$\phi(k)$$:
$$\begin{aligned}
@@ -70,7 +71,8 @@ $$\begin{aligned}
= i^n \: \overline{x^n}
\end{aligned}$$
-Next, the **cumulants** $$C^{(n)}$$ are defined from the Taylor expansion of $$\ln\!\big(\phi(k)\big)$$:
+Next, the **cumulants** $$C^{(n)}$$ are defined
+from the Taylor expansion of $$\ln\!\big(\phi(k)\big)$$:
$$\begin{aligned}
\ln\!\big( \phi(k) \big)
@@ -96,9 +98,8 @@ $$\begin{aligned}
= - \overline{x}^2 + \overline{x^2} = \sigma^2
\end{aligned}$$
-Now that we have introduced these tools,
-we define $$t$$ as the sum
-of $$N$$ independent variables $$x_n$$, in other words:
+Now that we have introduced these tools, we repeat our definition of $$t$$
+as the sum of $$N$$ independent variables $$x_n$$, in other words:
$$\begin{aligned}
t
@@ -116,10 +117,11 @@ $$\begin{aligned}
&= \Big( p_1 * \big( p_2 * ( ... * (p_N * \delta))\big)\Big)(t)
\end{aligned}$$
-In other words, the integrals pick out all combinations of $$x_n$$ which
-add up to the desired $$t$$-value, and multiply the probabilities
-$$p(x_1) p(x_2) \cdots p(x_N)$$ of each such case. This is a convolution,
-so the [convolution theorem](/know/concept/convolution-theorem/)
+In other words, we integrate over all possible combinations of $$x_n$$,
+and use the Dirac delta function to pick out the combinations
+where the $$x_n$$ add up to the desired $$t$$-value,
+and multiply the probabilities $$p(x_1) \, p(x_2) \cdots p(x_N)$$ of each such case.
+This is a convolution, so the [convolution theorem](/know/concept/convolution-theorem/)
states that it is a product in the Fourier domain:
$$\begin{aligned}
diff --git a/source/know/concept/clausius-mossotti-relation/index.md b/source/know/concept/clausius-mossotti-relation/index.md
index 03bdcac..61332db 100644
--- a/source/know/concept/clausius-mossotti-relation/index.md
+++ b/source/know/concept/clausius-mossotti-relation/index.md
@@ -18,19 +18,21 @@ $$\begin{aligned}
\end{aligned}$$
If there are $$N$$ such bodies per unit volume,
-the polarization density $$\vb{P} = \varepsilon_0 \chi_e \vb{E}$$
-with $$\vb{P} = N \vb{p}$$ suggests that $$\chi_e = N \alpha$$.
-However, this is an underestimation:
+the macroscopic polarization density $$\vb{P} = \varepsilon_0 \chi_e \vb{E}$$
+with $$\vb{P} = N \vb{p}$$ may suggest that $$\chi_e = N \alpha$$.
+However, this turns out to be an underestimation:
each body's induced dipole creates its own electric field,
weakening the field felt by its neighbors.
-We need to include this somehow,
-but $$\alpha$$ is defined for a single dipole in a vacuum.
+To calculate $$\chi_e$$ from $$\alpha$$, we need to include this effect,
+but $$\alpha$$ is defined only for a single dipole in a vacuum.
-Let $$\vb{E}_\mathrm{int}$$ be the uniform internal field excluding the dipoles' contributions,
-and $$\vb{E}(\vb{r})$$ the net field including them.
+Let $$\vb{E}_\mathrm{int}$$ be the uniform internal field
+excluding the dipoles' contributions,
+and $$\vb{E}(\vb{r})$$ be the net field including them.
Assume that the dipoles $$\vb{p}_i$$ are arranged
in a regular crystal lattice at sites $$\vb{R}_i$$.
-Then $$\vb{E}(\vb{r})$$ is the sum of $$\vb{E}_\mathrm{int}$$ and all the dipoles' fields:
+Then $$\vb{E}(\vb{r})$$ is the sum of $$\vb{E}_\mathrm{int}$$
+and all the dipoles' fields:
$$\begin{aligned}
\vb{E}(\vb{r})
@@ -45,6 +47,7 @@ $$\begin{aligned}
= - \frac{1}{4 \pi \varepsilon_0} \nabla \bigg( \frac{\vu{r} \cdot \vb{p}_i}{|\vb{r}|^2} \bigg)
\end{aligned}$$
+
{% include proof/start.html id="proof-dipole" -%}
The atoms or molecules $$\vb{p}_i$$ need not be perfect dipoles,
as long as they approximate one when viewed from a distance
@@ -84,6 +87,7 @@ $$\begin{aligned}
Then the corresponding electric field $$\vb{E}_i$$ is given by $$- \nabla V_i$$ as is well known.
{% include proof/end.html id="proof-dipole" -%}
+
The dipole $$\vb{p}_0$$ at $$\vb{r} = 0$$
feels a net local field $$\vb{E}_\mathrm{loc}$$, given below.
The crystal's symmetry ensures that all its neighbors' fields cancel out:
@@ -101,9 +105,10 @@ $$\begin{aligned}
Even if there is no regular lattice, this result still holds well enough,
as long as the dipoles are uniformly distributed over a large volume.
-So what was the point of including $$\vb{E}_i(\vb{r})$$ in the first place?
-Well, keep in mind that the sum over neighbors is nonzero for $$\vb{r} \neq \vb{R}_i$$,
-which *does* affect the macroscopic field $$\vb{E}$$, defined as:
+So... if all the neighbors' fields cancel out at $$\vb{r} \in \vb{R}_i$$,
+then what was the point of including $$\vb{E}_i(\vb{r})$$ in the first place?
+Well, those contributions do *not* cancel out for $$\vb{r} \not{\!\!\in} \: \vb{R}_i$$,
+and this fact *does* affect the average macroscopic field $$\vb{E}$$, defined as:
$$\begin{aligned}
\vb{E}
diff --git a/source/know/concept/ehrenfests-theorem/index.md b/source/know/concept/ehrenfests-theorem/index.md
index fba0192..14d17fa 100644
--- a/source/know/concept/ehrenfests-theorem/index.md
+++ b/source/know/concept/ehrenfests-theorem/index.md
@@ -8,20 +8,19 @@ categories:
layout: "concept"
---
-In quantum mechanics, **Ehrenfest's theorem** gives a general expression for the
-time evolution of an observable's expectation value $$\expval{\hat{L}}$$.
-
-The time-dependent Schrödinger equation is as follows,
+In quantum mechanics, **Ehrenfest's theorem** gives a general expression
+for the time evolution of an observable's expectation value $$\expval{\hat{L}}$$.
+Recall the time-dependent Schrödinger equation,
where prime denotes differentiation with respect to time $$t$$:
$$\begin{aligned}
\Ket{\psi'} = \frac{1}{i \hbar} \hat{H} \Ket{\psi}
- \qquad
+ \qquad \qquad
\Bra{\psi'} = - \frac{1}{i \hbar} \Bra{\psi} \hat{H}
\end{aligned}$$
Given an observable operator $$\hat{L}$$ and a state $$\Ket{\psi}$$,
-the time-derivative of the expectation value $$\expval{\hat{L}}$$ is as follows
+the $$t$$-derivative of the expectation value $$\expval{\hat{L}}$$ is as follows
(due to the product rule of differentiation):
$$\begin{aligned}
@@ -43,28 +42,26 @@ $$\begin{aligned}
}
\end{aligned}$$
-In practice, since most operators are time-independent,
-the last term often vanishes.
-
-As a interesting side note, in the [Heisenberg picture](/know/concept/heisenberg-picture/),
-this relation proves itself,
-when one simply wraps all terms in $$\Bra{\psi}$$ and $$\Ket{\psi}$$.
+In practice, since most operators are time-independent, the last term often vanishes.
+Note that this relation is trivial to prove
+in the [Heisenberg picture](/know/concept/heisenberg-picture/),
+by wrapping all terms in $$\Bra{\psi}$$ and $$\Ket{\psi}$$.
-Two observables of particular interest are the position $$\hat{X}$$ and momentum $$\hat{P}$$.
-Applying the above theorem to $$\hat{X}$$ yields the following,
-which we reduce using the fact that $$\hat{X}$$ commutes
-with the potential $$V(\hat{X})$$,
-because one is a function of the other:
+Two observables of particular interest
+are position $$\hat{X}$$ and momentum $$\hat{P}$$.
+Applying the theorem to $$\hat{X}$$ yields the following,
+using $$\hat{H} = \hat{P}^2 / (2 m) + V(\hat{X})$$
+and a few basic properties of commutators:
$$\begin{aligned}
\dv{\expval{\hat{X}}}{t}
&= \frac{1}{i \hbar} \Expval{[\hat{X}, \hat{H}]}
- = \frac{1}{2 i \hbar m} \Expval{[\hat{X}, \hat{P}^2] + 2 m [\hat{X}, V(\hat{X})]}
- = \frac{1}{2 i \hbar m} \Expval{[\hat{X}, \hat{P}^2]}
+ \\
+ &= \frac{1}{2 i \hbar m} \Expval{[\hat{X}, \hat{P}^2] + 2 m [\hat{X}, V(\hat{X})]}
\\
&= \frac{1}{2 i \hbar m} \Expval{\hat{P} [\hat{X}, \hat{P}] + [\hat{X}, \hat{P}] \hat{P}}
- = \frac{2 i \hbar}{2 i \hbar m} \expval{\hat{P}}
- = \frac{\expval{\hat{P}}}{m}
+ \\
+ &= \frac{2 i \hbar}{2 i \hbar m} \expval{\hat{P}}
\end{aligned}$$
This is the first part of the "original" form of Ehrenfest's theorem,
@@ -72,7 +69,8 @@ which is reminiscent of classical Newtonian mechanics:
$$\begin{gathered}
\boxed{
- \dv{\expval{\hat{X}}}{t} = \frac{\expval{\hat{P}}}{m}
+ \dv{\expval{\hat{X}}}{t}
+ = \frac{\expval{\hat{P}}}{m}
}
\end{gathered}$$
@@ -82,33 +80,32 @@ gives us:
$$\begin{aligned}
\dv{\expval{\hat{P}}}{t}
&= \frac{1}{i \hbar} \Expval{[\hat{P}, \hat{H}]}
- = \frac{1}{2 i \hbar m} \Expval{[\hat{P}, \hat{P}^2] + 2 m [\hat{P}, V(\hat{X})]}
- = \frac{1}{i \hbar} \Expval{[\hat{P}, V(\hat{X})]}
+ \\
+ &= \frac{1}{2 i \hbar m} \Expval{[\hat{P}, \hat{P}^2] + 2 m [\hat{P}, V(\hat{X})]}
+ \\
+ &= \frac{1}{i \hbar} \Expval{[\hat{P}, V(\hat{X})]}
\end{aligned}$$
-To find the commutator, we go to the $$\hat{X}$$-basis and use a test
-function $$f(x)$$:
+To evaluate the commutator,
+we go to the $$\hat{X}$$-basis and use a test function $$f(x)$$:
$$\begin{aligned}
\Comm{- i \hbar \dv{}{x}}{V(x)} \: f(x)
+ &= - i \hbar \dv{}{x} \Big( V(x) \: f(x) \Big) - V(x) \Big( \!-\! i \hbar \dv{}{x} \Big) f(x)
+ \\
&= - i \hbar \frac{dV}{dx} f(x) - i \hbar V(x) \frac{df}{dx} + i \hbar V(x) \frac{df}{dx}
- = - i \hbar \frac{dV}{dx} f(x)
-\end{aligned}$$
-
-By inserting this result back into the previous equation, we find the following:
-
-$$\begin{aligned}
- \dv{\expval{\hat{P}}}{t}
- &= - \frac{i \hbar}{i \hbar} \Expval{\frac{d V}{d \hat{X}}}
- = - \Expval{\frac{d V}{d \hat{X}}}
+ \\
+ &= - i \hbar \frac{dV}{dx} f(x)
\end{aligned}$$
-This is the second part of Ehrenfest's theorem,
-which is also similar to Newtonian mechanics:
+By inserting this result back into the previous equation,
+we find the second part of Ehrenfest's original theorem,
+which is again reminiscent Newtonian mechanics:
$$\begin{gathered}
\boxed{
- \dv{\expval{\hat{P}}}{t} = - \Expval{\pdv{V}{\hat{X}}}
+ \dv{\expval{\hat{P}}}{t}
+ = - \Expval{\pdv{V}{\hat{X}}}
}
\end{gathered}$$
@@ -121,7 +118,7 @@ $$\begin{gathered}
\Expval{\pdv{\hat{H}}{\hat{P}}}
= \dv{\expval{\hat{X}}}{t}
}
- \qquad \quad
+ \qquad \qquad
\boxed{
- \Expval{\pdv{\hat{H}}{\hat{X}}}
= \dv{\expval{\hat{P}}}{t}
diff --git a/source/know/concept/ficks-laws/index.md b/source/know/concept/ficks-laws/index.md
index 8d5da7d..20bc50b 100644
--- a/source/know/concept/ficks-laws/index.md
+++ b/source/know/concept/ficks-laws/index.md
@@ -21,10 +21,12 @@ as opposed to **non-Fickian** or **anomalous diffusion**.
moves from regions of high concentration to regions of lower concentration,
at a rate proportional to the difference in concentration.
-Let $$\vec{J}$$ be the **diffusion flux** (with unit $$\mathrm{m}^{-2} \mathrm{s}^{-1}$$),
+Let $$\vec{J}$$ be the **diffusion flux**
+(with unit $$\mathrm{m}^{-2} \mathrm{s}^{-1}$$),
whose magnitude and direction describes the "flow" of diffusing matter.
Formally, Fick's first law predicts that the flux
-is proportional to the gradient of the concentration $$C$$ (with unit $$\mathrm{m}^{-3}$$):
+is proportional to the gradient of the concentration $$C(\vec{r})$$
+(with unit $$\mathrm{m}^{-3}$$):
$$\begin{aligned}
\boxed{
@@ -37,12 +39,9 @@ Where $$D$$ (with unit $$\mathrm{m}^{2}/\mathrm{s}$$)
is known as the **diffusion coefficient** or **diffusivity**,
and depends on both the medium and the diffusing substance.
-Fick's first law is a general physical principle,
-which was discovered experimentally,
-and thus does not have a general derivation.
-Proofs for specific systems do exist,
-but they say more about those systems
-than about diffusion in general.
+Fick's first law is an empirical physical principle,
+and therefore does not have a general derivation,
+although proofs for specific systems do exist.
@@ -59,12 +58,12 @@ $$\begin{aligned}
\end{aligned}$$
Over time $$t$$, matter enters/leaves $$V$$.
-Let $$S$$ be the surface of $$V$$, and $$\vec{J}$$ the diffusion flux,
-then $$M$$ changes as follows, to which we apply the divergence theorem:
+Let $$\partial V$$ be the surface of $$V$$, and $$\vec{J}$$ the diffusion flux,
+then $$M$$ changes as follows, applying the divergence theorem:
$$\begin{aligned}
\dv{M}{t}
- = - \int_S \vec{J} \cdot \dd{\vec{S}}
+ = - \int_{\partial V} \vec{J} \cdot \dd{\vec{S}}
= - \int_V \nabla \cdot \vec{J} \dd{V}
\end{aligned}$$
@@ -91,7 +90,7 @@ the general form of Fick's second law:
$$\begin{aligned}
\boxed{
\pdv{C}{t}
- = \nabla \cdot \Big( D \: \nabla C \Big)
+ = \nabla \cdot \Big( D \, \nabla C \Big)
}
\end{aligned}$$
@@ -100,7 +99,8 @@ with respect to space $$\vec{r}$$ and concentration $$C$$,
in which case Fick's second law reduces to:
$$\begin{aligned}
- \pdv{C}{t} = D \: \nabla^2 C
+ \pdv{C}{t}
+ = D \, \nabla^2 C
\end{aligned}$$
@@ -108,7 +108,7 @@ $$\begin{aligned}
## Fundamental solution
Fick's second law has exact solutions for many situations,
-but the most important one is arguably the **fundamental solution**.
+but the most important one is arguably the **fundamental solution** $$H$$.
Consider a 1D system (for simplicity) with constant diffusivity $$D$$,
where the initial concentration $$C(x, 0)$$ is
a [Dirac delta function](/know/concept/dirac-delta-function/):
@@ -118,8 +118,8 @@ $$\begin{aligned}
= \delta(x - x_0)
\end{aligned}$$
-By solving Fick's second law with this initial condition,
-$$C$$'s time evolution turns out to be:
+By solving Fick's second law with this initial condition (details omitted),
+we find that $$C$$ obeys:
$$\begin{aligned}
H(x - x_0, t)
@@ -127,13 +127,12 @@ $$\begin{aligned}
= \frac{1}{\sqrt{4 \pi D t}} \exp\!\Big( \!-\!\frac{(x - x_0)^2}{4 D t} \Big)
\end{aligned}$$
-This result is a normalized Gaussian,
-as a consequence of
-the [central limit theorem](/know/concept/central-limit-theorem/):
-the diffusion behaviour is a sum of many independent steps
-(i.e. molecular collisions).
+This result is a normalized Gaussian:
+diffusion is a sum of many independent molecular collisions,
+so the [central limit theorem](/know/concept/central-limit-theorem/) applies,
+hence this result.
The standard deviation is $$\sqrt{2 D t}$$,
-meaning that the distance of a diffusion is proportional to $$\sqrt{t}$$.
+meaning that the expected distance of a diffusion is proportional to $$\sqrt{t}$$.
This solution $$H$$ is extremely useful,
because any initial concentration $$C(x, 0)$$ can be written as
@@ -146,22 +145,19 @@ $$\begin{aligned}
\end{aligned}$$
In other words, any function is a linear combination of delta functions.
-Fick's second law is linear,
-so the overall solution $$C(x, t)$$ is the same combination of fundamental solutions $$H$$:
+Fick's second law is linear, so the overall solution $$C(x, t)$$
+is the same combination of fundamental solutions $$H$$:
$$\begin{aligned}
C(x, t)
= (C * H)(x)
&= \int_{-\infty}^\infty C(x_0, 0) \: H(x - x_0, t) \dd{x_0}
- \\
- &= \int_{-\infty}^\infty \frac{1}{\sqrt{4 \pi D t}} \exp\!\Big( \!-\!\frac{(x - x_0)^2}{4 D t} \Big) \: C(x_0, 0) \dd{x_0}
\end{aligned}$$
This technique is analogous to using
the [impulse response](/know/concept/impulse-response/)
-of a linear operator to extrapolate all its inhomogeneous solutions.
-The difference is that here, we used the initial condition
-instead of the forcing function.
+of a linear operator to extrapolate all its inhomogeneous solutions,
+but here we used the initial condition instead of the forcing function.
diff --git a/source/know/concept/grad-shafranov-equation/index.md b/source/know/concept/grad-shafranov-equation/index.md
index b86c032..c9104d2 100644
--- a/source/know/concept/grad-shafranov-equation/index.md
+++ b/source/know/concept/grad-shafranov-equation/index.md
@@ -36,9 +36,9 @@ $$\begin{aligned}
= 0
\end{aligned}$$
-Notice that $$\vb{E} = 0$$ is a result of the ideal generalized Ohm's law.
-Under these assumptions, the relevant MHD equations to be solved are
-Gauss' law for magnetism, Ampère's law, and the MHD momentum equation, respectively:
+Notice that $$\vb{E} = 0$$ is a result of ideal MHD's generalized Ohm's law.
+Under these assumptions, the relevant equations to be solved are
+Gauss' law for magnetism, Ampère's law, and the momentum equation of MHD, respectively:
$$\begin{aligned}
0
@@ -51,11 +51,12 @@ $$\begin{aligned}
= \vb{J} \cross \vb{B}
\end{aligned}$$
-The goal is to analyze them in this order,
+The idea is to analyze them in this order,
exploiting toroidal symmetry along the way,
to arrive at a general equilibrium condition.
-[Cylindrical polar coordinates](/know/concept/cylindrical-polar-coordinates/) $$(r, \theta, z)$$
-are a natural choice, with the $$z$$-axis running through the middle of the torus.
+[Cylindrical polar coordinates](/know/concept/cylindrical-polar-coordinates/)
+$$(r, \theta, z)$$ are a natural choice,
+with the $$z$$-axis running through the middle of the torus.
As preparation, it is a good idea to write $$\vb{B}$$
as the curl of a magnetic vector potential $$\vb{A}$$,
diff --git a/source/know/concept/holomorphic-function/index.md b/source/know/concept/holomorphic-function/index.md
index 976758b..db3bdfb 100644
--- a/source/know/concept/holomorphic-function/index.md
+++ b/source/know/concept/holomorphic-function/index.md
@@ -28,7 +28,8 @@ $$\begin{aligned}
}
\end{aligned}$$
-We decompose $$f$$ into the real functions $$u$$ and $$v$$ of real variables $$x$$ and $$y$$:
+We decompose $$f$$ into the real functions $$u$$ and $$v$$
+of real variables $$x$$ and $$y$$:
$$\begin{aligned}
f(z)
@@ -36,7 +37,8 @@ $$\begin{aligned}
= u(x, y) + i v(x, y)
\end{aligned}$$
-Since we are free to choose the direction of $$\Delta z$$, we choose $$\Delta x$$ and $$\Delta y$$:
+Since we are free to choose the direction of $$\Delta z$$,
+we choose $$\Delta x$$ and $$\Delta y$$:
$$\begin{aligned}
f'(z)
@@ -53,9 +55,13 @@ we thus arrive at the **Cauchy-Riemann equations**:
$$\begin{aligned}
\boxed{
- \pdv{u}{x} = \pdv{v}{y}
- \qquad
- \pdv{v}{x} = - \pdv{u}{y}
+ \begin{aligned}
+ \pdv{u}{x}
+ &= \pdv{v}{y}
+ \\
+ \pdv{v}{x}
+ &= - \pdv{u}{y}
+ \end{aligned}
}
\end{aligned}$$
@@ -85,7 +91,8 @@ Just like before, we decompose $$f(z)$$ into its real and imaginary parts:
$$\begin{aligned}
\oint_C f(z) \dd{z}
&= \oint_C (u + i v) \dd{(x + i y)}
- = \oint_C (u + i v) \:(\dd{x} + i \dd{y})
+ \\
+ &= \oint_C (u + i v) \:(\dd{x} + i \dd{y})
\\
&= \oint_C u \dd{x} - v \dd{y} + i \oint_C v \dd{x} + u \dd{y}
\end{aligned}$$
@@ -137,10 +144,10 @@ $$\begin{aligned}
{% include proof/end.html id="proof-int-formula" %}
-Similarly, **Cauchy's differentiation formula**,
-or **Cauchy's integral formula for derivatives**
-gives all derivatives of a holomorphic function as follows,
-and also guarantees their existence:
+Similarly, **Cauchy's differentiation formula**
+or **integral formula for derivatives**
+gives the $$n$$th-order derivative of a holomorphic function as follows,
+and guarantees its existence:
$$\begin{aligned}
\boxed{
diff --git a/source/know/concept/larmor-precession/index.md b/source/know/concept/larmor-precession/index.md
index 601dae7..e29432b 100644
--- a/source/know/concept/larmor-precession/index.md
+++ b/source/know/concept/larmor-precession/index.md
@@ -11,28 +11,29 @@ layout: "concept"
Consider a stationary spin-1/2 particle,
placed in a [magnetic field](/know/concept/magnetic-field/)
with magnitude $$B$$ pointing in the $$z$$-direction.
-In that case, its Hamiltonian $$\hat{H}$$ is given by:
+In that case, the Hamiltonian $$\hat{H}$$ is given by:
$$\begin{aligned}
\hat{H} = - \gamma B \hat{S}_z = - \frac{\hbar}{2} \gamma B \hat{\sigma_z}
\end{aligned}$$
-Where $$\gamma = - q / m$$ is the gyromagnetic ratio,
+Where $$\gamma = q g / (2 m)$$ is the so-called *gyromagnetic ratio*
+for a particle with charge $$q$$, mass $$m$$,
+and a system-dependent *$$g$$-factor* (for electrons $$g \approx 2$$),
and $$\hat{\sigma}_z$$ is the Pauli spin matrix for the $$z$$-direction.
-Since $$\hat{H}$$ is proportional to $$\hat{\sigma}_z$$,
-they share eigenstates $$\Ket{\downarrow}$$ and $$\Ket{\uparrow}$$.
-The respective eigenenergies $$E_{\downarrow}$$ and $$E_{\uparrow}$$ are as follows:
+Because $$\hat{H}$$ is proportional to $$\hat{\sigma}_z$$,
+they share eigenstates $$\Ket{\downarrow}$$ and $$\Ket{\uparrow}$$,
+so the respective eigenenergies $$E_{\downarrow}$$ and $$E_{\uparrow}$$ are as follows:
$$\begin{aligned}
E_{\downarrow} = \frac{\hbar}{2} \gamma B
- \qquad
+ \qquad \qquad
E_{\uparrow} = - \frac{\hbar}{2} \gamma B
\end{aligned}$$
Because $$\hat{H}$$ is time-independent,
the general time-dependent solution $$\Ket{\chi(t)}$$ is of the following form,
-where $$a$$ and $$b$$ are constants,
-and the exponentials are "twiddle factors":
+where $$a$$ and $$b$$ are constants:
$$\begin{aligned}
\Ket{\chi(t)}
@@ -72,7 +73,7 @@ $$\begin{aligned}
\\
&= \frac{\hbar}{2} \cos(\theta/2) \sin(\theta/2) \Big( e^{i \gamma B t} + e^{- i \gamma B t} \Big)
\\
- &= \frac{\hbar}{2} \cos(\gamma B t) \cdot 2 \cos(\theta/2) \sin(\theta/2)
+ &= \frac{\hbar}{2} \cos(\theta/2) \sin(\theta/2) \cdot 2 \cos(\gamma B t)
\\
&= \frac{\hbar}{2} \sin(\theta) \cos(\gamma B t)
\end{aligned}$$
@@ -82,12 +83,13 @@ with the following results:
$$\begin{aligned}
\matrixel{\chi}{\hat{S}_y}{\chi} = - \frac{\hbar}{2} \sin(\theta) \sin(\gamma B t)
- \qquad
+ \qquad \qquad
\matrixel{\chi}{\hat{S}_z}{\chi} = \frac{\hbar}{2} \cos(\theta)
\end{aligned}$$
-The result is that the spin axis is off by $$\theta$$ from the $$z$$-direction,
-and is rotating (or **precessing**) around the $$z$$-axis at the **Larmor frequency** $$\omega$$:
+The result is that, if the spin axis is off by $$\theta$$ from the $$z$$-direction,
+then it rotates (or **precesses**) around the $$z$$-axis
+at the **Larmor frequency** $$\omega$$:
$$\begin{aligned}
\boxed{
diff --git a/source/know/concept/lubrication-theory/index.md b/source/know/concept/lubrication-theory/index.md
index 4015526..54200d3 100644
--- a/source/know/concept/lubrication-theory/index.md
+++ b/source/know/concept/lubrication-theory/index.md
@@ -9,8 +9,7 @@ categories:
layout: "concept"
---
-**Lubricants** are widely used
-to reduce friction between two moving surfaces.
+**Lubricants** are widely used to reduce friction between two moving surfaces.
In fluid mechanics, **lubrication theory**
is the study of fluids that are tightly constrained in one dimension,
especially those in small gaps between moving surfaces.
@@ -34,32 +33,32 @@ $$\begin{aligned}
\approx \frac{d^2}{L^2} \mathrm{Re}
\end{aligned}$$
-If $$d$$ is small enough compared to $$L$$,
-then $$\mathrm{Re}_\mathrm{gap} \ll 1$$.
+If $$d$$ is small enough compared to $$L$$, then $$\mathrm{Re}_\mathrm{gap} \ll 1$$.
More formally, we need $$d \ll L / \sqrt{\mathrm{Re}}$$,
so we are inside the boundary layer,
in the realm of the [Prandtl equations](/know/concept/prandtl-equations/).
Let $$\mathrm{Re}_\mathrm{gap} \ll 1$$.
-We are thus dealing with *Stokes flow*, in which case
+We are then dealing with *Stokes flow*, in which case
the [Navier-Stokes equations](/know/concept/navier-stokes/equations/)
can be reduced to the following *Stokes equations*:
$$\begin{aligned}
\pdv{p}{x}
= \eta \: \Big( \pdvn{2}{v_x}{x} + \pdvn{2}{v_x}{y} \Big)
- \qquad \quad
+ \qquad \qquad
\pdv{p}{y}
= \eta \: \Big( \pdvn{2}{v_y}{x} + \pdvn{2}{v_y}{y} \Big)
\end{aligned}$$
-Let the $$y = 0$$ plane be an infinite flat surface,
+Let the $$y = 0$$ plane be an infinite flat surface
+(a good approximation because $$d \ll L$$),
sliding in the positive $$x$$-direction at a constant velocity $$U$$.
-On the other side of the gap,
-an arbitrary surface is described by $$h(x)$$.
+On the other side of the gap, an arbitrary surface
+is described by a height function $$h(x)$$.
Since the gap is so narrow,
-and the surfaces' movements cause large shear stresses inside,
+and the surfaces' movements cause large shear stresses inside it,
$$v_y$$ is negligible compared to $$v_x$$.
Furthermore, because the gap is so long,
we assume that $$\ipdv{v_x}{x}$$ is negligible compared to $$\ipdv{v_x}{y}$$.
@@ -68,7 +67,7 @@ This reduces the Stokes equations to:
$$\begin{aligned}
\pdv{p}{x}
= \eta \pdvn{2}{v_x}{y}
- \qquad \quad
+ \qquad \qquad
\pdv{p}{y}
= 0
\end{aligned}$$
@@ -92,18 +91,20 @@ $$\begin{aligned}
\end{aligned}$$
The moving bottom surface drags fluid in the $$x$$-direction
-at a volumetric rate $$Q$$, given by:
+at a volumetric rate $$Q(x)$$, given by:
$$\begin{aligned}
- Q
- = \int_0^{h(x)} v_x(x, y) \dd{y}
- = \bigg[ \frac{p'}{6 \eta} y^3 - \frac{p'}{4 \eta} h y^2 - \frac{U}{2 h} y^2 + U y \bigg]_0^{h}
- = - \frac{p'}{12 \eta} h^3 + \frac{U}{2} h
+ Q(x)
+ &= \int_0^{h(x)} v_x(x, y) \dd{y}
+ \\
+ &= \bigg[ \frac{p'}{6 \eta} y^3 - \frac{p'}{4 \eta} h y^2 - \frac{U}{2 h} y^2 + U y \bigg]_0^{h}
+ \\
+ &= - \frac{p'}{12 \eta} h^3(x) + \frac{U}{2} h(x)
\end{aligned}$$
-Assuming that the lubricant is incompressible,
-meaning that the same volume of fluid must be leaving a point as is entering it.
-In other words, $$Q$$ is independent of $$x$$,
+Let us assume that the lubricant is incompressible,
+meaning that the same volume of fluid must be both leaving and entering the gap.
+In that case, $$Q$$ is independent of $$x$$,
which allows us to write $$p'(x)$$ in terms of
measurable constants and the known function $$h(x)$$:
@@ -139,7 +140,8 @@ $$\begin{aligned}
= - 2 h' \frac{U h - 3 Q}{h^4} \big( 2 h y - 3 y^2 \big)
\end{aligned}$$
-Integrating with respect to $$y$$ thus leads to the following transverse velocity $$v_y$$:
+Integrating with respect to $$y$$ therefore leads to
+the following transverse velocity $$v_y$$:
$$\begin{aligned}
\boxed{
@@ -148,10 +150,11 @@ $$\begin{aligned}
}
\end{aligned}$$
-Typically, the lubricant is not in a preexisting pressure differential,
-i.e it is not getting pumped through the system.
-Although the pressure gradient $$p'$$ need not be zero,
-we therefore expect that its integral vanishes:
+Usually, the lubricant is not getting pumped through the system.
+In that case, although the pressure gradient $$p'$$ need not be zero in all points
+(i.e. there may be complex dynamics inside the gap),
+we do expect that its integral across the gap vanishes
+(because both sides are at the same pressure):
$$\begin{aligned}
0
@@ -164,7 +167,7 @@ Isolating this for $$Q$$, and defining $$q$$ as below, yields a simple equation:
$$\begin{aligned}
Q
= \frac{1}{2} U q
- \qquad \quad
+ \qquad \qquad
q
\equiv \frac{\int_L h^{-2} \dd{x}}{\int_L h^{-3} \dd{x}}
\end{aligned}$$
@@ -178,27 +181,25 @@ $$\begin{aligned}
&= U \Big( 1 - \frac{y}{h} \Big) \Big( 1 - \frac{3 y (h - q)}{h^2} \Big)
\end{aligned}$$
-The first factor is always positive,
-but the second can be negative,
-if for some $$y$$-values:
+The first factors are always positive, but the last one can be negative,
+if any $$y$$-values satisfy:
$$\begin{aligned}
h^2 < 3 y (h - q)
- \quad \implies \quad
+ \qquad \implies \qquad
y > \frac{h^2}{3 (h - q)}
\end{aligned}$$
-Since $$h > y$$, such $$y$$-values will only exist
+Since $$h \le y$$, such $$y$$-values will only exist
if $$h$$ is larger than some threshold:
$$\begin{aligned}
3 (h - q) > h
- \quad \implies \quad
+ \qquad \implies \qquad
h > \frac{3}{2} q
\end{aligned}$$
-If this condition is satisfied,
-there will be some flow reversal:
+If this condition is satisfied, there will be some flow reversal:
rather than just getting dragged by the shearing motion,
the lubricant instead "rolls" inside the gap.
This is confirmed by $$v_y$$:
diff --git a/source/know/concept/lyddane-sachs-teller-relation/index.md b/source/know/concept/lyddane-sachs-teller-relation/index.md
index 9cec9dc..60c8984 100644
--- a/source/know/concept/lyddane-sachs-teller-relation/index.md
+++ b/source/know/concept/lyddane-sachs-teller-relation/index.md
@@ -20,7 +20,7 @@ creating lattice vibrations (phonons),
i.e. a photon-phonon conversion,
where the total energy and momentum must be conserved.
If the photon has frequency $$\omega$$ and wavenumber $$k$$,
-and the phonon $$\Omega$$ and $$K$$, then:
+and the phonon has $$\Omega$$ and $$K$$, then:
$$\begin{aligned}
\hbar \omega
@@ -71,8 +71,8 @@ $$\begin{aligned}
Where $$\vb{E}(t) = \vb{E}_0 e^{- i \omega t}$$ represents the light,
and $$\kappa$$ is the spring constant of the polar bonds' restoring force.
-Note that the latter depends on the displacement between the ions,
-instead of from their equilibrium position,
+The latter depends on the displacement between the ions,
+instead of their displacement from their equilibrium position,
so we need to write $$\vb{x}_{+} - \vb{x}_{-}$$ instead of $$\vb{x}_{+}$$.
Respectively dividing the equations by $$m_{+}$$ and $$m_{-}$$
@@ -95,10 +95,10 @@ $$\begin{aligned}
\end{aligned}$$
Note that $$\Omega_\mathrm{TO}$$ is the phonon frequency for $$K = 0$$.
-This is because IR light waves are much larger than the crystal's unit cell,
-so we are ignoring all spatial variation in $$\vb{E}$$
-(i.e. the [electric dipole approximation](/know/concept/electric-dipole-approximation/)).
-This is equivalent to assuming that $$K \approx 0$$.
+This is close enough, because IR light waves are much larger
+than the crystal's unit cell, so we can ignore all spatial variation in $$\vb{E}$$
+(the [electric dipole approximation](/know/concept/electric-dipole-approximation/)),
+which is equivalent to assuming that $$K = 0$$.
For the sake of generality,
we also introduce an empirical damping rate $$\gamma$$,
@@ -147,7 +147,9 @@ $$\begin{aligned}
\end{aligned}$$
In the limits of low and high frequencies $$\omega$$,
-we see that $$\varepsilon_r$$ is higher in the former:
+we see that $$\varepsilon_r$$ is higher in the former
+(also recall that $$\chi_\mathrm{low} > \chi_\mathrm{high}$$
+according to the original Lorentz oscillator model):
$$\begin{aligned}
\varepsilon_{\mathrm{low}}
@@ -159,7 +161,8 @@ $$\begin{aligned}
= 1 + \chi_\mathrm{high}
\end{aligned}$$
-We can use these quantities to rewrite the relative permittivity $$\varepsilon_r$$ as follows:
+We can use these quantities to rewrite
+the relative permittivity $$\varepsilon_r$$ as follows:
$$\begin{aligned}
\varepsilon_r(\omega)
@@ -167,9 +170,8 @@ $$\begin{aligned}
\frac{\Omega_\mathrm{TO}^2}{\Omega_\mathrm{TO}^2 - \omega^2 - i \gamma \omega}
\end{aligned}$$
-For weak damping $$\gamma \approx 0$$, there exists a frequency,
-which we will call $$\Omega_\mathrm{LO}$$ in anticipation,
-where the dielectric function is zero:
+For weak damping $$\gamma \approx 0$$, there exists a frequency
+with zero permittivity, which we call $$\Omega_\mathrm{LO}$$:
$$\begin{aligned}
0
@@ -179,8 +181,8 @@ $$\begin{aligned}
\end{aligned}$$
The physical significance of $$\varepsilon_r = 0$$ can be
-seen from [Gauss' law](/know/concept/maxwells-equations), under the assumption that there is
-no net charge density:
+seen from [Gauss' law](/know/concept/maxwells-equations),
+under the assumption that there is no net charge density:
$$\begin{aligned}
\nabla \cdot \vb{D}
@@ -188,10 +190,10 @@ $$\begin{aligned}
= 0
\end{aligned}$$
-If $$\varepsilon_r \neq 0$$, then $$\nabla \cdot \vec{E} = 0$$,
+If $$\varepsilon_r \neq 0$$, then $$\nabla \cdot \vb{E} = 0$$,
corresponding to a transverse light wave as usual.
-However, if $$\varepsilon_r = 0$$, then $$\nabla \cdot \vec{E} \neq 0$$,
-representing a longitudinal electric wave, like a plasmon in metal.
+However, if $$\varepsilon_r = 0$$, then $$\nabla \cdot \vb{E} \neq 0$$,
+representing a longitudinal electric wave, analogous to plasmons in metals.
Rearranging the equation for $$\Omega_\mathrm{LO}$$
gives us the **Lyddane-Sachs-Teller (LST) relation**:
@@ -230,17 +232,18 @@ In practice, real materials have $$\gamma > 0$$, which reduces $$R$$ somewhat.
Because the photons and TO phonons interact so strongly
for $$\omega \approx \Omega_\mathrm{TO}$$,
they can be treated as a single **phonon polariton** there,
-with a dispersion relation given by:
+with a self-referential dispersion relation given by:
$$\begin{aligned}
\omega_\mathrm{pp}(K)
- = \frac{c}{\sqrt{\varepsilon_r(\omega_\mathrm{pp})}} K
+ = \frac{c}{\sqrt{\varepsilon_r(\omega_\mathrm{pp}(K))}} K
\end{aligned}$$
Earlier, when treating the photon and phonon separately,
we wanted the intersection between $$\omega(k)$$ and $$\Omega(K)$$.
-But now, for $$\omega_\mathrm{pp}(K)$$, there is none! This is a good example
-of the typical *anti-crossing* behavior of strongly coupled systems.
+But now, plotting $$\omega_\mathrm{pp}(K)$$ reveals that there is no intersection!
+This is a good example of the typical *anti-crossing*
+behavior of strongly coupled quantum systems.
diff --git a/source/know/concept/prandtl-equations/index.md b/source/know/concept/prandtl-equations/index.md
index d82657c..8f5c4d0 100644
--- a/source/know/concept/prandtl-equations/index.md
+++ b/source/know/concept/prandtl-equations/index.md
@@ -11,13 +11,12 @@ layout: "concept"
In fluid dynamics, the **Prandtl equations** or **boundary layer equations**
describe the movement of a [viscous](/know/concept/viscosity/) fluid
-with a large [Reynolds number](/know/concept/reynolds-number/) $$\mathrm{Re} \gg 1$$
-close to a solid surface.
+with a large [Reynolds number](/know/concept/reynolds-number/)
+$$\mathrm{Re} \gg 1$$ close to a solid surface.
-Fluids with a large Reynolds number
-are often approximated as having zero viscosity,
-since the simpler [Euler equations](/know/concept/euler-equations)
-can then be used instead of the [Navier-Stokes equations](/know/concept/navier-stokes-equations/).
+Fluids with a large Reynolds number are often approximated as having zero viscosity,
+since the simpler [Euler equations](/know/concept/euler-equations) can then be used
+instead of the [Navier-Stokes equations](/know/concept/navier-stokes-equations/).
However, in reality, a viscous fluid obeys the *no-slip* boundary condition:
at every solid surface the local velocity must be zero.
@@ -29,9 +28,9 @@ This is in contrast to the ideal flow far away from the surface.
We consider a simple theoretical case in 2D:
a large flat surface located at $$y = 0$$ for all $$x \in \mathbb{R}$$,
with a fluid *trying* to flow parallel to it at $$U$$.
-The 2D treatment can be justified by assuming that everything is constant in the $$z$$-direction.
-We will not solve this case,
-but instead derive general equations
+The 2D treatment can be justified by assuming
+that everything is constant in the $$z$$-direction.
+We will not solve this case, but instead derive general equations
to describe the flow close to a flat surface.
At the wall, there is a very thin boundary layer of thickness $$\delta$$,
@@ -39,8 +38,7 @@ where the fluid is assumed to be completely stationary $$\va{v} = 0$$.
We are mainly interested in the region $$\delta < y \ll L$$,
where $$L$$ is the distance at which the fluid becomes practically ideal.
This the so-called **slip-flow** region,
-in which the fluid is not stationary,
-but still viscosity-dominated.
+in which the fluid is not stationary, but still viscosity-dominated.
In 2D, the steady Navier-Stokes equations are as follows,
where the flow $$\va{v} = (v_x, v_y)$$:
@@ -66,13 +64,13 @@ Let $$\tilde{x}$$ and $$\tilde{y}$$ be dimenionless variables of order $$1$$:
$$\begin{aligned}
x
= L \tilde{x}
- \qquad \quad
+ \qquad \qquad
y
= \delta \tilde{x}
- \qquad \quad
+ \qquad \qquad
\pdv{}{x}
= \frac{1}{L} \pdv{}{\tilde{x}}
- \qquad \quad
+ \qquad \qquad
\pdv{}{y}
= \frac{1}{\delta} \pdv{}{\tilde{y}}
\end{aligned}$$
@@ -85,10 +83,10 @@ by [Bernoulli's theorem](/know/concept/bernoullis-theorem/):
$$\begin{aligned}
v_x
= U \tilde{v}_x
- \qquad \quad
+ \qquad \qquad
v_y
= \frac{U \delta}{L} \tilde{v}_y
- \qquad \quad
+ \qquad \qquad
p
= \rho U^2 \tilde{p}
\end{aligned}$$
@@ -124,15 +122,15 @@ and that faster velocities $$U$$ give thinner layers.
Furthermore, we expect *downstream thickening*:
with distance $$x$$, viscous stresses slow down the slip-flow,
leading to a gradual increase of $$\delta(x)$$.
-Some dimensional analysis thus yields the following estimate:
+Some dimensional analysis yields the following estimate:
$$\begin{aligned}
\delta
\approx \sqrt{\frac{\nu x}{U}}
- \sim \sqrt{\frac{\nu L}{U}}
+ \approx \sqrt{\frac{\nu L}{U}}
\end{aligned}$$
-We thus insert $$\delta = \sqrt{\nu L / U}$$ into the Navier-Stokes equations, giving us:
+So we insert $$\delta = \sqrt{\nu L / U}$$ into the Navier-Stokes equations, giving us:
$$\begin{aligned}
\tilde{v}_x \pdv{\tilde{v}_x}{\tilde{x}} + \tilde{v}_y \pdv{\tilde{v}_x}{\tilde{y}}
@@ -163,15 +161,14 @@ so we can drop many terms, leaving us with these redimensionalized equations:
$$\begin{aligned}
v_x \pdv{v_x}{x} + v_y \pdv{v_x}{y}
= - \frac{1}{\rho} \pdv{p}{x} + \nu \pdvn{2}{v_x}{y}
- \qquad \quad
+ \qquad \qquad
\pdv{p}{y}
= 0
\end{aligned}$$
The second one tells us that for a given $$x$$-value,
-the pressure is the same at the surface
-as in the main flow $$y > L$$, where the fluid is ideal.
-In the latter regime, we apply Bernoulli's theorem to rewrite $$p$$,
+the pressure is the same at the surface as in the ideal main flow $$y > L$$.
+In the latter regime, we can use Bernoulli's theorem to rewrite $$p$$,
using the *Bernoulli head* $$H$$ and the mainstream velocity $$U(x)$$:
$$\begin{aligned}
@@ -185,18 +182,19 @@ we arrive at the Prandtl equations:
$$\begin{aligned}
\boxed{
- v_x \pdv{v_x}{x} + v_y \pdv{v_x}{y}
- = U \dv{U}{x} + \nu \pdvn{2}{v_x}{y}
- \qquad \quad
- \pdv{v_x}{x} + \pdv{v_y}{y}
- = 0
+ \begin{aligned}
+ v_x \pdv{v_x}{x} + v_y \pdv{v_x}{y}
+ &= U \dv{U}{x} + \nu \pdvn{2}{v_x}{y}
+ \\
+ \pdv{v_x}{x} + \pdv{v_y}{y}
+ &= 0
+ \end{aligned}
}
\end{aligned}$$
A notable application of these equations is
the [Blasius boundary layer](/know/concept/blasius-boundary-layer/),
-where the surface in question
-is a semi-infinite plane.
+where the surface in question is a semi-infinite plane.
diff --git a/source/know/concept/probability-current/index.md b/source/know/concept/probability-current/index.md
index bd41dab..81ca586 100644
--- a/source/know/concept/probability-current/index.md
+++ b/source/know/concept/probability-current/index.md
@@ -10,48 +10,49 @@ layout: "concept"
In quantum mechanics, the **probability current** describes the movement
of the probability of finding a particle at given point in space.
-In other words, it treats the particle as a heterogeneous fluid with density $$|\psi|^2$$.
-Now, the probability of finding the particle within a volume $$V$$ is:
+Basically, it treats the particle as a heterogeneous fluid with density $$|\psi|^2$$.
+Clearly, the probability of finding the particle within a volume $$V$$ is:
$$\begin{aligned}
- P = \int_{V} | \psi |^2 \ddn{3}{\vb{r}}
+ P = \int_{V} | \psi |^2 \dd{\vb{r}}
\end{aligned}$$
-As the system evolves in time, this probability may change, so we take
-its derivative with respect to time $$t$$, and when necessary substitute
-in the other side of the Schrödinger equation to get:
+As the system evolves in time, this probability may change,
+so we take its derivative with respect to time $$t$$,
+and substitute in the other side of the Schrödinger equation to get:
$$\begin{aligned}
\pdv{P}{t}
- &= \int_{V} \psi \pdv{\psi^*}{t} + \psi^* \pdv{\psi}{t} \ddn{3}{\vb{r}}
- = \frac{i}{\hbar} \int_{V} \psi (\hat{H} \psi^*) - \psi^* (\hat{H} \psi) \ddn{3}{\vb{r}}
+ &= \int_{V} \bigg( \psi \pdv{\psi^*}{t} + \psi^* \pdv{\psi}{t} \bigg) \dd{\vb{r}}
\\
- &= \frac{i}{\hbar} \int_{V} \psi \Big( \!-\! \frac{\hbar^2}{2 m} \nabla^2 \psi^* + V(\vb{r}) \psi^* \Big)
- - \psi^* \Big( \!-\! \frac{\hbar^2}{2 m} \nabla^2 \psi + V(\vb{r}) \psi \Big) \ddn{3}{\vb{r}}
+ &= \frac{i}{\hbar} \int_{V} \bigg( \psi (\hat{H} \psi^*) - \psi^* (\hat{H} \psi) \bigg) \dd{\vb{r}}
\\
- &= \frac{i \hbar}{2 m} \int_{V} - \psi \nabla^2 \psi^* + \psi^* \nabla^2 \psi \ddn{3}{\vb{r}}
- = - \int_{V} \nabla \cdot \vb{J} \ddn{3}{\vb{r}}
+ &= \frac{i}{\hbar} \int_{V} \bigg( \psi \Big( \!-\! \frac{\hbar^2}{2 m} \nabla^2 \psi^* + V(\vb{r}) \psi^* \Big)
+ - \psi^* \Big( \!-\! \frac{\hbar^2}{2 m} \nabla^2 \psi + V(\vb{r}) \psi \Big) \bigg) \dd{\vb{r}}
+ \\
+ &= \frac{i \hbar}{2 m} \int_{V} \bigg( \!-\! \psi \nabla^2 \psi^* + \psi^* \nabla^2 \psi \bigg) \dd{\vb{r}}
+ \\
+ &= - \int_{V} \nabla \cdot \vb{J} \dd{\vb{r}}
\end{aligned}$$
-Where we have defined the probability current $$\vb{J}$$ as follows in
-the $$\vb{r}$$-basis:
+Where we have defined the probability current $$\vb{J}$$
+as follows in the $$\vb{r}$$-basis:
$$\begin{aligned}
\vb{J}
- = \frac{i \hbar}{2 m} (\psi \nabla \psi^* - \psi^* \nabla \psi)
- = \mathrm{Re} \Big\{ \psi \frac{i \hbar}{m} \psi^* \Big\}
+ &\equiv \frac{i \hbar}{2 m} (\psi \nabla \psi^* - \psi^* \nabla \psi)
+ = \Real\!\bigg\{ \psi \Big( \frac{i \hbar}{m} \Big) \nabla \psi^* \bigg\}
\end{aligned}$$
Let us rewrite this using the momentum operator
-$$\vu{p} = -i \hbar \nabla$$ as follows, noting that $$\vu{p} / m$$ is
-simply the velocity operator $$\vu{v}$$:
+$$\vu{p} = -i \hbar \nabla = - \vu{p}^*$$
+as follows, noting that $$\vu{p} / m$$ is simply the velocity operator $$\vu{v}$$:
$$\begin{aligned}
\boxed{
\vb{J}
- = \frac{1}{2 m} ( \psi^* \vu{p} \psi - \psi \vu{p} \psi^*)
- = \mathrm{Re} \Big\{ \psi^* \frac{\vu{p}}{m} \psi \Big\}
- = \mathrm{Re} \{ \psi^* \vu{v} \psi \}
+ = \Real\!\Big\{ \psi^* \frac{\vu{p}}{m} \psi \Big\}
+ = \Real\{ \psi^* \vu{v} \psi \}
}
\end{aligned}$$
@@ -60,8 +61,8 @@ equation:
$$\begin{aligned}
\pdv{P}{t}
- = \int_{V} \pdv{|\psi|^2}{t} \ddn{3}{\vb{r}}
- = - \int_{V} \nabla \cdot \vb{J} \ddn{3}{\vb{r}}
+ = \int_{V} \pdv{|\psi|^2}{t} \dd{\vb{r}}
+ = - \int_{V} \nabla \cdot \vb{J} \dd{\vb{r}}
\end{aligned}$$
By removing the integrals, we thus arrive at the **continuity equation**
@@ -74,16 +75,17 @@ $$\begin{aligned}
}
\end{aligned}$$
-This states that the total probability is conserved, and is reminiscent of charge
-conservation in electromagnetism. In other words, the probability at a
-point can only change by letting it "flow" towards or away from it. Thus
-$$\vb{J}$$ represents the flow of probability, which is analogous to the
-motion of a particle.
+This states that the total probability is conserved,
+and is reminiscent of electric charge conservation.
+In other words, the probability at a point can only change
+by "flowing" towards or away from it.
+Thus $$\vb{J}$$ represents the flow of probability as if it were a fluid.
-As a bonus, this still holds for a particle in an electromagnetic vector
-potential $$\vb{A}$$, thanks to the gauge invariance of the Schrödinger
-equation. We can thus extend the definition to a particle with charge
-$$q$$ in an SI-unit field, neglecting spin:
+As a bonus, the continuity relation still holds
+for a particle in an electromagnetic vector potential $$\vb{A}$$,
+thanks to the gauge invariance of the Schrödinger equation.
+We can thus extend the definition to a particle
+with charge $$q$$ in an SI-unit field, neglecting spin:
$$\begin{aligned}
\boxed{
diff --git a/source/know/concept/rabi-oscillation/index.md b/source/know/concept/rabi-oscillation/index.md
index 9497ad4..a2cea23 100644
--- a/source/know/concept/rabi-oscillation/index.md
+++ b/source/know/concept/rabi-oscillation/index.md
@@ -14,12 +14,12 @@ In quantum mechanics, we know from the
[amplitude rate equations](/know/concept/amplitude-rate-equations/)
that a time-dependent term $$\hat{H}_1$$ in the Hamiltonian
affects the state as follows,
-where $$c_n(t)$$ are the coefficients of the linear combination
+where $$c_n(t)$$ are coefficients of a linear combination
of unperturbed basis states $$\ket{n} e^{-i E_n t / \hbar}$$:
$$\begin{aligned}
i \hbar \dv{c_m}{t}
- = \sum_{n} c_n(t) \matrixel{m}{\hat{H}_1}{n} e^{i \omega_{mn} t}
+ = \sum_{n} c_n(t) \matrixel{m}{\hat{H}_1(t)}{n} e^{i \omega_{mn} t}
\end{aligned}$$
Where $$\omega_{mn} \equiv (E_m \!-\! E_n) / \hbar$$
@@ -36,7 +36,7 @@ $$\begin{aligned}
\end{aligned}$$
Where $$\omega_0 \equiv \omega_{ba}$$ is positive.
-We assume that $$\hat{H}_1$$ has odd spatial parity,
+It is realistic to assume that $$\hat{H}_1$$ has odd spatial parity,
in which case [Laporte's selection rule](/know/concept/selection-rules/)
states that the diagonal matrix elements vanish, leaving:
@@ -49,16 +49,16 @@ $$\begin{aligned}
\end{aligned}$$
We now choose $$\hat{H}_1$$ to be as follows,
-sinusoidally oscillating with a spatially odd $$V(\vec{r})$$:
+sinusoidally oscillating with a spatially odd $$\hat{V}(\vec{r})$$:
$$\begin{aligned}
\hat{H}_1(t)
- = V \cos(\omega t)
- = \frac{V}{2} \Big( e^{i \omega t} + e^{-i \omega t} \Big)
+ = \hat{V} \cos(\omega t)
+ = \frac{\hat{V}}{2} \Big( e^{i \omega t} + e^{-i \omega t} \Big)
\end{aligned}$$
We insert this into the equations for $$c_a$$ and $$c_b$$,
-and define $$V_{ab} \equiv \matrixel{a}{V}{b}$$, leading us to:
+and define $$V_{ab} \equiv \matrixel{a}{\hat{V}}{b}$$, leading us to:
$$\begin{aligned}
\dv{c_a}{t}
@@ -124,7 +124,7 @@ which are found to be:
$$\begin{aligned}
\lambda_1
= i \frac{\omega - \omega_0 + \tilde{\Omega}}{2}
- \qquad \quad
+ \qquad \qquad
\lambda_2
= i \frac{\omega - \omega_0 - \tilde{\Omega}}{2}
\end{aligned}$$
@@ -140,7 +140,7 @@ $$\begin{aligned}
So that the general solution $$c_a(t)$$ is as follows,
where $$A$$ and $$B$$ are arbitrary constants,
-to be determined from initial conditions (and normalization):
+determined by the initial conditions and normalization:
$$\begin{aligned}
\boxed{
@@ -154,7 +154,7 @@ from the coupled equation we started at,
or, if we only care about the probability density $$|c_a|^2$$,
we can use $$|c_b|^2 = 1 - |c_a|^2$$.
For example, if $$A = 0$$ and $$B = 1$$,
-we get the following probabilities
+we get the following probabilities:
$$\begin{aligned}
|c_a(t)|^2
@@ -168,9 +168,8 @@ $$\begin{aligned}
Note that the period was halved by squaring.
This periodic "flopping" of the particle between $$\ket{a}$$ and $$\ket{b}$$
-is known as **Rabi oscillation**, **Rabi flopping** or the **Rabi cycle**.
-This is a more accurate treatment
-of the flopping found from first-order
+is called **Rabi oscillation**, **Rabi flopping** or the **Rabi cycle**.
+This is a more accurate treatment of the flopping found from first-order
[time-dependent perturbation theory](/know/concept/time-dependent-perturbation-theory/).
The name **generalized Rabi frequency** suggests
@@ -183,11 +182,13 @@ $$\begin{aligned}
\equiv \frac{V_{ba}}{\hbar}
\end{aligned}$$
-Some authors use $$|V_{ba}|$$ instead,
-but not doing that lets us use $$\Omega$$ as a nice abbreviation.
-As an example, Rabi oscillation arises
-in the [electric dipole approximation](/know/concept/electric-dipole-approximation/),
-where $$\hat{H}_1$$ is:
+Some authors write $$|V_{ba}|$$ instead,
+but not doing so lets us use $$\Omega$$ as a nice abbreviation.
+For example, Rabi oscillation arises for electrons
+in an oscillating electric field (e.g. a light wave),
+in which case $$\hat{H}_1$$ is as follows according to
+the [electric dipole approximation](/know/concept/electric-dipole-approximation/),
+with charge $$q < 0$$:
$$\begin{aligned}
\hat{H}_1(t)
diff --git a/source/know/concept/time-dependent-perturbation-theory/index.md b/source/know/concept/time-dependent-perturbation-theory/index.md
index b4b35e1..841c219 100644
--- a/source/know/concept/time-dependent-perturbation-theory/index.md
+++ b/source/know/concept/time-dependent-perturbation-theory/index.md
@@ -70,11 +70,11 @@ $$\begin{aligned}
\end{aligned}$$
And so forth. The pattern here is clear: we can calculate the $$(j\!+\!1)$$th
-correction using only our previous result for the $$j$$th correction.
+correction using our result for the $$j$$th correction.
The only purpose of $$\lambda$$ was to help us collect its orders;
in the end we simply set $$\lambda = 1$$ or absorb it into $$\hat{H}_1$$.
Now we have the essence of time-dependent perturbation theory,
-we cannot go any further without considering a specific $$\hat{H}_1$$.
+and we cannot go any further without considering a specific $$\hat{H}_1$$.