Subsection 4.2.3 An Application of the Divergence Theorem — Buoyancy
In this section, we use the divergence theorem to show that when you immerse an object in a fluid the net effect of fluid pressure acting on the surface of the object is a vertical force (called the buoyant force) whose magnitude equals the weight of fluid displaced by the object. This is known as Archimedes’ principle.
We shall also show that the buoyant force acts through the “centre of buoyancy” which is the centre of mass of the fluid displaced by the object. The design of self-righting boats exploits the fact that the centre of buoyancy and the centre of gravity, where gravity acts, need not be the same.
We start by computing the total force due to the pressure of the fluid pushing on the object. Recall that pressure
Thus the force due to pressure that acts on an infinitesimal piece of the object’s surface at \(\vr=(x,y,z)\) with surface area \(\dee{S}\) and outward normal \(\hn\) is \(-p(\vr)\,\hn \dee{S}\text{.}\) The minus sign is there because pressure is directed into the object. If the object fills the volume \(V\) and has surface \(\partial
V\text{,}\) then the total force on the object due to fluid pressure, called the buoyant force, is
\begin{equation*}
\vB=-\dblInt_{\partial V}p(\vr)\,\hn\,\dee{S}
\end{equation*}
We now wish to apply a variant of the divergence theorem to rewrite \(\vB=-\tripInt_V \vnabla p\ \dee{V}\text{.}\) But there is a problem with this: \(p(\vr)\) is the fluid pressure at \(\vr\) and is only defined where there is fluid. In particular, there is no fluid inside the object, so \(p(\vr)\) is not defined for any \(\vr\) in the interior of \(V\text{.}\)
So we pretend that we remove the object from the fluid and we call \(P(\vr)\) the fluid pressure at \(\vr\) when there is no object in the fluid. We also make the assumption that at any point \(\vr\) outside of the object, the pressure at \(\vr\) does not depend on whether the object is in the fluid or not. In other words, we assume that
\begin{equation*}
p(\vr)=\begin{cases}
P(\vr)& \text{if $\vr$ is not in $V$}\\
\text{not defined} & \text{if $\vr$ is in the $V$}
\end{cases}
\end{equation*}
This assumption is only an approximation to reality, but, in practice, it is a very good approximation. So, by Theorem
4.2.9,
\begin{equation}
\vB=-\dblInt_{\partial V}p(\vr)\,\hn\,\dee{S}
=-\dblInt_{\partial V}P(\vr)\,\hn\,\dee{S}
=-\tripInt_{V}\vnabla P(\vr)\,\dee{V}\tag{4.2.1}
\end{equation}
Our next job is to compute \(\vnabla P\text{.}\) Concentrate on an infinitesimal cube of fluid whose edges are parallel to the coordinate axes. Call the lengths of the edges \(\dee{x}\text{,}\) \(\dee{y}\) and \(\dee{z}\) and the position of the centre of the cube \((x,y,z)\text{.}\) The forces applied to the various faces of the cube by the pressure of fluid outside the cube are illustrated in the figure
The total force due to the pressure acting on the cube is the sum
\begin{align*}
&-P\left(x+\frac{\dee{x}}{2},y,z\right)\,dy\dee{z}\,\hi
+P\left(x-\frac{\dee{x}}{2},y,z\right)\,dy\dee{z}\,\hi\\
&-P\left(x,y+\frac{dy}{2},z\right)\,\dee{x}\dee{z}\,\hj
+P\left(x,y-\frac{dy}{2},z\right)\,\dee{x}\dee{z}\,\hj\\
&-P\left(x,y,z+\frac{\dee{z}}{2}\right)\,\dee{x}dy\,\hk
+P\left(x,y,z-\frac{\dee{z}}{2}\right)\,\dee{x}dy\,\hk
\end{align*}
of the forces acting on the six faces. Consider the \(\hi\) component and rewrite it as
\begin{align*}
&-P\left(x+\frac{\dee{x}}{2},y,z\right)\,dy\dee{z}\,\hi
+P\left(x-\frac{\dee{x}}{2},y,z\right)\,dy\dee{z}\,\hi\\
&\hskip1in
=-\frac{P(x+{\dee{x}\over2},y,z)-P(x-{\dee{x}\over2},y,z)}{\dee{x}}\,\hi\
\dee{x} \dee{y} \dee{z}\\
&\hskip1in
= - \frac{\partial P}{\partial x}(x,y,z)\,\hi\
\dee{x} \dee{y} \dee{z}
\end{align*}
Doing this for the other components as well, we see that the total force due to the pressure acting on the cube is
\begin{gather*}
-\Big\{\frac{\partial P}{\partial x}(x,y,z)\,\hi
\!+\!\frac{\partial P}{\partial y}(x,y,z)\,\hj
\!+\!\frac{\partial P}{\partial z}(x,y,z)\,\hk
\Big\}\dee{x} \dee{y} \dee{z}
=-\vnabla P(x,y,z)\, \dee{x} \dee{y} \dee{z}
\end{gather*}
We shall assume that the only other force acting on the cube is gravity and that the fluid is stationary (or at least not accelerating). Hence the total force acting on the cube is zero. If the fluid has density \(\rhof\text{,}\) then the cube has mass \(\rhof\, \dee{x}\dee{y}\dee{z}\) so that the force of gravity is \(- g\rhof\, \dee{x}\dee{y}\dee{z}\,\hk\text{.}\) The vanishing of the total force now tells us that
\begin{equation*}
-\vnabla P(\vr)\, \dee{x} \dee{y} \dee{z}
- g\rhof\, \dee{x} \dee{y} \dee{z}\,\hk=0
\implies \vnabla P(\vr)= - g\rhof \,\hk
\end{equation*}
\begin{equation*}
\vB= g\,\hk\tripInt_{V}\rhof\,\dee{V} = gM_f\,\hk
\end{equation*}
where \(M_f =\tripInt_V \rhof\,\dee{V}\) is the mass of the fluid displaced by the object — not the mass of the object itself. Thus the buoyant force acts straight up and has magnitude equal to \(gM_f \text{,}\) which is also the magnitude of the force of gravity acting on the fluid displaced by the object. In other words, it is the weight of the displaced fluid. This is exactly Archimedes’ principle.
We next consider the rotational motion of our submerged object. The physical law that determines the rotational motion of a rigid body about a point \(\vr_0\) is analogous to the familiar Newton’s law, \(m\frac{d\vv}{\dee{t}}=\vF\text{,}\) that determines the translational motion of the object. For the rotational law of motion,
the mass \(m\) is replaced by a physical quantity, characteristic of the object, called the moment of inertia, and
the ordinary velocity \(\vv\) is replaced by the angular velocity, which is a vector whose length is the rate of rotation (i.e. angle rotated per unit time) and whose direction is parallel to the axis of rotation (with the sign determined by a right hand rule), and
the force \(\vF\) is replaced by a vector called the torque about \(\vr_0\text{.}\) A force \(\vF\) applied at \(\vr=(x,y,z)\) produces the torque \((\vr-\vr_0)\times\vF\) about \(\vr_0\text{.}\)
This is derived in the optional §
4.2.4, entitled “Torque”, and is all that we need to know about rotational motion of rigid bodies in this discussion.
Fix any point \(\vr_0\text{.}\) The total torque about \(\vr_0\) produced by force of pressure acting on the surface of the submerged object is
\begin{equation*}
\vT=\dblInt_{\partial V} (\vr-\vr_0)\times\big(-p(\vr)\hn\big)\,\dee{S}
=\dblInt_{\partial V} \hn\times\big(P(\vr)\, (\vr-\vr_0)\big)\,\dee{S}
\end{equation*}
Recall that in these integrals
\(\vr=(x,y,z)\) is the position of the infinitesimal piece
\(\dee{S}\) of the surface
\(S\text{.}\) Applying the cross product variant of the divergence theorem in Theorem
4.2.9, followed by the vector identity Theorem
4.1.5.c, gives
\begin{align*}
\vT&=\tripInt_V \vnabla\times\big(P(\vr)\,(\vr-\vr_0)\big)\,\dee{V}\\
&=\tripInt_V \big\{\vnabla P(\vr)\times(\vr-\vr_0)
+P(\vr)\underbrace{\vnabla\times(\vr-\vr_0)}_{=\vZero}\big\}\,\dee{V}\cr
&=\tripInt_V \vnabla P(\vr)\times(\vr-\vr_0)\,\dee{V}
\end{align*}
since \(\vnabla\times\vr_0=0\text{,}\) because \(\vr_0\) is a constant, and
\begin{equation*}
\vnabla\times\vr=\det\left[\begin{matrix}
\hi&\hj&\hk\cr
\frac{\partial }{\partial x}&
\frac{\partial }{\partial y}&
\frac{\partial }{\partial z}\\
x&y&z
\end{matrix}\right]
=0
\end{equation*}
We have already found that \(\vnabla P(\vr)=-g\rhof\hk\text{.}\) Substituting it in gives
\begin{align*}
\vT&=-\tripInt_V g\rhof\hk\times(\vr-\vr_0)\,\dee{V}\\
&=-g\hk\times\tripInt_V \rhof (\vr-\vr_0)\,\dee{V}\\
&=-g\hk\times\bigg\{\tripInt_V\! \vr\rhof\,\dee{V}
-\vr_0\!\tripInt_V\! \rhof\,\dee{V}\bigg\}\\
&=-g\bigg\{\tripInt_V\! \rhof\,\dee{V}\bigg\}\hk\times \bigg\{
\frac{\tripInt_V \vr\rhof\,\dee{V}}{\tripInt_V\rhof\,
\dee{V}}-\vr_0\bigg\}\\
&=-\vB\times\bigg\{\frac{\tripInt_V \vr\rhof\,\dee{V}}
{\tripInt_V\rhof\,\dee{V}}-\vr_0\bigg\}\\
&=\bigg\{\frac{\tripInt_V \vr\rhof\,\dee{V}}
{\tripInt_V\rhof\,\dee{V}}-\vr_0\bigg\}\times\vB
\end{align*}
So the torque generated at \(\vr_0\) by pressure over the entire surface is the same the torque generated at \(\vr_0\) by a force \(\vB\) applied at the single point
\begin{equation*}
\vC_\vB=\frac{\tripInt_V \vr\rhof\,\dee{V}}{\tripInt_V\rhof\,\dee{V}}
\end{equation*}
This point is called the centre of buoyancy. It is the centre of mass of the displaced fluid.
The moral of the above discussion is that the buoyant force, \(\vB\text{,}\) on a rigid body
acts straight upward,
has magnitude equal to the weight of the displaced fluid and
acts at the centre of buoyancy, which is the centre of mass of the displaced fluid.
As above, denoting by \(\rhob\) the density of the object, the torque about \(\vr_0\) due to gravity acting on the object is
\begin{equation*}
\tripInt_V (\vr-\vr_0)\times(-g\rhob\hk)\,\dee{V}
=\bigg\{\frac{\tripInt_V \vr\rhob\,\dee{V}}
{\tripInt_V\rhob\,\dee{V}}-\vr_0\bigg\}\times
\left(-g\bigg\{\tripInt_V \rhob\,\dee{V}\bigg\}\ \hk\right)
\end{equation*}
So the gravitational force, \(\vG\text{,}\)
acts straight down,
has magnitude equal to the weight \(g M_b=g\tripInt_V \vr\rhob\,\dee{V}\) (where \(\rhob\) is the density of the object) of the object and
acts at the centre of mass, \(\vC_\vG=\frac{\tripInt_V \vr\rhob\,\dee{V}}{\tripInt_V\rhob\,\dee{V}}
\text{,}\) of the object.
Because the mass distribution of the object need not be the same as the mass distribution of the displaced fluid, buoyancy and gravity may act at two different points. This is exploited in the design of self-righting boats.
These boats are constructed with a heavy, often lead (which is cheap and dense), keel. As a result, the centre of gravity is lower in the boat than the center of buoyancy, which, because the displaced fluid has constant density, is at the geometric centre of the boat. As the figure below illustrates, a right side up configuration of such a boat is stable, while an upside down configuration is unstable. The boat rotates so as to keep the centre of gravity straight below the centre of buoyancy. To see this pretend that you are holding on to the boat with one hand holding the centre of buoyancy and the other hand holding the centre of gravity. Use your hands to apply forces in the directions of the arrows and think about how the boat will respond.
Subsection 4.2.4 Optional — Torque
In this section, we derive the properties of torque that we used in the last section. Newton’s law of motion says that the position \(\vr(t)\) of a single particle moving under the influence of a force \(\vF\) obeys \(m\vr''(t)=\vF\text{.}\) Similarly, the positions \(\vr_i(t)\text{,}\) \(1\le i\le n\text{,}\) of a set of particles moving under the influence of forces \(\vF_i\) obey \(m\vr_i''(t)=\vF_i\text{,}\) \(1\le i\le n\text{.}\) Very often systems of interest consist of some small number of rigid bodies. Suppose that we are interested in the motion of a single rigid body, say a piece of wood. The piece of wood is made up of a huge number of atoms. So the system of equations determining the motion of all of the individual atoms in the piece of wood is huge. On the other hand, we shall see that because the piece of wood is rigid, its configuration is completely determined by the position of, for example, its centre of mass and its orientation (we won’t get into what precisely is meant by “orientation”, but it is certainly determined by, for example, the positions of a few of the corners of the piece of wood). To be precise, we shall extract from the huge system of equations that determine the motion of all of the individual atoms, a small system of equations that determine the motion of the centre of mass and the orientation. We’ll do so now.
Imagine a piece of wood moving in \(\bbbr^3\text{.}\)
Furthermore, imagine that the piece of wood consists of a huge number of particles joined by a huge number of weightless but very strong steel rods. The steel rod joining particle number one to particle number two just represents a force acting between particles number one and two. Suppose that
there are \(n\) particles, with particle number \(i\) having mass \(m_i\text{,}\)
at time \(t\text{,}\) particle number \(i\) has position \(\vr_i(t)\text{,}\)
at time \(t\text{,}\) the external force (gravity and the like) acting on particle number \(i\) is \(\vF_i(t)\text{,}\) and
at time \(t\text{,}\) the force acting on particle number \(i\text{,}\) due to the steel rod joining particle number \(i\) to particle number \(j\) is \(\vF_{i,j}(t)\text{.}\) If there is no steel rod joining particles number \(i\) and \(j\text{,}\) just set \(\vF_{i,j}(t)=0\text{.}\) In particular, \(\vF_{i,i}(t)=0\text{.}\)
The only assumptions that we shall make about the steel rod forces are
- (A1)
for each \(i\ne j\text{,}\) \(\vF_{i,j}(t)=-\vF_{j,i}(t)\text{.}\) In words, the steel rod joining particles \(i\) and \(j\) applies equal and opposite forces to particles \(i\) and \(j\text{.}\)
- (A2)
for each \(i\ne j\text{,}\) there is a function \(M_{i,j}(t)\) such that \(\vF_{i,j}(t)=M_{i,j}(t)\big[\vr_i(t)-\vr_j(t)\big]\text{.}\) In words, the force due to the rod joining particles \(i\) and \(j\) acts parallel to the line joining particles \(i\) and \(j\text{.}\) For (A1) to be true, that is to have \(M_{i,j}(t)\big[\vr_i(t)-\vr_j(t)\big]
=-M_{j,i}(t)\big[\vr_j(t)-\vr_i(t)\big]\text{,}\) we need \(M_{i,j}(t)=M_{j,i}(t)\text{.}\)
Newton’s law of motion, applied to particle number \(i\text{,}\) now tells us that
\begin{equation*}
m_i \vr''_i(t)
= \vF_i(t)+\sum_{j=1}^n \vF_{i,j}(t)
\tag{$N_i$}
\end{equation*}
Adding up all of the equations (\(N_i\)), for \(i=1,\ 2,\ 3,\ \cdots,\ n\) gives
\begin{equation*}
\sum_{i=1}^n m_i \vr''_i(t)
= \sum_{i=1}^n \vF_i(t)+\sum_{1\le i,j\le n} \vF_{i,j}(t)
\tag{$\Sigma N_i$}
\end{equation*}
The sum \(\sum\limits_{1\le i,j\le n} \vF_{i,j}(t)\) contains \(\vF_{1,2}(t)\) exactly once and it also contains \(\vF_{2,1}(t)\) exactly once and these two terms cancel exactly, by assumption (A1). In this way, all terms in \(\sum\limits_{1\le i,j\le n} \vF_{i,j}(t)\) with \(i\ne j\) exactly cancel. All terms with \(i=j\) are assumed to be zero. So \(\sum\limits_{1\le i,j\le n} \vF_{i,j}(t)=0\) and the equation (\(\Sigma N_i\)) simplifies to
\begin{equation*}
\sum_{i=1}^n m_i \vr''_i(t)
= \sum_{i=1}^n \vF_i(t)
\tag{$ \Sigma N_i $}
\end{equation*}
Phew! Denote by \(M=\sum\limits_{i=1}^n m_i\) the total mass of the body, by \(\vR(t)=\frac{1}{M}\sum\limits_{i=1}^n m_i\vr_i(t)\) the centre of mass of the body and by \(\vF(t)=\sum\limits_{i=1}^n \vF_i(t)\) the total external force acting on the system. In this notation, equation (\(\Sigma N_i\)) can be written as
Equation 4.2.10.
\begin{equation*}
M\vR''(t)=\vF(t)
\end{equation*}
The upshot is that the centre of mass of the system moves just like a single particle of mass \(M\) subject to the total external force. This is why we can often replace an extended object by a point mass at its centre of mass.
Now take the cross product of \(\vr_i(t)\) and equation (\(N_i\)) and sum over \(i\text{.}\) This gives
\begin{align*}
&\sum_{i=1}^n m_i\ \vr_i(t)\times\vr''_i(t)\\
&\hskip0.5in= \sum_{i=1}^n \vr_i(t)\times\vF_i(t)
+\sum_{1\le i,j\le n} \vr_i(t)\times\vF_{i,j}(t)
\tag{$\Sigma \vr_i\times N_i$}
\end{align*}
By the assumption (A2)
\begin{align*}
\vr_1(t)\times\vF_{1,2}(t)
&=M_{1,2}(t)\ \vr_1(t)\times\big[\vr_1(t)-\vr_2(t)\big]\\
\vr_2(t)\times\vF_{2,1}(t)
&=M_{2,1}(t)\ \vr_2(t)\times\big[\vr_2(t)-\vr_1(t)\big]\\
&=-M_{1,2}(t)\ \vr_2(t)\times\big[\vr_1(t)-\vr_2(t)\big]\\
\end{align*}
so that
\begin{align*}
\vr_1(t)\times\vF_{1,2}(t)
+\vr_2(t)\times\vF_{2,1}(t)
&=M_{1,2}(t)\ \big[\vr_1(t)-\vr_2(t)\big]\times\big[\vr_1(t)-\vr_2(t)\big]
=0
\end{align*}
because the cross product of any two parallel vectors is zero.
The last equation says that the \(i=1\text{,}\) \(j=2\) term in \(\sum\limits_{1\le i,j\le n} \vr_i(t)\times\vF_{i,j}(t)\) exactly cancels the \(i=2\text{,}\) \(j=1\) term. In this way all of the terms in \(\sum\limits_{1\le i,j\le n} \vr_i(t)\times\vF_{i,j}(t)\) with \(i\ne j\) cancel. Each term with \(i=j\) is exactly zero because \(\vF_{ii}=0\text{.}\) So \(\sum\limits_{1\le i,j\le n} \vr_i(t)\times\vF_{i,j}(t)=0\) and (\(\Sigma \vr_i\times N_i\)) simplifies to
\begin{equation*}
\sum_{i=1}^n m_i\ \vr_i(t)\times\vr''_i(t)
= \sum_{i=1}^n \vr_i(t)\times\vF_i(t)
\tag{$\Sigma \vr_i\times N_i$}
\end{equation*}
At this point it makes sense to define vectors
\begin{align*}
\vL(t)&= \sum_{i=1}^n m_i\ \vr_i(t)\times\vr'_i(t)\\
\vT(t)&=\sum_{i=1}^n \vr_i(t)\times\vF_i(t)
\end{align*}
because, in this notation, (\(\Sigma \vr_i\times N_i\)) becomes
Equation 4.2.11.
\begin{equation*}
\diff{ }{t}\vL(t)=\vT(t)
\end{equation*}
Equation
4.2.11 plays the role of Newton’s law of motion for rotational motion.
\(\vT(t)\) is called the torque and plays the role of “rotational force”.
\(\vL(t)\) is called the angular momentum (about the origin) and is a measure of the rate at which the piece of wood is rotating. For example, if a particle of mass
\(m\) is travelling in a circle of radius
\(\rho\) in the
\(xy\)-plane at
\(\om\) radians per unit time, then
\(\vr(t)=\rho\cos(\om t)\hi+\rho\sin(\om t)\hj\) and
\begin{align*}
m\vr(t)\times\vr'(t)
&= m \big[\rho\cos(\om t)\hi+\rho\sin(\om t)\hj\big]
\times\big[-\om\rho\sin(\om t)\hi+\om\rho\cos(\om t)\hj\big]\\
&=m \rho^2\ \om\ \hk
\end{align*}
is proportional to \(\om\text{,}\) which is the rate of rotation about the origin and is in the direction \(\hk\text{,}\) which is normal to the plane containing the circle.
In any event, in order for the piece of wood to remain stationary, equations
4.2.10 and
4.2.11 force
\(\vF(t)=\vT(t)=0\text{.}\)
Now suppose that the piece of wood is a seesaw that is supported on a fulcrum at \(\vp\text{.}\) The forces consist of gravity, \(-m_ig\hk\text{,}\) acting on particle number \(i\text{,}\) for each \(1\le i\le n\text{,}\) and the
force \(\vPhi\) imposed by the fulcrum that is pushing up on the particle at \(\vp\text{.}\) The total external force is \(\vF=\vPhi-\sum\limits_{i=1}^n m_ig\hk
=\vPhi-Mg\hk\text{.}\) If the seesaw is to remain stationary, this must be zero so that \(\vPhi=Mg\hk\text{.}\)
The total torque (about the origin) is
\begin{equation*}
\vT=\vp\times\vPhi-\sum_{i=1}^n m_ig \vr_i\times\hk
=g\Big(M\vp-\sum_{i=1}^n m_i \vr_i\Big)\times\hk
\end{equation*}
If the seesaw is to remain stationary, this must also be zero. This will be the case if the fulcrum is placed at
\begin{equation*}
\vp=\frac{1}{M}\sum_{i=1}^n m_i \vr_i
\end{equation*}
which is just the centre of mass of the piece of wood.
More generally, suppose that the external forces acting on the piece of wood consist of \(\vF_i\text{,}\) acting on particle number \(i\text{,}\) for each \(1\le i\le n\text{,}\) and a “fulcrum force” \(\vPhi\) acting on a particle at \(\vp\text{.}\) The total external force is \(\vF=\vPhi+\sum\limits_{i=1}^n \vF_i\text{.}\) If the piece of wood is to remain stationary, this must be zero so that \(\vPhi=-\sum\limits_{i=1}^n \vF_i\text{.}\) The total torque (about the origin) is
\begin{equation*}
\vT=\vp\times\vPhi+\sum_{i=1}^n \vr_i\times\vF_i
=\sum_{i=1}^n (\vr_i-\vp)\times\vF_i
\end{equation*}
If the piece of wood is to remain stationary, this must also be zero. That is, the torque about point \(\vp\) due to all of the forces \(\vF_i\text{,}\) \(1\le i\le n\text{,}\) must be zero.
Subsection 4.2.5 Optional — Solving Poisson’s Equation
In this section we shall use the divergence theorem to find a formula for the solution of Poisson’s equation
\begin{equation*}
\vnabla^2\varphi = 4\pi\rho
\end{equation*}
Here \(\rho=\rho(\vr)\) is a given (continuous) function and \(\varphi\) is the unknown function that we wish to find. This equation arises, for example, in electrostatics, where \(\rho\) is the charge density and \(\varphi\) is the electric potential.
The main step in finding this solution formula will be to consider an
arbitrary (smooth) function \(\varphi\) and an
arbitrary (smooth) region \(V\) in \(\bbbr^3\) and an
arbitrary point \(\vr_0\) in the interior of \(V\)
and to find an auxiliary formula which expresses \(\varphi(\vr_0)\) in terms of
\(\vnabla^2\varphi(\vr)\text{,}\) with \(\vr\) running over \(V\) and
\(\vnabla\varphi(\vr)\) and \(\varphi(\vr)\text{,}\) with \(\vr\) running only over \(\partial V\text{.}\)
This auxiliary formula, which we shall derive below, is
\begin{align*}
\varphi(\vr_0)&=-\frac{1}{4\pi}\bigg\{
\tripInt_V\frac{ \vnabla^2\varphi(\vr)}{|\vr-\vr_0|}\ d^3\vr
-\dblInt_{\partial V}\varphi(\vr)\frac{\vr-\vr_0}{|\vr-\vr_0|^3}\cdot\hn\ \dee{S}\\
&\hskip1in-\dblInt_{\partial V}\frac{\vnabla\varphi(\vr)}{|\vr-\vr_0|}\cdot\hn\ \dee{S}\bigg\}
\tag{$V$}
\end{align*}
When we take the limit as \(V\) expands to fill all of \(\bbbr^3\) then, assuming that \(\varphi\) and \(\vnabla\varphi\) go to zero sufficiently quickly at \(\infty\text{,}\) the two integrals over \(\partial V\) will converge to zero and we will end up with the formula
\begin{equation*}
\varphi(\vr_0)=-\frac{1}{4\pi}
\tripInt_{\bbbr^3}\frac{ \vnabla^2\varphi(\vr)}{|\vr-\vr_0|}\ d^3\vr
\end{equation*}
This expresses \(\varphi\) evaluated at an arbitrary point, \(\vr_0\text{,}\) of \(\bbbr^3\) in terms of \(\vnabla^2\varphi(\vr)\text{,}\) with \(\vr\) running over \(\bbbr^3\text{,}\) which is exactly what we want, since \(\vnabla^2\varphi = 4\pi\rho\) for any solution of Poisson’s equation. So once we have proven (V) we will have proven
Theorem 4.2.12.
Assume that \(\rho(\vr)\) is continuous and decays sufficiently quickly as \(\vr\rightarrow\infty\text{.}\) If \(\varphi\) obeys \(\vnabla^2\varphi = 4\pi\rho\) on \(\bbbr^3\text{,}\) and \(\varphi\) and \(\vnabla\varphi\) decay sufficiently quickly as \(\vr\rightarrow\infty\text{,}\) then
\begin{equation*}
\varphi(\vr_0)=
-\tripInt_{\bbbr^3}\frac{ \rho(\vr)}{|\vr-\vr_0|}\ d^3\vr
\end{equation*}
for all \(\vr_0\) in \(\bbbr^3\text{.}\)
Let
\begin{align*}
\vr(x,y,z)&=x\,\hi+y\,\hj+z\,\hk\\
\vr_0&=x_0\,\hi+y_0\,\hj+z_0\,\hk
\end{align*}
We shall exploit three properties of the function \(\frac{1}{|\vr-\vr_0|}\text{.}\) The first two properties are
\begin{align*}
\vnabla \frac{1}{|\vr-\vr_0|} &=-\frac{\vr-\vr_0}{|\vr-\vr_0|^3}\tag{P1}\\
\vnabla^2 \frac{1}{|\vr-\vr_0|} &=-\vnabla\cdot\frac{\vr-\vr_0}{|\vr-\vr_0|^3}
=0
\tag{P2}
\end{align*}
and are valid for all \(\vr\ne \vr_0\text{.}\) Verification of the first property is a simple one line computation. Verification of the second property is a simple three line computation. (See the solution to Question 6 in Section 4.1.)
The other property of \(\frac{1}{|\vr-\vr_0|}\) that we shall use is the following. Let \(S_\veps\) be the sphere of radius \(\veps\) centered on \(\vr_0\text{.}\) Then, for any continuous function \(\psi(\vr)\text{,}\)
\begin{align*}
\lim_{\veps\rightarrow 0+}\dblInt_{S_\veps}
\frac{\psi(\vr)}{|\vr-\vr_0|^p}\ \dee{S}
&=\lim_{\veps\rightarrow 0+} \frac{1}{\veps^p} \dblInt_{S_\veps}
\psi(\vr)\ \dee{S}
=\lim_{\veps\rightarrow 0+}\frac{\psi(\vr_0)}{\veps^p}
\dblInt_{S_\veps}\ \dee{S}\\
&=\lim_{\veps\rightarrow 0+}\frac{\psi(\vr_0)}{\veps^p}4\pi\veps^2
\notag\\
&=\begin{cases}4\pi\psi(\vr_0)& \text{if } p=2 \\
0 & \text{if } p \lt 2\\
\text{undefined} & \text{if } p \gt 2
\end{cases}
\tag{P3}
\end{align*}
Derivation of (V):
Here is the derivation of (\(V\)). Let \(V_\veps\) be the part of \(V\) outside of \(S_\veps\text{.}\)
Note that the boundary \(\partial V_\veps\) of \(V_\veps\) consists of two parts — the boundary \(\partial V\) of \(V\) and the sphere \(S_\veps\) — and that the unit outward normal to \(\partial V_\veps\) on \(S_\veps\) is \(-\frac{\vr-\vr_0}{|\vr-\vr_0|}\text{,}\) because it points towards \(\vr_0\) and hence outside of \(V_\veps\text{.}\)
Recall the vector identity Theorem
4.1.7.d, which says
\begin{equation*}
\vnabla\cdot(f\vnabla g-g\vnabla f)=f\,\vnabla^2g-g\,\vnabla^2f
\end{equation*}
Applying this identity with \(f= \frac{1}{|\vr-\vr_0|}\) and \(g=\varphi\) gives
\begin{align*}
\vnabla\cdot\Big(\frac{1}{|\vr-\vr_0|}\vnabla\varphi
-\varphi\vnabla\frac{1}{|\vr-\vr_0|}\Big)
&=\frac{\vnabla^2\varphi}{|\vr-\vr_0|}
-\varphi\,\overbrace{ \vnabla^2\frac{1}{|\vr-\vr_0|} }^{=0\text{ by (P2)}}\\
&=\frac{\vnabla^2\varphi}{|\vr-\vr_0|}
\end{align*}
which is the integrand of the first integral on the right hand side of (V). So, by the divergence theorem
\begin{align*}
&\tripInt_{V_\veps} \frac{\vnabla^2\varphi}{|\vr-\vr_0|} dV
=\tripInt_{V_\veps}\vnabla\cdot\Big(\frac{1}{|\vr-\vr_0|}\vnabla\varphi
-\varphi\vnabla\frac{1}{|\vr-\vr_0|}\Big) dV\\
&\hskip0.25in=\dblInt_{\partial V}\Big(\frac{1}{|\vr-\vr_0|}\vnabla\varphi
-\varphi\vnabla\frac{1}{|\vr-\vr_0|}\Big)\cdot\hn\ \dee{S}\\
&\hskip1.0in+\dblInt_{S_\veps}\Big(\frac{1}{|\vr-\vr_0|}\vnabla\varphi
-\varphi\vnabla\frac{1}{|\vr-\vr_0|}\Big)\cdot
\Big(-\frac{\vr-\vr_0}{|\vr-\vr_0|}\Big) \dee{S}
\tag{M}
\end{align*}
To see the connection between (M) and the rest of (V), note that,
by (P1), the first term on the right hand side of (M) is
\begin{align*}
&\dblInt_{\partial V}\Big(\frac{1}{|\vr-\vr_0|}\vnabla\varphi
-\varphi\vnabla\frac{1}{|\vr-\vr_0|}\Big)\cdot\hn\ \dee{S}\\
&\hskip0.5in=\dblInt_{\partial V}\frac{\vnabla\varphi(\vr)}{|\vr-\vr_0|}\cdot\hn\ \dee{S}
+\dblInt_{\partial V}\varphi(\vr)\frac{\vr-\vr_0}{|\vr-\vr_0|^3}\cdot\hn\ \dee{S}
\tag{R1}
\end{align*}
which is
\(4\pi\) times the second and third terms on the right hand side of (V),
and substituting in
\(\vnabla \frac{1}{|\vr-\vr_0|} =-\frac{\vr-\vr_0}{|\vr-\vr_0|^3}\text{,}\) from (P1), and applying (P3) with
\(p=2\text{,}\) the limit of the second term on the right hand side of (M) is
\begin{align*}
&\lim_{\veps\rightarrow 0+}
\dblInt_{S_\veps}\Big(\frac{1}{|\vr-\vr_0|}\vnabla\varphi
-\varphi\vnabla\frac{1}{|\vr-\vr_0|}\Big)\cdot
\Big(-\frac{\vr-\vr_0}{|\vr-\vr_0|}\Big) \dee{S}\\
&\hskip1in=-\lim_{\veps\rightarrow 0+}
\dblInt_{B_\veps}\big[\vnabla\varphi\cdot(\vr-\vr_0)+\varphi\big]
\frac{1}{|\vr-\vr_0|^2} \dee{S}\\
&\hskip1in=-4\pi\Big[\vnabla\varphi\cdot(\vr-\vr_0)+\varphi\Big]_{\vr=\vr_0}\\
&\hskip1in=-4\pi\varphi(\vr_0)
\tag{R2}
\end{align*}
So applying \(\lim_{\veps\rightarrow 0+}\) to (M) and substituting in (R1) and (R2) gives
\begin{gather*}
\tripInt_{V}\frac{\vnabla^2\varphi}{|\vr-\vr_0|}\ dV
=\dblInt_{\partial V}\frac{\vnabla\varphi(\vr)}{|\vr-\vr_0|}\cdot\hn\ \dee{S}
+\dblInt_{\partial V}\varphi(\vr)\frac{\vr-\vr_0}{|\vr-\vr_0|^3}\cdot\hn\ \dee{S}
-4\pi\varphi(\vr_0)
\end{gather*}
which is exactly equation (V).