Integration and Gauss's Theorem

At the center of this Chapter is the celebrated divergence theorem, also known as Gauss's theorem, as well as by a number of other names, which is a direct consequence of the Fundamental Theorem of Calculus and, in some ways, a generalization of it.
The Fundamental Theorem of Calculus reads
abf(ξ)dξ=F(b)F(a),(11.1)\int_{a}^{b}f\left( \xi\right) d\xi=F\left( b\right) -F\left( a\right) ,\tag{11.1}
where f(x)f\left( x\right) is the derivative of F(x)F\left( x\right) . In words, the Fundamental Theorem of Calculus states that an integral of the derivative f(x)f\left( x\right) of a function F(x)F\left( x\right) can be expressed in terms of the values of F(x)F\left( x\right) at the ends of the integration interval. The divergence theorem applies to a multi-dimensional domain Ω\Omega with boundary SS and states that the integral of the divergence iTi\nabla_{i}T^{i} of a tensor field TiT^{i} over the domain can be expressed in terms of the values of TiT^{i} on the boundary.
(11.2)
Specifically, the divergence theorem reads
ΩiTidΩ=SNiTidS,(11.3)\int_{\Omega}\nabla_{i}T^{i}d\Omega=\int_{S}N_{i}T^{i}dS,\tag{11.3}
where NiN_{i} are the components the outward normal N\mathbf{N}.
(11.4)
Note that the divergence theorem remains valid for tensors Ti\mathbf{T}^{i} with vector elements, i.e.
ΩiTidΩ=SNiTidS,(11.5)\int_{\Omega}\nabla_{i}\mathbf{T}^{i}d\Omega=\int_{S}N_{i}\mathbf{T}^{i}dS,\tag{11.5}
in which case both integrals represent vector quantities.
Remarkably, the tensor formulation of the divergence theorem remains completely intact for curved domains. Suppose that SS is a curved domain with a contour boundary LL and let nαn^{\alpha} be the surface components of its outward geodesic normal n\mathbf{n}.
(11.6)
Then, for a surface tensor TαT^{\alpha}, the divergence theorem reads
SαTαdS=LnαTαdL.(11.7)\int_{S}\nabla_{\alpha}T^{\alpha}dS=\int_{L}n_{\alpha}T^{\alpha}dL.\tag{11.7}
The curved form of the divergence theorem also remains valid for tensors with vector elements, i.e.
SαTαdS=LnαTαdL.(11.8)\int_{S}\nabla_{\alpha}\mathbf{T}^{\alpha}dS=\int_{L}n_{\alpha}\mathbf{T} ^{\alpha}dL.\tag{11.8}
Note that one of the essential aspects of the divergence theorem is its invariant nature. Indeed, all elements of the theorem are invariant objects that can, at least conceptually, be evaluated without the use of a coordinate system.
Crucially, the scalar forms of the divergence theorem do not include any elements specific to Euclidean spaces. Thus, the statements of the theorem remain meaningful -- and, perhaps more importantly, correct -- in the more general Riemannian spaces and generalize to arbitrary dimension. Note that while the use of the letters SS and LL, which we have typically used for two-dimensional domains and their one-dimensional contour boundaries, suggests that the equation
SαTαdS=LnαTαdL(11.7)\int_{S}\nabla_{\alpha}T^{\alpha}dS=\int_{L}n_{\alpha}T^{\alpha}dL \tag{11.7}
is two-dimensional, it can actually be validly interpreted for a domain SS of any dimension nn with an (n1)\left( n-1\right) -dimensional boundary LL. In this arbitrary-dimensional Riemannian interpretation, there is in fact no difference between the above form and
ΩiTidΩ=SNiTidS,(11.3)\int_{\Omega}\nabla_{i}T^{i}d\Omega=\int_{S}N_{i}T^{i}dS, \tag{11.3}
which can be considered a special case of the more general Riemannian interpretation.
In the upcoming investigations, we will strike a compromise between the Euclidean and Riemannian perspectives. For the sake of geometric intuition, we will discuss the specific case of a curved two-dimensional surface SS in a Euclidean space. However, we will restrict ourselves to analytical arguments that remain valid in the more general Riemannian spaces.
Before we turn our attention to the derivation of the divergence theorem, let us take a look at a few of its striking theoretical applications in a Euclidean space

11.2.1The integral SNdS\int_{S}\mathbf{N}dS

For any Euclidean domain Ω\Omega, the integral of the unit normal N\mathbf{N} over its boundary SS vanishes, i.e.
SNdS=0.(11.9)\int_{S}\mathbf{N}dS=\mathbf{0}.\tag{11.9}
The demonstration of this relationship by the divergence theorem is entirely straightforward. Since the integral in question can be written in component form as
SNdS=SNiZi dS,(11.10)\int_{S}\mathbf{N}dS=\int_{S}N^{i}\mathbf{Z}_{i}~dS,\tag{11.10}
an application of the divergence theorem yields
SNdS=ΩiZi dΩ.(11.11)\int_{S}\mathbf{N}dS=\int_{\Omega}\nabla^{i}\mathbf{Z}_{i}~d\Omega.\tag{11.11}
Now, thanks to the metrinilic property of the covariant derivative with respect to the covariant basis Zi\mathbf{Z}_{i}, i.e.
iZi=0,(11.12)\nabla^{i}\mathbf{Z}_{i}=0,\tag{11.12}
we find that
SNdS=0,(11.9)\int_{S}\mathbf{N}dS=\mathbf{0,} \tag{11.9}
as we set out to show. Finally, we note that this integral may be interpreted as the net force on the body occupying the domain Ω\Omega from a uniform pressure field. The fact that the integral vanishes is consistent with our experience that a free body placed in a uniform pressure field remains at equilibrium.

11.2.2The integral SNBααdS\int_{S}\mathbf{N}B_{\alpha}^{\alpha}dS

For an application of the divergence theorem to a curved domain, let us now consider a similar integral
SNBααdS(11.13)\int_{S}\mathbf{N}B_{\alpha}^{\alpha}dS\tag{11.13}
of the curvature normal NBαα\mathbf{N}B_{\alpha}^{\alpha} over a surface patch SS with boundary LL. Under the Laplace model of capillary forces, this integral may be interpreted as the net force of surface tension acting upon a soap film represented by the curved surface SS. Since, in our experience, the center of mass of a soap bubble does not experience acceleration under the influence of surface tension, we expect this integral to also equal zero for a closed surface SS.
Recall that the combination NBαα\mathbf{N}B_{\alpha}^{\alpha} equals the surface Laplacian of the position vector R\mathbf{R}, i.e.
NBαα=ααR,(11.14)\mathbf{N}B_{\alpha}^{\alpha}=\nabla_{\alpha}\nabla^{\alpha}\mathbf{R},\tag{11.14}
or, equivalently, the divergence of the surface contravariant basis Sα\mathbf{S}^{\alpha}, i.e.
NBαα=αSα.(11.15)\mathbf{N}B_{\alpha}^{\alpha}=\nabla_{\alpha}\mathbf{S}^{\alpha}.\tag{11.15}
Therefore, by the divergence theorem, we have
SNBααdS=SαSαdS=LnαSαdL.(11.16)\int_{S}\mathbf{N}B_{\alpha}^{\alpha}dS=\int_{S}\nabla_{\alpha}\mathbf{S} ^{\alpha}dS=\int_{L}n_{\alpha}\mathbf{S}^{\alpha}dL.\tag{11.16}
Since the combination nαSαn_{\alpha}\mathbf{S}^{\alpha} represents the outward geodesic normal n\mathbf{n}, we have
SNBααdS=LndL(11.17)\int_{S}\mathbf{N}B_{\alpha}^{\alpha}dS=\int_{L}\mathbf{n}dL\tag{11.17}
In words, the integral of the curvature normal NBαα\mathbf{N}B_{\alpha}^{\alpha} over a surface patch equals the integral of the outward geodesic normal n\mathbf{n} over the contour of the patch.
By all accounts, this relationship makes intuitive geometric sense, especially over a small patch: the more curved is the patch, the more the geodesic normals at its boundary point in a consistent direction.
(11.18)
If the patch is flat, i.e. Bαα=0B_{\alpha}^{\alpha}=0, then the contour integral vanishes, i.e.
LndL=0,(11.19)\int_{L}\mathbf{n}dL=\mathbf{0,}\tag{11.19}
which is precisely the two-dimensional version of the Euclidean formula
SNdS=0(11.9)\int_{S}\mathbf{N}dS=\mathbf{0} \tag{11.9}
in the previous example.
Furthermore, we observe that the curvature normal NBαα\mathbf{N}B_{\alpha }^{\alpha} at a given point PP is given by the limit
NBαα=limS0LndLSdS,(11.20)\mathbf{N}B_{\alpha}^{\alpha}=\lim_{S\rightarrow0}\frac{\int_{L}\mathbf{n} dL}{\int_{S}dS},\tag{11.20}
where each integral is calculated over a patch SS that is shrinking to the point PP in a regular manner. Dotting both sides with N\mathbf{N} gives an explicit limit for the mean curvature BααB_{\alpha}^{\alpha}, i.e.
Bαα=NlimS0LndLSdS.(11.21)B_{\alpha}^{\alpha}=\mathbf{N}\cdot\lim_{S\rightarrow0}\frac{\int _{L}\mathbf{n}dL}{\int_{S}dS}.\tag{11.21}
Finally, note that when the patch SS represents a closed surface, i.e. there is no boundary, the formula
SNBααdS=LndL(11.17)\int_{S}\mathbf{N}B_{\alpha}^{\alpha}dS=\int_{L}\mathbf{n}dL \tag{11.17}
implies that the integral of the curvature normal NBαα\mathbf{N}B_{\alpha }^{\alpha} vanishes, i.e.
SNBααdS=0,(11.22)\int_{S}\mathbf{N}B_{\alpha}^{\alpha}dS=\mathbf{0},\tag{11.22}
as we expected.

11.2.3A few other surface integrals

The relationships discussed above have interesting "companion" formulas where the integrand is dot multiplied by the position vector field R\mathbf{R}. All of these formulas also follow from the divergence theorem and their proofs are left as exercises.
For a closed surface SS, the volume VV of the enclosed domain Ω\Omega is given in terms of the surface integral of RN\mathbf{R}\cdot\mathbf{N} by the formula
V=1nSRNdS,(11.23)V=\frac{1}{n}\int_{S}\mathbf{R}\cdot\mathbf{N}dS,\tag{11.23}
where nn is the dimension of the ambient space.
Similarly, the surface integral of RNBαα\mathbf{R}\cdot\mathbf{N}B_{\alpha }^{\alpha} over SS yields its area AA according to the formula
A=1n1SRNBααdS.(11.24)A=-\frac{1}{n-1}\int_{S}\mathbf{R}\cdot\mathbf{N}B_{\alpha}^{\alpha }dS.\tag{11.24}
For a non-closed patch SS with boundary LL, the analogous formula reads
A=1n1(LRndLSRNBααdS).(11.25)A=\frac{1}{n-1}\left( \int_{L}\mathbf{R}\cdot\mathbf{n}dL-\int_{S} \mathbf{R}\cdot\mathbf{N}B_{\alpha}^{\alpha}dS\right) .\tag{11.25}
(Note that despite the use of the same letter, there is no relation between the dimension nn of the ambient space and the geodesic normal n\mathbf{n}.)
What happens when the mean curvature BααB_{\alpha}^{\alpha} in the above integrals is replaced with Gaussian curvature KK? It turns out that for a closed two-dimensional surface SS, the integral of NK\mathbf{N}K vanishes, i.e.
SNKdS=0.(11.26)\int_{S}\mathbf{N}KdS=\mathbf{0.}\tag{11.26}
Meanwhile, the companion formula reads
SRNKdS=12SBααdS.(11.27)\int_{S}\mathbf{R}\cdot\mathbf{N}KdS=-\frac{1}{2}\int_{S}B_{\alpha}^{\alpha }dS.\tag{11.27}

11.3.1Conversion of geometric integrals to arithmetic integrals

In Chapter TBD of Introduction Tensor Calculus we described the concept of a geometric integral. Whether it is a volume integral
ΩFdΩ,(11.28)\int_{\Omega}Fd\Omega,\tag{11.28}
a surface integral
SFdS,(11.29)\int_{S}FdS,\tag{11.29}
or a line integral
LFdL,(11.30)\int_{L}FdL,\tag{11.30}
a geometric integral represents the additive total of an invariant quantity over a geometric domain. In the same Chapter, we described the evaluation of geometric integrals by a limiting procedure that involves subdividing the domain into ever small pieces and adding up the individual infinitesimal contributions. The main takeaway of the procedure is that, at least theoretically, geometric integrals can be evaluated by invariant means without a reference to a coordinate system.
On the other hand, for many practical as well as theoretical reasons, geometric integrals must be converted into arithmetic integrals which can be evaluated by the techniques of ordinary Calculus, such as the Fundamental Theorem of Calculus, or other means, such as numerical computation. Naturally, translation to an arithmetic integral becomes possible once the domain is referred to a coordinate system. As we stated in Chapter TBD of Introduction to Tensor Calculus, the volume integral
ΩFdΩ(11.31)\int_{\Omega}Fd\Omega\tag{11.31}
corresponds to the arithmetic integral
A3B3A2B2A1B1F(Z)ZdZ1dZ2dZ3,(11.32)\int_{A^{3}}^{B^{3}}\int_{A^{2}}^{B^{2}}\int_{A^{1}}^{B^{1}}F\left( Z\right) \sqrt{Z}dZ^{1}dZ^{2}dZ^{3},\tag{11.32}
where Z\sqrt{Z} is the volume element, the limits of integration reflect the domain, and it is further stipulated that each lower limit is less than the corresponding limit, i.e.
A1<B1A2<B2, and A3<B3.(11.33)A_{1} \lt B_{1}\text{, }A_{2} \lt B_{2}\text{, and }A_{3} \lt B_{3}.\tag{11.33}
Correspondingly, for surface and line integrals, we have
SFdS=A2B2A1B1F(S)SdS1dS2(11.34)\int_{S}FdS=\int_{A^{2}}^{B^{2}}\int_{A^{1}}^{B^{1}}F\left( S\right) \sqrt{S}dS^{1}dS^{2}\tag{11.34}
and
LFdL=A1B1F(L)LdL1,(11.35)\int_{L}FdL=\int_{A^{1}}^{B^{1}}F\left( L\right) \sqrt{L}dL^{1},\tag{11.35}
with the same stipulation regarding the integration limits. In order for these conversions to be valid, however, it must be demonstrated that the arithmetic integrals are invariant with respect to coordinate changes. This will be one of the tasks accomplished in the next Section.
For an example of conversion from a geometric to an arithmetic integral, consider the classical calculation of the volume VV of a sphere of radius RR. As a geometric integral, VV is given by the formula
V=Ω1dΩ.(11.36)V=\int_{\Omega}1d\Omega.\tag{11.36}
In Cartesian coordinates x,y,zx,y,z, the volume element Z\sqrt{Z} is given by
Z=1(11.37)\sqrt{Z}=1\tag{11.37}
and therefore the corresponding arithmetic integral reads
V=RRR2z2R2z2R2y2z2R2y2z21dxdydz.(11.38)V=\int_{-R}^{R}\int_{-\sqrt{R^{2}-z^{2}}}^{\sqrt{R^{2}-z^{2}}}\int _{-\sqrt{R^{2}-y^{2}-z^{2}}}^{\sqrt{R^{2}-y^{2}-z^{2}}}1dxdydz.\tag{11.38}
In spherical coordinates r,θ,φr,\theta,\varphi, on the other hand, the expression for the volume element Z\sqrt{Z} is
Z=r2sinθ(11.39)\sqrt{Z}=r^{2}\sin\theta\tag{11.39}
and therefore the corresponding arithmetic integral reads
V=02π0π0Rr2sinθdrdθdφ.(11.40)V=\int_{0}^{2\pi}\int_{0}^{\pi}\int_{0}^{R}r^{2}\sin\theta drd\theta d\varphi.\tag{11.40}
Both integrals evaluate to
V=43πR3(11.41)V=\frac{4}{3}\pi R^{3}\tag{11.41}
consistent with the expected invariance of the arithmetic integral with respect to coordinate changes. The latter integral, however, is much easier to evaluate which illustrates the benefit of choosing a coordinate system that is suited to a specific task.

11.3.2Invariance of arithmetic integrals under a change of coordinates

The argument presented in this Section relies on the change-of-variables theorem from Multivariable Calculus. Our goal is to show that the two arithmetic integrals
A3B3A2B2A1B1F(Z)ZdZ1dZ2dZ3(11.42)\int_{A^{3}}^{B^{3}}\int_{A^{2}}^{B^{2}}\int_{A^{1}}^{B^{1}}F\left( Z\right) \sqrt{Z}dZ^{1}dZ^{2}dZ^{3}\tag{11.42}
and
A3B3A2B2A1B1F(Z)ZdZ1dZ2dZ3,(11.43)\int_{A^{3^{\prime}}}^{B^{3^{\prime}}}\int_{A^{2^{\prime}}}^{B^{2^{\prime}} }\int_{A^{1^{\prime}}}^{B^{1^{\prime}}}F\left( Z^{\prime}\right) \sqrt{Z^{\prime}}dZ^{1^{\prime}}dZ^{2^{\prime}}dZ^{3^{\prime}},\tag{11.43}
constructed according to the algorithm described above for two alternative coordinate systems ZiZ^{i} and ZiZ^{i^{\prime}}, are equal.
Recall that according to the change-of-variables theorem, the integral
A3B3A2B2A1B1g(Z)dZ1dZ2dZ3(11.44)\int_{A^{3}}^{B^{3}}\int_{A^{2}}^{B^{2}}\int_{A^{1}}^{B^{1}}g\left( Z\right) dZ^{1}dZ^{2}dZ^{3}\tag{11.44}
for a function g(Z)g\left( Z\right) in coordinates ZiZ^{i} can be transformed to an equivalent integral in coordinates ZiZ^{i^{\prime}} by implementing three changes: 1. substituting the change of variables Zi(Z)Z^{i}\left( Z^{\prime}\right) for the variables in the function g(Z)g\left( Z\right) , 2. introducing a factor of det1J\det^{-1}J, where JJ is the matrix representing the Jacobian JiiJ_{i^{\prime}}^{i}, and 3. appropriately adjusting the limits of integration. These three steps are summarized by the formula
A3B3A2B2A1B1g(Z)dZ1dZ2dZ3                =A3B3A2B2A1B1g(Z)det1JdZ1dZ2dZ3.          (11.45)\begin{aligned}& \hspace{-0.4in}\int_{A^{3}}^{B^{3}}\int_{A^{2}}^{B^{2}}\int_{A^{1}}^{B^{1} }g\left( Z\right) dZ^{1}dZ^{2}dZ^{3}\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ = \int_{A^{3^{\prime}}}^{B^{3^{\prime}}}\int_{A^{2^{\prime}}}^{B^{2^{\prime}} }\int_{A^{1^{\prime}}}^{B^{1^{\prime}}}g\left( Z^{\prime}\right) \det\nolimits^{-1}JdZ^{1^{\prime}}dZ^{2^{\prime}}dZ^{3^{\prime}}.\ \ \ \ \ \ \ \ \ \ \left(11.45\right)\end{aligned}
When we apply this formula to the integral
A3B3A2B2A1B1F(Z)ZdZ1dZ2dZ3(11.46)\int_{A^{3}}^{B^{3}}\int_{A^{2}}^{B^{2}}\int_{A^{1}}^{B^{1}}F\left( Z\right) \sqrt{Z}dZ^{1}dZ^{2}dZ^{3}\tag{11.46}
we find
A3B3A2B2A1B1F(Z)ZdZ1dZ2dZ3                =A3B3A2B2A1B1F(Z(Z))ZJ1dZ1dZ2dZ3          (11.47)\begin{aligned}& \hspace{-0.4in}\int_{A^{3}}^{B^{3}}\int_{A^{2}}^{B^{2}}\int_{A^{1}}^{B^{1} }F\left( Z\right) \sqrt{Z}dZ^{1}dZ^{2}dZ^{3}\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ = \int_{A^{3^{\prime}}}^{B^{3^{\prime}}}\int_{A^{2^{\prime}}}^{B^{2^{\prime}} }\int_{A^{1^{\prime}}}^{B^{1^{\prime}}}F\left( Z\left( Z^{\prime}\right) \right) \sqrt{Z}J^{-1}dZ^{1^{\prime}}dZ^{2^{\prime}}dZ^{3^{\prime}}\ \ \ \ \ \ \ \ \ \ \left(11.47\right)\end{aligned}
Of course, the composition F(Z(Z))F\left( Z\left( Z^{\prime}\right) \right) is precisely F(Z)F\left( Z^{\prime}\right) , i.e. the field FF as a function of the primed coordinates ZiZ^{i^{\prime}}. Also, recall from Section TBD of Introduction to Tensor Calculus that the volume element Z\sqrt{Z} transforms as a relative invariant of weight 1-1, i.e.
Z=J1Z.(11.48)\sqrt{Z^{\prime}}=J^{-1}\sqrt{Z}.\tag{11.48}
Thus, the combination F(Z(Z))ZJ1F\left( Z\left( Z^{\prime}\right) \right) \sqrt {Z}J^{-1} equals F(Z)ZF\left( Z^{\prime}\right) \sqrt{Z^{\prime}} and we have
A3B3A2B2A1B1F(Z)ZdZ1dZ2dZ3                =A3B3A2B2A1B1F(Z)ZdZ1dZ2dZ3,          (11.49)\begin{aligned}& \hspace{-0.4in}\int_{A^{3}}^{B^{3}}\int_{A^{2}}^{B^{2}}\int_{A^{1}}^{B^{1} }F\left( Z\right) \sqrt{Z}dZ^{1}dZ^{2}dZ^{3}\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ = \int_{A^{3^{\prime}}}^{B^{3^{\prime}}}\int_{A^{2^{\prime}}}^{B^{2^{\prime}} }\int_{A^{1^{\prime}}}^{B^{1^{\prime}}}F\left( Z^{\prime}\right) \sqrt{Z^{\prime}}dZ^{1^{\prime}}dZ^{2^{\prime}}dZ^{3^{\prime}},\ \ \ \ \ \ \ \ \ \ \left(11.49\right)\end{aligned}
as we set out to show.
We will prove the divergence theorem in two steps. In this Section, we will demonstrate the "arithmetic" version of the divergence theorem
SˉˉαTαdSˉ=LˉnˉαTαdLˉ,(11.50)\int_{\bar{S}}\bar{\nabla}_{\alpha}T^{\alpha}d\bar{S}=\int_{\bar{L}}\bar {n}_{\alpha}T^{\alpha}d\bar{L},\tag{11.50}
for a tensor field TαT^{\alpha} over a planar domain Sˉ\bar{S} with boundary Lˉ\bar{L} referred to Cartesian coordinates xx and yy. Although the domain Sˉ\bar{S} and its boundary Lˉ\bar{L} need not be the arithmetic representation of some curved domain SS with boundary LL, we chose to use the bar accent to highlight the Cartesian nature of the present discussion. Note that
ˉαTα=T1x+T2y(11.51)\bar{\nabla}_{\alpha}T^{\alpha}=\frac{\partial T^{1}}{\partial x} +\frac{\partial T^{2}}{\partial y}\tag{11.51}
and
nˉαTα=nˉ1T1+nˉ2T2.(11.52)\bar{n}_{\alpha}T^{\alpha}=\bar{n}_{1}T^{1}+\bar{n}_{2}T^{2}.\tag{11.52}
Therefore, in the unpacked form, the arithmetic divergence theorem reads
Sˉ(T1x+T2y)dSˉ=Lˉ(nˉ1T1+nˉ2T2)dLˉ.(11.53)\int_{\bar{S}}\left( \frac{\partial T^{1}}{\partial x}+\frac{\partial T^{2} }{\partial y}\right) d\bar{S}=\int_{\bar{L}}\left( \bar{n}_{1}T^{1}+\bar {n}_{2}T^{2}\right) d\bar{L}.\tag{11.53}
Once we prove the arithmetic version of the divergence theorem, we will prove the general divergence theorem
SαTαdS=LnαTαdL(11.7)\int_{S}\nabla_{\alpha}T^{\alpha}dS=\int_{L}n_{\alpha}T^{\alpha}dL \tag{11.7}
by reducing it to its arithmetic version
SˉˉαTαdSˉ=LˉnˉαTαdLˉ.(11.50)\int_{\bar{S}}\bar{\nabla}_{\alpha}T^{\alpha}d\bar{S}=\int_{\bar{L}}\bar {n}_{\alpha}T^{\alpha}d\bar{L}. \tag{11.50}

11.4.1The arithmetic space

In Chapter TBD of Introduction to Tensor Calculus, we defined the arithmetic space associated with a Riemannian space as a Cartesian visualization of the coordinate system in a Euclidean space. For instance, for a two-dimensional surface referred to surface coordinates SαS^{\alpha}, the arithmetic space imagines the coordinates S1S^{1} and S2S^{2} as Cartesian coordinates in the plane.
For a specific example, consider a sphere of radius RR referred to the standard spherical coordinates θ\theta and φ\varphi. The corresponding arithmetic space occupies a π×2π\pi\times2\pi rectangle in the plane, as illustrated in the following figure.
  (11.54)
Furthermore, to any surface curve described by the equations
Sα=Sα(L),(11.55)S^{\alpha}=S^{\alpha}\left( L\right) ,\tag{11.55}
there corresponds a curve in the arithmetic space described by the same equations. The following figure shows an example of a curve on a sphere along with its arithmetic counterpart.
  (11.56)
Entirely unsurprisingly, the two shapes are completely different.
In the upcoming demonstration of the divergence theorem, we will use a generic curved patch illustrated in the following figure along with its arithmetic representation.
  (11.57)
The fascinating aspect of the argument that we are about to present is that the geometry of the arithmetic representation will take on central relevance. We will use the bar accent above the symbol to denote the geometric objects in the arithmetic space. Thus, the domain SS corresponds to the arithmetic domain Sˉ\bar{S} and its boundary LL corresponds to the curve Lˉ\bar{L}. The shape of the curve Lˉ\bar{L} in the arithmetic space will give rise to the normal field nˉ\mathbf{\bar{n}}. And although we are about to show that the components nαn^{\alpha} and nˉα\bar{n}^{\alpha} are related, there is no reason whatsoever to expect that nα=nˉαn^{\alpha}=\bar{n}^{\alpha}.
While the curves LL and Lˉ\bar{L} live in completely different spaces, they are, by construction, described by the same equations
Sα=Sα(L).(11.58)S^{\alpha}=S^{\alpha}\left( L\right) .\tag{11.58}
Therefore, their respective shift tensors
SΦα=Sα(L)LΦ(11.59)S_{\Phi}^{\alpha}=\frac{\partial S^{\alpha}\left( L\right) }{\partial L^{\Phi}}\tag{11.59}
are identical as well.
On the other hand, the area elements S\sqrt{S} and Sˉ\sqrt{\bar{S}} are different, as are the line elements L\sqrt{L} and Lˉ\sqrt{\bar{L}}. Note that since the coordinates S1S^{1} and S2S^{2} play the role of Cartesian coordinates in arithmetic space, we have
Sˉ=1.(11.60)\sqrt{\bar{S}}=1.\tag{11.60}
We are now in a position to relate the components nαn^{\alpha} of the geodesic normal n\mathbf{n} to the original curve LL and the components nˉα\bar {n}^{\alpha} of the normal nˉ\mathbf{\bar{n}} to the arithmetic curve Lˉ\bar{L}. Recall that these components are given by the equations
nα=εαβεΦSΦα(11.61)n_{\alpha}=\varepsilon_{\alpha\beta}\varepsilon^{\Phi}S_{\Phi}^{\alpha}\tag{11.61}
and
nˉα=εˉαβεˉΦSΦα,(11.62)\bar{n}_{\alpha}=\bar{\varepsilon}_{\alpha\beta}\bar{\varepsilon}^{\Phi }S_{\Phi}^{\alpha},\tag{11.62}
where we once again point out that the shift tensor SΦαS_{\Phi}^{\alpha} is the same for both curves. Expressing the Levi-Civita symbols in terms of the corresponding permutation systems eαβe_{\alpha\beta} and eΦe^{\Phi}, we find
nα=SeαβeΦLSΦα          (11.63)nˉα=SˉeαβeΦLˉSΦα.          (11.64)\begin{aligned}n_{\alpha} & =\sqrt{S}e_{\alpha\beta}\frac{e^{\Phi}}{\sqrt{L}}S_{\Phi }^{\alpha}\ \ \ \ \ \ \ \ \ \ \left(11.63\right)\\\bar{n}_{\alpha} & =\sqrt{\bar{S}}e_{\alpha\beta}\frac{e^{\Phi}}{\sqrt {\bar{L}}}S_{\Phi}^{\alpha}.\ \ \ \ \ \ \ \ \ \ \left(11.64\right)\end{aligned}
Thus,
n~αLˉSˉ=eαβeΦSΦα=nαLS.(11.65)\tilde{n}_{\alpha}\frac{\sqrt{\bar{L}}}{\sqrt{\bar{S}}}=e_{\alpha\beta} e^{\Phi}S_{\Phi}^{\alpha}=n_{\alpha}\frac{\sqrt{L}}{\sqrt{S}}.\tag{11.65}
and therefore
nˉα=SˉLSLˉnα.(11.66)\bar{n}_{\alpha}=\frac{\sqrt{\bar{S}}\sqrt{L}}{\sqrt{S}\sqrt{\bar{L}} }n_{\alpha}.\tag{11.66}
Finally, since
we arrive at the formula
nˉα=LSLˉnα(11.67)\bar{n}_{\alpha}=\frac{\sqrt{L}}{\sqrt{S}\sqrt{\bar{L}}}n_{\alpha}\tag{11.67}
which will be used below to bridge the divergence theorem to its arithmetic analogue.

11.4.2Useful extensions of the Fundamental Theorem of Calculus

The Fundamental Theorem of Calculus tells us that the operations of integration and differentiation are the inverses of each other. The equation
abf(ξ)dξ=F(b)F(a)(11.1)\int_{a}^{b}f\left( \xi\right) d\xi=F\left( b\right) -F\left( a\right) \tag{11.1}
can be seen as the "integral of the derivative" form of the theorem. To obtain the "derivative of the integral form", allow the upper limit of the integral to vary, i.e.
axf(ξ)dξ=F(x)F(a),(11.68)\int_{a}^{x}f\left( \xi\right) d\xi=F\left( x\right) -F\left( a\right) ,\tag{11.68}
and differentiate both sides with respect to xx, i.e.
ddx(axf(ξ)dξ)=f(x)(11.69)\frac{d}{dx}\left( \int_{a}^{x}f\left( \xi\right) d\xi\right) =f\left( x\right)\tag{11.69}
It is this "derivative of the integral" form, along with its straightforward extensions we are about to describe, that will be of greater to use to us in our current discussion.
First, allow the upper limit to be a general function y(x)y\left( x\right) of xx. Then, by the chain rule, we have
ddx(ay(x)f(ξ)dξ)=f(y(x))y(x).(11.70)\frac{d}{dx}\left( \int_{a}^{y\left( x\right) }f\left( \xi\right) d\xi\right) =f\left( y\left( x\right) \right) y^{\prime}\left( x\right) .\tag{11.70}
It is left as an exercise to show that the corresponding formula for a variable lower limit reads
ddx(y(x)bf(ξ)dξ)=f(y(x))y(x).(11.71)\frac{d}{dx}\left( \int_{y\left( x\right) }^{b}f\left( \xi\right) d\xi\right) =-f\left( y\left( x\right) \right) y^{\prime}\left( x\right) .\tag{11.71}
Finally, suppose that the variable xx also appears as a parameter in the integrand, i.e.
abf(x,ξ)dξ.(11.72)\int_{a}^{b}f\left( x,\xi\right) d\xi.\tag{11.72}
Then the integral is once again a function of xx and can therefore be differentiated with respect to xx. Since an integral is essentially a sum, it is not surprising that in order to differentiate the integral we must differentiate the integrand, i.e.
ddx(abf(x,ξ)dξ)=abf(x,ξ)xdξ.(11.73)\frac{d}{dx}\left( \int_{a}^{b}f\left( x,\xi\right) d\xi\right) =\int _{a}^{b}\frac{\partial f\left( x,\xi\right) }{\partial x}d\xi.\tag{11.73}
In summary, let us combine the three possible ways in which the integral can depend on the variable xx in a single equation, i.e.
ddx(y1(x)y2(x)f(x,ξ)dξ)=y1(x)y2(x)f(x,ξ)xdξ                +f(x,y2(x))y2(x)f(x,y1(x))y1(x).          (11.74)\begin{aligned}\frac{d}{dx}\left( \int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }f\left( x,\xi\right) d\xi\right) & =\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }\frac{\partial f\left( x,\xi\right) }{\partial x}d\xi\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ +f\left( x,y_{2}\left( x\right) \right) y_{2}^{\prime }\left( x\right) -f\left( x,y_{1}\left( x\right) \right) y_{1}^{\prime }\left( x\right) .\ \ \ \ \ \ \ \ \ \ \left(11.74\right)\end{aligned}

11.4.3The fundamental elements of planar curves given by explicit equations

Finally, our proof of the arithmetic divergence theorem will require expressions for the length element LL and the normal components nan^{a} for a curve given by an explicit function
y=y(x)(11.75)y=y\left( x\right)\tag{11.75}
in Cartesian coordinates. Recall the equations from Chapter 4
Lˉ=1+yx2          (11.76)[nˉα]=11+yx2[yx1],          (11.77)\begin{aligned}\sqrt{\bar{L}} & =\sqrt{1+y_{x}^{2}}\ \ \ \ \ \ \ \ \ \ \left(11.76\right)\\\left[ \bar{n}^{\alpha}\right] & =\frac{1}{\sqrt{1+y_{x}^{2}}}\left[ \begin{array} {r} -y_{x}\\ 1 \end{array} \right] ,\ \ \ \ \ \ \ \ \ \ \left(11.77\right)\end{aligned}
where we switched from SS to Lˉ\bar{L} and from NiN^{i} to nˉα\bar{n}^{\alpha} to fit the current context. Note that the components of nˉα\bar{n}^{\alpha} were chosen so that they correspond to the "upward" normal.
Given the expression for Lˉ\bar{L}, the line integral
LˉFdLˉ(11.78)\int_{\bar{L}}Fd\bar{L}\tag{11.78}
in arithmetic form reads
LFdL=abF(γ)1+y(γ)2dγ.(11.79)\int_{L}FdL=\int_{a}^{b}F\left( \gamma\right) \sqrt{1+y^{\prime}\left( \gamma\right) ^{2}}d\gamma.\tag{11.79}

11.4.4The demonstration

Our argument will be limited to two-dimensional domains that correspond to a region between two functions y1(x)y_{1}\left( x\right) and y2(x)y_{2}\left( x\right) , as illustrated in the following figure.
(11.80)
Note that along the top potion of the curve, the exterior normal points up, while along the bottom portion of the curve, the exterior normal points down.
(11.81)
In the previous Section, we gave an expression for the "upward" normal. However, on the bottom portion of the curve described by y1(x)y_{1}\left( x\right) , the outward normal points downwards and we must therefore adjust our expressions. We have
[nˉα]=[nˉα]={11+y1(x)2[y1(x)1] along the bottom 11+y2(x)2[y2(x)1] along the top.(11.82)\left[ \bar{n}_{\alpha}\right] =\left[ \bar{n}^{\alpha}\right] =\left\{ \begin{array} {l} \frac{1}{\sqrt{1+y_{1}^{\prime}\left( x\right) ^{2}}}\left[ \begin{array} {c} -y_{1}^{\prime}\left( x\right) \\ 1 \end{array} \right] \text{ along the bottom }\\ \frac{1}{\sqrt{1+y_{2}^{\prime}\left( x\right) ^{2}}}\left[ \begin{array} {c} \phantom{-} y_{2}^{\prime}\left( x\right) \\ -1 \end{array} \right] \text{ along the top.} \end{array} \right.\tag{11.82}
Denote the elements of the tensor field TαT^{\alpha} by GG and HH, i.e.
[Tα]=[GH].(11.83)\left[ T^{\alpha}\right] =\left[ \begin{array} {c} G\\ H \end{array} \right] .\tag{11.83}
Then the divergence αTα\nabla_{\alpha}T^{\alpha} of TαT^{\alpha} is given by
αTα=Gx+Hy(11.84)\nabla_{\alpha}T^{\alpha}=\frac{\partial G}{\partial x}+\frac{\partial H}{\partial y}\tag{11.84}
and the volume integral of αTα\nabla_{\alpha}T^{\alpha} is given by the repeated integral
SˉαTαdSˉ=aby1(x)y2(x)(Gx+Hy)dydx.(11.85)\int_{\bar{S}}\nabla_{\alpha}T^{\alpha}d\bar{S}=\int_{a}^{b}\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }\left( \frac{\partial G}{\partial x}+\frac{\partial H}{\partial y}\right) dydx.\tag{11.85}
Breaking the repeated integral on the right up into two, we have
SˉαTαdSˉ= aby1(x)y2(x)GxdydxI1+aby1(x) y2(x) HydydxI2.(11.86)\int_{\bar{S}}\nabla_{\alpha}T^{\alpha}d\bar{S}=~\underset{I_{1}} {\underbrace{\int_{a}^{b}\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }\frac{\partial G}{\partial x}dydx}}+\underset{I_{2}}{\underbrace {\int_{a}^{b}\int_{y_{1}\left( x\right) \ }^{y_{2}\left( x\right) \ } \frac{\partial H}{\partial y}dydx}}.\tag{11.86}
We will now analyze each repeated integral individually. However, for both integrals, the key step involves an application of the Fundamental Theorem of Calculus to the "inner" integral, i.e.
i1=y1(x)y2(x)Gxdy(11.87)i_{1}=\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }\frac{\partial G}{\partial x}dy\tag{11.87}
in the case of I1I_{1} and
i2=y1(x) y2(x) Hydy(11.88)i_{2}=\int_{y_{1}\left( x\right) \ }^{y_{2}\left( x\right) \ } \frac{\partial H}{\partial y}dy\tag{11.88}
in the case of I2I_{2}. For each fixed value of xx, the integration in the inner integrals takes place along the vertical interval from y1(x)y_{1}\left( x\right) to y2(x)y_{2}\left( x\right) and reduces the integral to the difference of two values corresponding to the two ends of the integration intervals.
(11.89)
As a result, the "outer" integrals represent sums of combinations involving the boundary values of GG and HH as well as the derivatives of y1(x)y_{1}^{\prime}\left( x\right) and y2(x)y_{2}^{\prime}\left( x\right) and thus can eventually be converted into line integrals over the boundary Lˉ\bar{L}. This shows how the Fundamental Theorem of Calculus reduces a domain integral to a boundary integral and demonstrates why the divergence theorem may be considered a direct consequence of the Fundamental Theorem of Calculus.

11.4.5Analysis of I1I_{1}

We begin with the integral
I1=aby1(x)y2(x)Gxdydx.(11.90)I_{1}=\int_{a}^{b}\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }\frac{\partial G}{\partial x}dydx.\tag{11.90}
Consider the inner integral
i1=y1(x)y2(x)Gxdy(11.87)i_{1}=\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }\frac{\partial G}{\partial x}dy \tag{11.87}
and notice that this integral can be related to
ddxy1(x)y2(x)G(x,y)dyˉ(11.91)\frac{d}{dx}\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }G\left( x,y\right) d\bar{y}\tag{11.91}
with the help of the extension of the Fundamental Theorem of Calculus derived earlier and captured by the equation
ddx(y1(x)y2(x)f(x,ξ)dξ)=y1(x)y2(x)f(x,ξ)xdξ                +f(x,y2(x))y2(x)f(x,y1(x))y1(x).          (11.74)\begin{aligned}\frac{d}{dx}\left( \int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }f\left( x,\xi\right) d\xi\right) & =\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }\frac{\partial f\left( x,\xi\right) }{\partial x}d\xi\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ +f\left( x,y_{2}\left( x\right) \right) y_{2}^{\prime }\left( x\right) -f\left( x,y_{1}\left( x\right) \right) y_{1}^{\prime }\left( x\right) . \ \ \ \ \ \ \ \ \ \ \left(11.74\right)\end{aligned}
Substituting G(x,y)G\left( x,y\right) for f(x,ξ)f\left( x,\xi\right) , we find
ddx(y1(x)y2(x)G(x,y)dy)=y1(x)y2(x)Gxdy                 +G(x,y2(x))y2(x)G(x,y1(x))y1(x).          (11.92)\begin{aligned}\frac{d}{dx}\left( \int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }G\left( x,y\right) dy\right) & =\int_{y_{1}\left( x\right) } ^{y_{2}\left( x\right) }\frac{\partial G}{\partial x}dy\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ \ +G\left( x,y_{2}\left( x\right) \right) y_{2}^{\prime }\left( x\right) -G\left( x,y_{1}\left( x\right) \right) y_{1}^{\prime }\left( x\right) .\ \ \ \ \ \ \ \ \ \ \left(11.92\right)\end{aligned}
Thus,
i1=y1(x)y2(x)Gxdy=ddx(y1(x)y2(x)G(x,y)dy)                             +G(x,y1(x))y1(x)G(x,y2(x))y2(x).          (11.93)\begin{aligned}i_{1} & =\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) } \frac{\partial G}{\partial x}dy=\frac{d}{dx}\left( \int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }G\left( x,y\right) dy\right)\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ +G\left( x,y_{1}\left( x\right) \right) y_{1}^{\prime}\left( x\right) -G\left( x,y_{2}\left( x\right) \right) y_{2}^{\prime}\left( x\right) .\ \ \ \ \ \ \ \ \ \ \left(11.93\right)\end{aligned}
Now, recall that
I1=abi1dx(11.94)I_{1}=\int_{a}^{b}i_{1}dx\tag{11.94}
and note that, by the Fundamental Theorem of Calculus,
aβddx(y1(x)y2(x)G(x,y)dy)dx          (11.95)      =y1(x) y2(x) G(x,y)dyx=by1(x) y2(x) G(x,y)dyx=a,          (11.96)\begin{aligned}& \hspace{-0.4in}\int_{a}^{\beta}\frac{d}{dx}\left( \int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }G\left( x,y\right) dy\right) dx\ \ \ \ \ \ \ \ \ \ \left(11.95\right)\\& \ \ \ \ \ \ = \left. \int_{y_{1}\left( x\right) \ }^{y_{2}\left( x\right) \ }G\left( x,y\right) dy\right\vert _{x=b}-\left. \int_{y_{1}\left( x\right) \ }^{y_{2}\left( x\right) \ }G\left( x,y\right) dy\right\vert _{x=a},\ \ \ \ \ \ \ \ \ \ \left(11.96\right)\end{aligned}
and each integral on the right vanishes since
y1(a)=y2(a)   and   y1(b)=y2(b)(11.97)y_{1}\left( a\right) =y_{2}\left( a\right) \text{ \ \ and \ \ } y_{1}\left( b\right) =y_{2}\left( b\right)\tag{11.97}
and therefore the lower and the upper limits for each integral coincide.
Consequently, the final expression for I1I_{1} reads
I1=abG(x,y1(x))y1(x)dxaβG(x,y2(x))y2(x)dx.(11.98)I_{1}=\int_{a}^{b}G\left( x,y_{1}\left( x\right) \right) y_{1}^{\prime }\left( x\right) dx-\int_{a}^{\beta}G\left( x,y_{2}\left( x\right) \right) y_{2}^{\prime}\left( x\right) dx.\tag{11.98}
We will now turn our attention to the integral I2I_{2}.

11.4.6Analysis of I2I_{2}

The analysis of
I2=aby1(x) y2(x) Hydydx(11.99)I_{2}=\int_{a}^{b}\int_{y_{1}\left( x\right) \ }^{y_{2}\left( x\right) \ }\frac{\partial H}{\partial y}dydx\tag{11.99}
is far simpler than that of I1I_{1} since the inner integral
y1(x) y2(x) Hydy(11.88)\int_{y_{1}\left( x\right) \ }^{y_{2}\left( x\right) \ }\frac{\partial H}{\partial y}dy \tag{11.88}
is tailor-made for an application of the Fundamental Theorem of Calculus. Indeed,
y1(x)y2(x)Hydy=H(x,y2(x))H(x,y1(x)).(11.100)\int_{y_{1}\left( x\right) }^{y_{2}\left( x\right) }\frac{\partial H}{\partial y}dy=H\left( x,y_{2}\left( x\right) \right) -H\left( x,y_{1}\left( x\right) \right) .\tag{11.100}
Therefore,
I2=abH(x,y2(x))dxabH(x,y1(x))dx.(11.101)I_{2}=\int_{a}^{b}H\left( x,y_{2}\left( x\right) \right) dx-\int_{a} ^{b}H\left( x,y_{1}\left( x\right) \right) dx.\tag{11.101}

11.4.7Combining I1I_{1}and I2I_{2}

Combining the two integrals and grouping together the terms involving y1(x)y_{1}\left( x\right) and those involving y2(x)y_{2}\left( x\right) , we find
SˉαTαdSˉ=ab(G(x,y1(x))y1(x)H(x,y1(x)))dx                   +ab(G(x,y2(x))y2(x)+H(x,y2(x)))dx          (11.102)\begin{aligned}\int_{\bar{S}}\nabla_{\alpha}T^{\alpha}d\bar{S} & =\int_{a}^{b}\left( \rule{0pt}{12pt}G\left( x,y_{1}\left( x\right) \right) y_{1}^{\prime }\left( x\right) -H\left( x,y_{1}\left( x\right) \right) \right) dx\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ \ \ \ +\int_{a}^{b}\left( \rule{0pt}{12pt}-G\left( x,y_{2}\left( x\right) \right) y_{2}^{\prime}\left( x\right) +H\left( x,y_{2}\left( x\right) \right) \right) dx\ \ \ \ \ \ \ \ \ \ \left(11.102\right)\end{aligned}
We can rewrite the integrand of each integral as a dot product, i.e.
SˉαTαdSˉ=ab[G(x,y1(x))H(x,y1(x))][y1(x)1]dx                 +ab[G(x,y2(x))H(x,y2(x))][y2(x)1]dx          (11.103)\begin{aligned}\int_{\bar{S}}\nabla_{\alpha}T^{\alpha}d\bar{S} & =\int_{a}^{b}\left[ \begin{array} {c} G\left( x,y_{1}\left( x\right) \right) \\ H\left( x,y_{1}\left( x\right) \right) \end{array} \right] \cdot\left[ \begin{array} {c} y_{1}^{\prime}\left( x\right) \\ -1 \end{array} \right] dx\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ \ +\int_{a}^{b}\left[ \begin{array} {c} G\left( x,y_{2}\left( x\right) \right) \\ H\left( x,y_{2}\left( x\right) \right) \end{array} \right] \cdot\left[ \begin{array} {c} -y_{2}^{\prime}\left( x\right) \\ 1 \end{array} \right] dx\ \ \ \ \ \ \ \ \ \ \left(11.103\right)\end{aligned}
Note the objects
[y1(x)1]    and    [y2(x)1](11.104)\left[ \begin{array} {c} y_{1}^{\prime}\left( x\right) \\ -1 \end{array} \right] \text{\ \ \ \ and \ \ \ }\left[ \begin{array} {c} -y_{2}^{\prime}\left( x\right) \\ 1 \end{array} \right]\tag{11.104}
are not quite the components nˉα\bar{n}^{\alpha} of the normal along Lˉ1\bar {L}_{1} and Lˉ2\bar{L}_{2}, since they are missing factors of
11+y1(x)2    and    11+y2(x)2.(11.105)\frac{1}{\sqrt{1+y_{1}^{\prime}\left( x\right) ^{2}}}\text{\ \ \ \ and \ \ \ }\frac{1}{\sqrt{1+y_{2}^{\prime}\left( x\right) ^{2}}}.\tag{11.105}
Similarly, the two integrals above do not quite represent line integrals over Lˉ1\bar{L}_{1} and Lˉ2\bar{L}_{2} since they are missing the requisite factors of
1+y1(x)2    and    1+y2(x)2.(11.106)\sqrt{1+y_{1}^{\prime}\left( x\right) ^{2}}\text{\ \ \ \ and \ \ \ } \sqrt{1+y_{2}^{\prime}\left( x\right) ^{2}}.\tag{11.106}
Clearly, the missing factors are the reciprocals of each other and therefore both problems can be easily remedied at the same time by writing the integrals in the form
SˉαTαdSˉ=ab[G(x,y1(x))H(x,y1(x))][y1(x)1+y1(x)211+y1(x)2]1+y1(x)2dx                 +ab[G(x,y2(x))H(x,y2(x))][y2(x)1+y2(x)211+y2(x)2]1+y2(x)2dx.          (11.107)\begin{aligned}\int_{\bar{S}}\nabla_{\alpha}T^{\alpha}d\bar{S} & =\int_{a}^{b}\left[ \begin{array} {c} G\left( x,y_{1}\left( x\right) \right) \\ H\left( x,y_{1}\left( x\right) \right) \end{array} \right] \cdot\left[ \begin{array} {c} \frac{y_{1}^{\prime}\left( x\right) }{\sqrt{1+y_{1}^{\prime}\left( x\right) ^{2}}}\\ -\frac{1}{\sqrt{1+y_{1}^{\prime}\left( x\right) ^{2}}} \end{array} \right] \sqrt{1+y_{1}^{\prime}\left( x\right) ^{2}}dx\ \ \ \ \ \ \ \ \ \ \\& \ \ \ \ \ \ \ +\int_{a}^{b}\left[ \begin{array} {c} G\left( x,y_{2}\left( x\right) \right) \\ H\left( x,y_{2}\left( x\right) \right) \end{array} \right] \cdot\left[ \begin{array} {c} -\frac{y_{2}^{\prime}\left( x\right) }{\sqrt{1+y_{2}^{\prime}\left( x\right) ^{2}}}\\ \frac{1}{\sqrt{1+y_{2}^{\prime}\left( x\right) ^{2}}} \end{array} \right] \sqrt{1+y_{2}^{\prime}\left( x\right) ^{2}}dx.\ \ \ \ \ \ \ \ \ \ \left(11.107\right)\end{aligned}
We now readily recognize the first integrand as Lˉ1nˉαTαdLˉ\int_{\bar{L}_{1}}\bar {n}_{\alpha}T^{\alpha}d\bar{L} and the second integral as Lˉ2nˉαTαdLˉ\int_{\bar{L}_{2} }\bar{n}_{\alpha}T^{\alpha}d\bar{L}. Thus,
SˉˉαTαdSˉ=LˉnˉαTαdLˉ,(11.50)\int_{\bar{S}}\bar{\nabla}_{\alpha}T^{\alpha}d\bar{S}=\int_{\bar{L}}\bar {n}_{\alpha}T^{\alpha}d\bar{L}, \tag{11.50}
as we set out to prove.
We will now use the "arithmetic" divergence theorem to prove the general formulation
SαTαdS=LnαTαdL,(11.7)\int_{S}\nabla_{\alpha}T^{\alpha}dS=\int_{L}n_{\alpha}T^{\alpha}dL, \tag{11.7}
for a curved domain SS with boundary LL.
As step one, convert the volume integral to a repeated arithmetic integral, i.e.
SαTαdS=αTαSdS1dS2.(11.108)\int_{S}\nabla_{\alpha}T^{\alpha}dS=\int\int\nabla_{\alpha}T^{\alpha}\sqrt {S}dS^{1}dS^{2}.\tag{11.108}
Note that we have omitted the limits of integration for the repeated integrals and it is understood that the limits are chosen in such a way as to correctly describe the domain SS.
Recall that, according to the Voss-Weyl formula
αTα=1S(STα)Sα.(1.41)\nabla_{\alpha}T^{\alpha}=\frac{1}{\sqrt{S}}\frac{\partial\left( \sqrt {S}T^{\alpha}\right) }{\partial S^{\alpha}}. \tag{1.41}
Thus the combination αTαS\nabla_{\alpha}T^{\alpha}\sqrt{S} is given by
αTαS=(STα)Sα(11.109)\nabla_{\alpha}T^{\alpha}\sqrt{S}=\frac{\partial\left( \sqrt{S}T^{\alpha }\right) }{\partial S^{\alpha}}\tag{11.109}
and therefore
SαTαdS=(STα)SαdS1dS2.(11.110)\int_{S}\nabla_{\alpha}T^{\alpha}dS=\int\int\frac{\partial\left( \sqrt {S}T^{\alpha}\right) }{\partial S^{\alpha}}dS^{1}dS^{2}.\tag{11.110}
Notice that the integral on the right equals the integral
Sˉˉα(STα)dSˉ,(11.111)\int_{\bar{S}}\bar{\nabla}_{\alpha}\left( \sqrt{S}T^{\alpha}\right) d\bar {S},\tag{11.111}
since the "missing" factor of Sˉ\sqrt{\bar{S}} equals 11. Thus, by the arithmetic divergence theorem that we have just demonstrated, we have
SαTαdS=Sˉˉα(STα)dSˉ=L~nˉαTαSdLˉ.(11.112)\int_{S}\nabla_{\alpha}T^{\alpha}dS=\int_{\bar{S}}\bar{\nabla}_{\alpha}\left( \sqrt{S}T^{\alpha}\right) d\bar{S}=\int_{\tilde{L}}\bar{n}_{\alpha}T^{\alpha }\sqrt{S}d\bar{L}.\tag{11.112}
Let us now express the line integral on the right by the corresponding arithmetic integral, i.e.
S~nˉαTαZdLˉ=abnˉαTαSLˉdL1.(11.113)\int_{\tilde{S}}\bar{n}_{\alpha}T^{\alpha}\sqrt{Z}d\bar{L}=\int_{a}^{b}\bar {n}_{\alpha}T^{\alpha}\sqrt{S}\sqrt{\bar{L}}dL^{1}.\tag{11.113}
Recall that
n~α=nαLSL~.(11.67)\tilde{n}_{\alpha}=n_{\alpha}\frac{\sqrt{L}}{\sqrt{S}\sqrt{\tilde{L}}}. \tag{11.67}
Thus
abnˉαTαSLˉdL1=nαTαLdL1(11.114)\int_{a}^{b}\bar{n}_{\alpha}T^{\alpha}\sqrt{S}\sqrt{\bar{L}}dL^{1}=\int n_{\alpha}T^{\alpha}\sqrt{L}dL^{1}\tag{11.114}
which, of course, is the precisely arithmetic representation for the line integral
LnαTαdL.(11.115)\int_{L}n_{\alpha}T^{\alpha}dL.\tag{11.115}
In other words,
SαTαdS=LnαTαdL,(11.7)\int_{S}\nabla_{\alpha}T^{\alpha}dS=\int_{L}n_{\alpha}T^{\alpha}dL, \tag{11.7}
as we set out to show.
In order to demonstrate Stokes' theorem, introduce the unit tangent vector T\mathbf{T}. Its ambient components TiT_{i} are given by expression
Ti=εijkNjnαZαk(11.116)T_{i}=\varepsilon_{ijk}N^{j}n^{\alpha}Z_{\alpha}^{k}\tag{11.116}
The contour integral is given by
UFiTi dU=UFiεijkNjnαZαkdU,(11.117)\int_{U}F^{i}T_{i}\ dU=\int_{U}F^{i}\varepsilon_{ijk}N^{j}n^{\alpha}Z_{\alpha }^{k}dU,\tag{11.117}
where the integral on the right is immediately subject to Gauss's theorem:
UFiTi dU=Sα(FiεijkNjZαk)dS(11.118)\int_{U}F^{i}T_{i}\ dU=\int_{S}\nabla^{\alpha}\left( F^{i}\varepsilon _{ijk}N^{j}Z_{\alpha}^{k}\right) dS\tag{11.118}
Expand the integrand by the product rule
UFiTi dU=SαFiεijkNjZαk+FiεijkαNjZαk+FiεijkNjαZαkdS,(11.119)\int_{U}F^{i}T_{i}\ dU=\int_{S}\nabla^{\alpha}F^{i}\varepsilon_{ijk} N^{j}Z_{\alpha}^{k}+F^{i}\varepsilon_{ijk}\nabla^{\alpha}N^{j}Z_{\alpha} ^{k}+F^{i}\varepsilon_{ijk}N^{j}\nabla^{\alpha}Z_{\alpha}^{k}dS,\tag{11.119}
and apply the proper differential identity to each term
UFiTi dU=S(ZmαmFiεijkNjZαkFiεijkZβjBαβZαk+FiεijkNjNkBαα)dS.(11.120)\int_{U}F^{i}T_{i}\ dU=\int_{S}\left( Z_{m}^{\alpha}\nabla^{m}F^{i} \varepsilon_{ijk}N^{j}Z_{\alpha}^{k}-F^{i}\varepsilon_{ijk}Z_{\beta} ^{j}B^{\alpha\beta}Z_{\alpha}^{k}+F^{i}\varepsilon_{ijk}N^{j}N^{k}B_{\alpha }^{\alpha}\right) dS.\tag{11.120}
The second and the third terms vanish due to the skew-symmetry of the Levi-Civita symbol εijk\varepsilon_{ijk}. Thus, we are left with a single term
UFiTi dU=SmFiεijkNjZαkZmαdS.(11.121)\int_{U}F^{i}T_{i}\ dU=\int_{S}\nabla^{m}F^{i}\varepsilon_{ijk}N^{j}Z_{\alpha }^{k}Z_{m}^{\alpha}dS.\tag{11.121}
By the projection formula, we have
UFiTi dU=SmFiεijkNjδmkdSmFiεijkNjNkNmdS.(11.122)\int_{U}F^{i}T_{i}\ dU=\int_{S}\nabla^{m}F^{i}\varepsilon_{ijk}N^{j}\delta _{m}^{k}dS-\nabla^{m}F^{i}\varepsilon_{ijk}N^{j}N^{k}N_{m}dS.\tag{11.122}
The term with the three normals vanishes due to the skew-symmetry of εijk\varepsilon_{ijk} and the remaining term (with the indices rotated ijkii\rightarrow j\rightarrow k\rightarrow i) gives us precisely the statement of Stokes theorem
UFiTi dU=SεijkiFjNkdS, Q.E.D.(11.123)\int_{U}F^{i}T_{i}\ dU=\int_{S}\varepsilon_{ijk}\nabla^{i}F^{j}N^{k}dS\text{, Q.E.D.}\tag{11.123}
Exercise 11.1Show that the volume VV of the domain inside a closed surface SS is given by the equation
V=1nSRNdS,(11.23)V=\frac{1}{n}\int_{S}\mathbf{R}\cdot\mathbf{N}dS, \tag{11.23}
where R\mathbf{R} is the position vector, N\mathbf{N} is the outward normal and nn is the dimension of the ambient space.
Exercise 11.2Show that the area AA of a closed surface SS is given by the equation
A=1n1SRNBααdS,(11.24)A=-\frac{1}{n-1}\int_{S}\mathbf{R}\cdot\mathbf{N}B_{\alpha}^{\alpha}dS, \tag{11.24}
where R\mathbf{R} is the position vector, N\mathbf{N} is the outward normal, and nn is the dimension of the ambient space.
Exercise 11.3Show that the area AA of a non-closed surface SS with boundary LL is given by the equation
A=1n1(LRndLSRNBααdS),(11.25)A=\frac{1}{n-1}\left( \int_{L}\mathbf{R}\cdot\mathbf{n}dL-\int_{S} \mathbf{R}\cdot\mathbf{N}B_{\alpha}^{\alpha}dS\right) ,\tag{11.25}
where R\mathbf{R} is the position vector, N\mathbf{N} is the outward normal, n\mathbf{n} is the outward geodesic normal, and nn is the dimension of the ambient space.
Problem 11.1Show that for a two-dimensional closed surface SS,
SNKdS=0,(11.26)\int_{S}\mathbf{N}KdS=0, \tag{11.26}
where KK is the Gaussian curvature.
Problem 11.2Show that for a two-dimensional closed surface SS,
SRNKdS=12SBααdS.(11.27)\int_{S}\mathbf{R}\cdot\mathbf{N}KdS=-\frac{1}{2}\int_{S}B_{\alpha}^{\alpha }dS. \tag{11.27}
Exercise 11.4Show that the vector T\mathbf{T} whose components are given by
Ti=εijkNjnαZαk(11.116)T_{i}=\varepsilon_{ijk}N^{j}n^{\alpha}Z_{\alpha}^{k}\tag{11.116}
is indeed the unit tangent to the contour boundary. That is, T\mathbf{T} is unit length
TT=1,(11.124)\mathbf{T}\cdot\mathbf{T}=1,\tag{11.124}
orthogonal to the surface normal N\mathbf{N}
TN=0,(11.125)\mathbf{T}\cdot\mathbf{N}=0,\tag{11.125}
and the contour normal n\mathbf{n}
Tn=0.(11.126)\mathbf{T}\cdot\mathbf{n}=0.\tag{11.126}
Exercise 11.5Explain why the term εijkZβjZαkBαβ\varepsilon_{ijk}Z_{\beta}^{j}Z_{\alpha}^{k} B^{\alpha\beta} in the proof of Stokes' theorem vanishes.
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