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Lecture 13: Surface Integrals

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13.1 Surfaces for Surface Integral​

The idea that will lead to the concept of a surface integral is quite similar to that which led to a line integral. We say briefly 'surface' also for a portion of a surface, just as we said 'curve' for an arc of a curve, for simplicity. Representations of a surface SS in xyzxyz-space are

z=f(x,y)org(x,y,z)=0(1)z = f(x,y) \qquad \text{or} \qquad g(x,y,z) = 0 \qquad (1)

For example, z=+a2−x2−y2z = +\sqrt{a^2-x^2-y^2} or x2+y2+z2−a2=0x^2+y^2+z^2-a^2 = 0 (z≥0)(z \geq 0) represents hemisphere of radius aa and centre 0.

Now for curves CC in line integrals, it was more practical and gave greater flexibility to use a parametric representation r=r(t)\mathbf{r} = \mathbf{r}(t) where a≤t≤ba \leq t \leq b. This is a mapping of the interval a≤t≤ba \leq t \leq b located on the tt-axis, onto the curve CC in the xyzxyz-space. It maps every tt in that interval onto the point of CC with position vector r(t)\mathbf{r}(t) (see Figure 13.1)

Figure 13.1: Parametric representations of a curve and a surface

Figure 13.1: Parametric representations of a curve and a surface

Similarly, for surfaces SS in surface integrals, it will often be more practical to use a parametric representation. Surfaces are two-dimensional. Hence we need two parameters, which we call uu and vv. Thus a parametric representation of a surface SS in space is of the form

r(u,v)=[x(u,v),y(u,v),z(u,v)]=x(u,v) i+y(u,v) j+z(u,v) k(2)\mathbf{r}(u,v) = [x(u,v), y(u,v), z(u,v)] = x(u,v)\,\mathbf{i} + y(u,v)\,\mathbf{j} + z(u,v)\,\mathbf{k} \qquad (2)

when (u,v)(u,v) varies in some region RR of the uvuv-plane. This mapping (2) maps every point (u,v)(u,v) in RR onto the point of SS with position vector r(u,v)\mathbf{r}(u,v) (see Figure 13.1(B)).

Parametric Representation of a Cylinder​

The circular cylinder x2+y2=a2x^2+y^2 = a^2, −1≤z≤1-1 \leq z \leq 1, has radius aa, height 2, and the zz-axis as axis. A parametric representation is

r(u,v)=[acos⁡u,asin⁡u,v]=acos⁡u i+asin⁡u j+v k(3)\mathbf{r}(u,v) = [a\cos u, a\sin u, v] = a\cos u\,\mathbf{i} + a\sin u\,\mathbf{j} + v\,\mathbf{k} \qquad (3)

The components of r\mathbf{r} are x=acos⁡ux = a\cos u, y=asin⁡uy = a\sin u, z=vz = v. The parameters uu, vv vary in the rectangle RR: 0≤u≤2π0 \leq u \leq 2\pi, −1≤v≤1-1 \leq v \leq 1 in the uvuv-plane. The curves u=constu = \text{const} are vertical straight lines. The curves v=constv = \text{const} are parallel circles. The point PP in Figure 13.2 corresponds to u=π/3=60°u = \pi/3 = 60°, v=0.7v = 0.7.

Figure 13.2: Parametric representation of a cylinder

Figure 13.2: Parametric representation of a cylinder

Parametric Representation of a Sphere​

A sphere x2+y2+z2=a2x^2+y^2+z^2 = a^2 can be represented in the form

r(u,v)=acos⁡vcos⁡u i+acos⁡vsin⁡u j+asin⁡v k(4)\mathbf{r}(u,v) = a\cos v\cos u\,\mathbf{i} + a\cos v\sin u\,\mathbf{j} + a\sin v\,\mathbf{k} \qquad (4)

where the parameters uu, vv vary in the rectangle RR in the uvuv-plane given by the inequalities 0≤u≤2π0 \leq u \leq 2\pi, −π/2≤v≤π/2-\pi/2 \leq v \leq \pi/2. The components of r\mathbf{r} are

x=acos⁡vcos⁡u,y=acos⁡vsin⁡u,z=asin⁡vx = a\cos v\cos u, \qquad y = a\cos v\sin u, \qquad z = a\sin v

The curves u=constu = \text{const} and v=constv = \text{const} are the 'meridian' and 'parallels' on SS (as shown in Figure 13.3). This representation is used in geography for measuring the latitude and longitude of points on the globe. Another parametric representation of the sphere also used in mathematics is

r(u,v)=acos⁡usin⁡v i+asin⁡usin⁡v j+acos⁡v k(4∗)\mathbf{r}(u,v) = a\cos u\sin v\,\mathbf{i} + a\sin u\sin v\,\mathbf{j} + a\cos v\,\mathbf{k} \qquad (4^*)

where 0≤u≤2π0 \leq u \leq 2\pi, 0≤v≤π0 \leq v \leq \pi

Figure 13.3: Parametric representation of a sphere

Figure 13.3: Parametric representation of a sphere

Parametric Representation of a Cone​

A circular cone z=x2+y2z = \sqrt{x^2+y^2}, 0≤z≤H0 \leq z \leq H can be represented by

r(u,v)=[ucos⁡v,usin⁡v,u]=ucos⁡v i+usin⁡v j+u k(5)\mathbf{r}(u,v) = [u\cos v, u\sin v, u] = u\cos v\,\mathbf{i} + u\sin v\,\mathbf{j} + u\,\mathbf{k} \qquad (5)

in components x=ucos⁡vx = u\cos v, y=usin⁡vy = u\sin v, z=uz = u. The parameters vary in the rectangle RR: 0≤u≤H0 \leq u \leq H, 0≤v≤2π0 \leq v \leq 2\pi

13.2 Surface Integral​

The extension of the idea of an integral to line and double integrals are not the only generalization that can be made. We can also extend the idea to integration over a general surface, SS. Two types of such integrals occur:

∬Sf(x,y,z) dS(6)\iint_S f(x,y,z)\,dS \qquad (6)

Scalar field, e.g.: surface density

∬SF(r)⋅n^ dS=∬SF(r)⋅dS(7)\iint_S \mathbf{F}(\mathbf{r})\cdot\hat{\mathbf{n}}\,dS = \iint_S \mathbf{F}(\mathbf{r})\cdot d\mathbf{S} \qquad (7)

Vector field, e.g.: fluid velocity

Note that dS=n^ dSd\mathbf{S} = \hat{\mathbf{n}}\,dS is the vector element of area, where n^\hat{\mathbf{n}} is the unit outward-drawn normal vector to the element dSdS.

13.2.1 Surface Integral of Vector Field​

In general, the surface SS can be described in terms of two parameters, uu and vv say, so that on SS

r(u,v)=[x(u,v),y(u,v),z(u,v)]=x(u,v) i+y(u,v) j+z(u,v) k\mathbf{r}(u,v) = [x(u,v), y(u,v), z(u,v)] = x(u,v)\,\mathbf{i} + y(u,v)\,\mathbf{j} + z(u,v)\,\mathbf{k}

where (u,v)(u,v) varies over a region RR in the uvuv-plane. We assume SS to be piecewise smooth, so that SS has a normal vector

N=ru×rvand unit normal vectorn=1∣N∣N\mathbf{N} = \mathbf{r}_u \times \mathbf{r}_v \qquad \text{and unit normal vector} \qquad \mathbf{n} = \frac{1}{|\mathbf{N}|}\mathbf{N}

at every point (except perhaps for some edges or cusps, as for a cube or cone). For a given vector function F\mathbf{F} we can now define the surface integral over SS by

∬SF⋅n dS=∬RF(r(u,v))⋅N(u,v) du dv(8)\iint_S \mathbf{F}\cdot\mathbf{n}\,dS = \iint_R \mathbf{F}(\mathbf{r}(u,v))\cdot\mathbf{N}(u,v)\,du\,dv \qquad (8)

Here N=∣N∣n\mathbf{N} = |\mathbf{N}|\mathbf{n} by equation (12), and ∣N∣=∣ru×rv∣|\mathbf{N}| = |\mathbf{r}_u \times \mathbf{r}_v| is the area of the parallelogram with sides ru\mathbf{r}_u and rv\mathbf{r}_v, by the definition of cross product. Hence

n dS=n∣N∣ du dv=N du dv(8∗)\mathbf{n}\,dS = \mathbf{n}|\mathbf{N}|\,du\,dv = \mathbf{N}\,du\,dv \qquad (8^*)

and we see that dS=∣N∣ du dvdS = |\mathbf{N}|\,du\,dv is the element of area of SS.

also F⋅n\mathbf{F}\cdot\mathbf{n} is the normal component of F\mathbf{F}. This integral arises naturally in flow problems, where it gives the flux across SS when F=ρv\mathbf{F} = \rho\mathbf{v}. The flux across SS is the mass of fluid crossing SS per unit time. Furthermore, ρ\rho is the density of the fluid and v\mathbf{v} the velocity vector of the flow, as illustrated by Example 13.1 below. We may thus call the surface integral (8) the flux integral.

We can write (8) in components, using F=[F1,F2,F3]\mathbf{F} = [F_1, F_2, F_3], N=[N1,N2,N3]\mathbf{N} = [N_1, N_2, N_3], and n=[cos⁡α,cos⁡β,cos⁡γ]\mathbf{n} = [\cos\alpha, \cos\beta, \cos\gamma]. Here α\alpha, β\beta, γ\gamma are the angles between n\mathbf{n} and the coordinate axes; indeed, for the angle between n\mathbf{n} and i\mathbf{i}.

∬SF⋅n dS=∬S(F1cos⁡α+F2cos⁡β+F3cos⁡γ) dS(9)=∬R(F1N1+F2N2+F3N3) du dv\begin{aligned} \iint_S \mathbf{F}\cdot\mathbf{n}\,dS &= \iint_S (F_1\cos\alpha + F_2\cos\beta + F_3\cos\gamma)\,dS \qquad (9) \\ &= \iint_R (F_1N_1 + F_2N_2 + F_3N_3)\,du\,dv \end{aligned}

In (9) we can write cos⁡α dS=dydz\cos\alpha\,dS = dydz, cos⁡β dS=dzdx\cos\beta\,dS = dzdx, cos⁡γ dS=dxdy\cos\gamma\,dS = dxdy. Then (9) becomes the following integral for the flux:

∬SF⋅n dS=∬S(F1 dydz+F2 dzdx+F3 dxdy)(10)\iint_S \mathbf{F}\cdot\mathbf{n}\,dS = \iint_S (F_1\,dydz + F_2\,dzdx + F_3\,dxdy) \qquad (10)

We can use this formula to evaluate surface integrals by converting them to double integrals over regions in the coordinate planes of the xyz-coordinate system. But we must carefully take into account the orientation of SS (the choice of n\mathbf{n}), as described in Section 13.3.1.

The tangent vectors of all the curves on a surface SS through a point PP of SS form a plane, called the tangent plane of SS at PP (refer to Figure 13.4). Exceptions are points where SS has an edge or a cusp (like a cone), so that SS cannot have a tangent plane at such a point. Furthermore, a vector perpendicular to the tangent plane is called a normal vector of SS at PP.

Figure 13.4: Tangent plane and normal vector

Figure 13.4: Tangent plane and normal vector

Now since SS can be given by r=r(u,v)\mathbf{r} = \mathbf{r}(u,v) in (2), the new idea is that we get a curve CC on SS by taking a pair of differentiable functions

u=u(t),v=v(t)u = u(t), \qquad v = v(t)

whose derivatives u′=du/dtu' = du/dt and v′=dv/dtv' = dv/dt are continuous. Then CC has the position vector r~(t)=r(u(t),v(t))\tilde{\mathbf{r}}(t) = \mathbf{r}(u(t), v(t)). By differentiation and the use of the chain rule, we obtain a tangent vector of CC on SS

r~′(t)=dr~dt=∂r∂uu′+∂r∂vv′\tilde{\mathbf{r}}'(t) = \frac{d\tilde{\mathbf{r}}}{dt} = \frac{\partial\mathbf{r}}{\partial u}u' + \frac{\partial\mathbf{r}}{\partial v}v'

Hence the partial derivatives ru\mathbf{r}_u and rv\mathbf{r}_v at PP are tangential to SS at PP. We assume that they are linearly independent, which geometrically means that the curves u=constu = \text{const} and v=constv = \text{const} on SS intersect at PP at a non-zero angle. Then ru\mathbf{r}_u and rv\mathbf{r}_v span the tangent plane of SS at PP. Hence their cross product gives a normal vector N\mathbf{N} of SS at PP.

N=ru×rv≠0(11)\mathbf{N} = \mathbf{r}_u \times \mathbf{r}_v \neq 0 \qquad (11)

The corresponding unit normal vector n\mathbf{n} of SS at PP is (Figure 13.4)

n=1∣N∣N=1∣ru×rv∣ru×rv(12)\mathbf{n} = \frac{1}{|\mathbf{N}|}\mathbf{N} = \frac{1}{|\mathbf{r}_u \times \mathbf{r}_v|}\mathbf{r}_u \times \mathbf{r}_v \qquad (12)

There is an alternative way of obtaining a unit normal vector of a surface SS. If SS is represented by expression g(x,y,z)=0g(x,y,z) = 0, then, from prior knowledge that gradient of gg is always normal to gg:

n=1∣grad⁡g∣grad⁡g(12∗)\mathbf{n} = \frac{1}{|\operatorname{grad} g|}\operatorname{grad} g \qquad (12^*)

Tangent Plane and Surface Normal

If a surface SS is given by (2) with continuous ru=∂r∂u\mathbf{r}_u = \dfrac{\partial\mathbf{r}}{\partial u} and rv=∂r∂v\mathbf{r}_v = \dfrac{\partial\mathbf{r}}{\partial v} at every point of SS, then SS has, at every point PP, a unique tangent plane passing through PP and spanned by ru\mathbf{r}_u and rv\mathbf{r}_v and a unique normal whose direction depends continuously on the points of SS. A normal vector is given by (11) and the corresponding unit normal vector by (12) (see Figure 13.4).

Example 13.1​

Compute the flux of water through the parabolic cylinder S:y=x2S: y = x^2, 0≤x≤20 \leq x \leq 2, 0≤z≤30 \leq z \leq 3 if the velocity vector is v=F=[3z2,6,6xz]\mathbf{v} = \mathbf{F} = [3z^2, 6, 6xz], speed being measured in meters/sec. (Generally, F=ρv\mathbf{F} = \rho\mathbf{v}, but water has density ρ=1 g/cm3=1 ton/m3\rho = 1\ \text{g/cm}^3 = 1\ \text{ton/m}^3)

Parabolic cylinder S: y = x squared

Solution

Writing x=ux = u and z=vz = v, we have y=x2=u2y = x^2 = u^2. Hence a representation of SS is

S:r=[u,u2,v](0≤u≤2, 0≤v≤3)S: \quad \mathbf{r} = [u, u^2, v] \qquad (0 \leq u \leq 2, \ 0 \leq v \leq 3)

By differentiation and by the definition of the cross product,

N=ru×rv=[1,2u,0]×[0,0,1]=[2u,−1,0]\mathbf{N} = \mathbf{r}_u \times \mathbf{r}_v = [1, 2u, 0] \times [0, 0, 1] = [2u, -1, 0]

On SS, writing simply F(S)\mathbf{F}(S) for F[r(u,v)]\mathbf{F}[\mathbf{r}(u,v)], we have F(S)=[3v2,6,6uv]\mathbf{F}(S) = [3v^2, 6, 6uv]. Hence F(S)⋅N=6uv2−6\mathbf{F}(S)\cdot\mathbf{N} = 6uv^2 - 6. By integration we thus get from (7) the flux

∬SF⋅n dS=∫03∫02(6uv2−6) du dv=∫03[3u2v2−6u]u=02dv=∫03(12v2−12) dv=[4v3−12v]v=03=108−36=72 [m3/sec]\begin{aligned} \iint_S \mathbf{F}\cdot\mathbf{n}\,dS &= \int_0^3\int_0^2 (6uv^2 - 6)\,du\,dv = \int_0^3 \left[3u^2v^2 - 6u\right]_{u=0}^2 dv \\ &= \int_0^3 (12v^2 - 12)\,dv = \left[4v^3 - 12v\right]_{v=0}^3 = 108 - 36 = 72\ [\text{m}^3/\text{sec}] \end{aligned}

Or 72,000 liters/sec. Note that the yy-component of F\mathbf{F} is positive (equal to 6), so that in figure above, the flow goes from left to right.

Example 13.2​

Compute the flux through the surface SS, of the cylinder x2+y2=16x^2+y^2 = 16 in the first octant between z=0z = 0 and z=5z = 5 if the velocity vector is F=[z,x,−3y2z]\mathbf{F} = [z, x, -3y^2z], that is, the flux ∬SF⋅dS\displaystyle\iint_S \mathbf{F}\cdot d\mathbf{S}.

Quarter cylinder with surface element dS and normal n

Solution

Writing x=ux = u and z=vz = v, we have y=16−u2y = \sqrt{16-u^2} (from x2+y2=16x^2+y^2 = 16)

r(u,v)=[u,16−u2,v]\mathbf{r}(u,v) = \left[u, \sqrt{16-u^2}, v\right]

ru=∂r∂u=[1,−u16−u2,0]\mathbf{r}_u = \frac{\partial\mathbf{r}}{\partial u} = \left[1, -\frac{u}{\sqrt{16-u^2}}, 0\right]

rv=∂r∂v=[0,0,1]∴N=rv×ru=∣ijk0011−u16−u20∣=[u16−u2,1,0]\mathbf{r}_v = \frac{\partial\mathbf{r}}{\partial v} = [0, 0, 1] \qquad \therefore \mathbf{N} = \mathbf{r}_v \times \mathbf{r}_u = \begin{vmatrix} \mathbf{i} & \mathbf{j} & \mathbf{k} \\ 0 & 0 & 1 \\ 1 & -\frac{u}{\sqrt{16-u^2}} & 0 \end{vmatrix} = \left[\frac{u}{\sqrt{16-u^2}}, 1, 0\right]

F[r(u,v)]=[v,u,−3(16−u2)v]\mathbf{F}[\mathbf{r}(u,v)] = [v, u, -3(16-u^2)v]

F[r(u,v)]⋅N=uv16−u2+u\mathbf{F}[\mathbf{r}(u,v)]\cdot\mathbf{N} = \frac{uv}{\sqrt{16-u^2}} + u

∬SF⋅N dS=∫05∫04uv16−u2+u du dv\iint_S \mathbf{F}\cdot\mathbf{N}\,dS = \int_0^5\int_0^4 \frac{uv}{\sqrt{16-u^2}} + u\ du\,dv

∴∫05(v[∫04u16−u2 du]+∫04u du)=∫05[−v2∫04−2u16−u2 du+∫04u du]dv=∫05−v[16−u2]04dv+∫05[u22]04dv=∫054v dv+∫058 dv=90\begin{aligned} \therefore \int_0^5\left(v\left[\int_0^4 \frac{u}{\sqrt{16-u^2}}\,du\right] + \int_0^4 u\,du\right) &= \int_0^5\left[-\frac{v}{2}\int_0^4 \frac{-2u}{\sqrt{16-u^2}}\,du + \int_0^4 u\,du\right] dv \\ &= \int_0^5 -v\left[\sqrt{16-u^2}\right]_0^4 dv + \int_0^5\left[\frac{u^2}{2}\right]_0^4 dv \\ &= \int_0^5 4v\,dv + \int_0^5 8\,dv = 90 \end{aligned}

Comment: In this example, the solution shown uses a basic parameterization of x=ux = u, y=16−u2y = \sqrt{16-u^2}, z=vz = v, instead of the common cylindrical surface parameterization x=4cos⁡ux = 4\cos u, y=4sin⁡uy = 4\sin u, z=vz = v as learned earlier. Try to repeat this example using the cylindrical surface parameterization (Hint: integrals of the same field and the same surface should result in the same answer).

13.2.2 Surface Integral of Scalar Field​

When the field (function) to be integrated is a scalar field, the resulted integral is known as the surface integral of a scalar field, or simply the scalar surface integral. So, ∬Sf(x,y,z) dS\iint_S f(x,y,z)\,dS has essentially the same concept as vector surface integral, but with a scalar field instead. Just as the vector surface integral, here, for a given surface SS, suitable parameterization can be used: x=x(u,v)x = x(u,v), y=y(u,v)y = y(u,v), z=z(u,v)z = z(u,v), which gives again the position vector r(u,v)=x(u,v)i+y(u,v)j+z(u,v)k\mathbf{r}(u,v) = x(u,v)\mathbf{i} + y(u,v)\mathbf{j} + z(u,v)\mathbf{k}.

Just as the vector surface integral, the surface SS can be specified by a scalar point function C(r)=cC(\mathbf{r}) = c, where cc is a constant. Curves may be drawn on that surface, and in particular if we fix the value of one of the two parameters uu and vv then we obtain two families of curves. On one, Cu(r(u,v0))C_u(\mathbf{r}(u,v_0)) the value of uu varies while vv is fixed, and on the other, Cv(r(u0,v))C_v(\mathbf{r}(u_0,v)), the values of vv varies while uu is fixed, as shown in Figure 13.5. Then as indicated on Figure 13.5, the vector element of area dSd\mathbf{S} is given by:

Figure 13.5: Parametric curves on a surface

Figure 13.5: Parametric curves on a surface

dS=∂r∂udu×∂r∂vdv=∂r∂u×∂r∂vdu dvd\mathbf{S} = \frac{\partial\mathbf{r}}{\partial u}du \times \frac{\partial\mathbf{r}}{\partial v}dv = \frac{\partial\mathbf{r}}{\partial u} \times \frac{\partial\mathbf{r}}{\partial v} du\,dv

=(∂x∂u,∂y∂u,∂z∂u)×(∂x∂v,∂y∂v,∂z∂v)du dv=(J1i+J2j+J3k) du dv= \left(\frac{\partial x}{\partial u}, \frac{\partial y}{\partial u}, \frac{\partial z}{\partial u}\right) \times \left(\frac{\partial x}{\partial v}, \frac{\partial y}{\partial v}, \frac{\partial z}{\partial v}\right) du\,dv = (J_1\mathbf{i} + J_2\mathbf{j} + J_3\mathbf{k})\,du\,dv

where

J1=∂y∂u∂z∂v−∂y∂v∂z∂u,J2=∂z∂u∂x∂v−∂z∂v∂x∂u,J3=∂x∂u∂y∂v−∂x∂v∂y∂uJ_1 = \frac{\partial y}{\partial u}\frac{\partial z}{\partial v} - \frac{\partial y}{\partial v}\frac{\partial z}{\partial u}, \qquad J_2 = \frac{\partial z}{\partial u}\frac{\partial x}{\partial v} - \frac{\partial z}{\partial v}\frac{\partial x}{\partial u}, \qquad J_3 = \frac{\partial x}{\partial u}\frac{\partial y}{\partial v} - \frac{\partial x}{\partial v}\frac{\partial y}{\partial u}

However, instead of dS=∂r∂u×∂r∂vdu dvd\mathbf{S} = \dfrac{\partial\mathbf{r}}{\partial u} \times \dfrac{\partial\mathbf{r}}{\partial v} du\,dv, for scalar surface integral, we have:

dS=∣∂r∂u×∂r∂v∣du dv,where the magnitude∣∂r∂u×∂r∂v∣=J12+J22+J32dS = \left|\frac{\partial\mathbf{r}}{\partial u} \times \frac{\partial\mathbf{r}}{\partial v}\right| du\,dv, \quad \text{where the magnitude} \left|\frac{\partial\mathbf{r}}{\partial u} \times \frac{\partial\mathbf{r}}{\partial v}\right| = \sqrt{J_1^2 + J_2^2 + J_3^2}

∬Sf(x,y,z) dS=∬Af(u,v)J12+J22+J32 du dv(13)\iint_S f(x,y,z)\,dS = \iint_A f(u,v)\sqrt{J_1^2 + J_2^2 + J_3^2}\,du\,dv \qquad (13)

Once the entire integral can be described with only uu and vv, the integration can be carried out to obtain the value of the integral.

Sometimes, a given surface can be very clearly described by z=z(x,y)z = z(x,y). A quick example is a vertical cone with z=x2+y2z = \sqrt{x^2+y^2}. In this situation, we can simply adopt x=ux = u, y=vy = v (and z=u2+v2z = \sqrt{u^2+v^2}). In fact, we can directly write the two parameters as xx and yy without introducing new symbols uu and vv. For example, if z=z(x,y)z = z(x,y) describes a surface as in Figure 13.6, then

r=(x,y,z(x,y))\mathbf{r} = (x, y, z(x,y))

with xx and yy as independent variables. Then, the cross product becomes:

∂r∂u×∂r∂v=∂r∂x×∂r∂y=(−∂z∂x)i+(−∂z∂y)j+(1)k\frac{\partial\mathbf{r}}{\partial u} \times \frac{\partial\mathbf{r}}{\partial v} = \frac{\partial\mathbf{r}}{\partial x} \times \frac{\partial\mathbf{r}}{\partial y} = \left(-\frac{\partial z}{\partial x}\right)\mathbf{i} + \left(-\frac{\partial z}{\partial y}\right)\mathbf{j} + (1)\mathbf{k}

J1=−∂z∂xJ2=−∂z∂yJ3=1J_1 = -\frac{\partial z}{\partial x} \qquad J_2 = -\frac{\partial z}{\partial y} \qquad J_3 = 1

Since dS=∣∂r∂u×∂r∂v∣du dv=∣∂r∂x×∂r∂y∣dx dydS = \left|\dfrac{\partial\mathbf{r}}{\partial u} \times \dfrac{\partial\mathbf{r}}{\partial v}\right| du\,dv = \left|\dfrac{\partial\mathbf{r}}{\partial x} \times \dfrac{\partial\mathbf{r}}{\partial y}\right| dx\,dy,

∬Sf(x,y,z) dS=∬Rf(x,y,z(x,y))1+(∂z∂x)2+(∂z∂y)2 dx dy(14)\iint_S f(x,y,z)\,dS = \iint_R f(x,y,z(x,y))\sqrt{1 + \left(\frac{\partial z}{\partial x}\right)^2 + \left(\frac{\partial z}{\partial y}\right)^2}\,dx\,dy \qquad (14)

Figure 13.6: A surface described by z = z(x, y)

Figure 13.6: A surface described by z = z(x, y)

Example 13.3​

Evaluate the surface integral

∬S(x+y+z) dS\iint_S (x + y + z)\,dS

where SS is the portion of the sphere x2+y2+z2=1x^2+y^2+z^2 = 1 that lies in the first octant.

(a) Surface S and (b) quadrant of a circle in the (x, y) plane

(a) Surface S (b) quadrant of a circle in the (x, y) plane
Solution

The surface SS is illustrated in the above figure. Taking

z=1−x2−y2z = \sqrt{1-x^2-y^2}

we have

∂z∂x=−x1−x2−y2\frac{\partial z}{\partial x} = \frac{-x}{\sqrt{1-x^2-y^2}}

∂z∂y=−y1−x2−y2\frac{\partial z}{\partial y} = \frac{-y}{\sqrt{1-x^2-y^2}}

giving

1+(∂z∂x)2+(∂z∂y)2=x2+y2+(1−x2−y2)(1−x2−y2)=11−x2−y2\sqrt{1 + \left(\frac{\partial z}{\partial x}\right)^2 + \left(\frac{\partial z}{\partial y}\right)^2} = \sqrt{\frac{x^2+y^2+(1-x^2-y^2)}{(1-x^2-y^2)}} = \frac{1}{\sqrt{1-x^2-y^2}}

∴∬S(x+y+z) dS=∬A[x+y+1−x2−y2]11−x2−y2 dx dy\therefore \iint_S (x+y+z)\,dS = \iint_A \left[x + y + \sqrt{1-x^2-y^2}\right]\frac{1}{\sqrt{1-x^2-y^2}}\,dx\,dy

where AA is the quadrant of a circle in the (x,y)(x,y) plane illustrated in Figure (b) (refer to the above Figure).

Thus,

∬S(x+y+z) dS=∫01∫01−x2[x1−x2−y2+y1−x2−y2+1]dy dx\iint_S (x+y+z)\,dS = \int_0^1\int_0^{\sqrt{1-x^2}} \left[\frac{x}{\sqrt{1-x^2-y^2}} + \frac{y}{\sqrt{1-x^2-y^2}} + 1\right] dy\,dx

=∫01[xsin⁡−1(y1−x2)−1−x2−y2+y]01−x2dx=∫01[π2x+21−x2]dx=[π4x2+x1−x2+sin⁡−1x]01=34π\begin{aligned} &= \int_0^1 \left[x\sin^{-1}\left(\frac{y}{\sqrt{1-x^2}}\right) - \sqrt{1-x^2-y^2} + y\right]_0^{\sqrt{1-x^2}} dx \\ &= \int_0^1 \left[\frac{\pi}{2}x + 2\sqrt{1-x^2}\right] dx = \left[\frac{\pi}{4}x^2 + x\sqrt{1-x^2} + \sin^{-1}x\right]_0^1 = \frac{3}{4}\pi \end{aligned}

An alternative approach to evaluating the surface integral in this example is to evaluate it directly over the surface of the sphere using spherical polar coordinates. As illustrated in the Figure (c), on the surface of a sphere of radius aa we have,

x=asin⁡θcos⁡ϕ,y=asin⁡θsin⁡ϕ,z=acos⁡θ,dS=a2sin⁡θ dθ dϕx = a\sin\theta\cos\phi, \quad y = a\sin\theta\sin\phi, \quad z = a\cos\theta, \quad dS = a^2\sin\theta\,d\theta\,d\phi

(c) Surface element in spherical polar coordinates

(c) Surface element in spherical polar coordinates

The radius a=1a = 1, so that

∬S(x+y+z) dS=∫0π/2∫0π/2(sin⁡θcos⁡ϕ+sin⁡θsin⁡ϕ+cos⁡θ)sin⁡θ dθ dϕ\iint_S (x+y+z)\,dS = \int_0^{\pi/2}\int_0^{\pi/2}(\sin\theta\cos\phi + \sin\theta\sin\phi + \cos\theta)\sin\theta\,d\theta\,d\phi

=∫0π/2[14πcos⁡ϕ+14πsin⁡ϕ+12]dϕ=34π= \int_0^{\pi/2}\left[\frac{1}{4}\pi\cos\phi + \frac{1}{4}\pi\sin\phi + \frac{1}{2}\right]d\phi = \frac{3}{4}\pi

Example 13.4​

Calculate the surface integral ∬S(x+y+z) dS\displaystyle\iint_S (x+y+z)\,dS where SS is the portion of the plane x+2y+4z=4x + 2y + 4z = 4 lying in the first octant (x≥0x \geq 0, y≥0y \geq 0, z≥0z \geq 0)

Solution

Rewrite linear equation:

z=4−x−2y4=1−x4−y2z = \frac{4-x-2y}{4} = 1 - \frac{x}{4} - \frac{y}{2}

∂z∂x=−14∂z∂y=−12\frac{\partial z}{\partial x} = -\frac{1}{4} \qquad \frac{\partial z}{\partial y} = -\frac{1}{2}

∬Sf(x,y,z) dS=∬Af(x,y,z(x,y))1+(∂z∂x)2+(∂z∂y)2 dx dy\iint_S f(x,y,z)\,dS = \iint_A f(x,y,z(x,y))\sqrt{1 + \left(\frac{\partial z}{\partial x}\right)^2 + \left(\frac{\partial z}{\partial y}\right)^2}\,dx\,dy

∬Sf(x,y,z) dS=∬A(x+y+1−x4−y2)1+(−14)2+(−12)2 dx dy\iint_S f(x,y,z)\,dS = \iint_A \left(x + y + 1 - \frac{x}{4} - \frac{y}{2}\right)\sqrt{1 + \left(-\frac{1}{4}\right)^2 + \left(-\frac{1}{2}\right)^2}\,dx\,dy

=∬A(3x4+y2+1)214 dx dy= \iint_A \left(\frac{3x}{4} + \frac{y}{2} + 1\right)\frac{\sqrt{21}}{4}\,dx\,dy

=214∫02∫04−2y(3x4+y2+1)dx dy=2116∫02(3x22+2yx+4x)04−2ydy=2132∫02(3(16−16y+4y2)+16y−8y2+32−16y)dy=2132∫02(80−48y+4y2) dy=218∫0220−12y+y2 dy=218[20y−6y2+y33]02=218(40−24+83)=7213\begin{aligned} &= \frac{\sqrt{21}}{4}\int_0^2\int_0^{4-2y}\left(\frac{3x}{4} + \frac{y}{2} + 1\right) dx\,dy = \frac{\sqrt{21}}{16}\int_0^2\left(\frac{3x^2}{2} + 2yx + 4x\right)_0^{4-2y} dy \\ &= \frac{\sqrt{21}}{32}\int_0^2\left(3(16-16y+4y^2) + 16y - 8y^2 + 32 - 16y\right) dy = \frac{\sqrt{21}}{32}\int_0^2 (80 - 48y + 4y^2)\,dy \\ &= \frac{\sqrt{21}}{8}\int_0^2 20 - 12y + y^2\,dy = \frac{\sqrt{21}}{8}\left[20y - 6y^2 + \frac{y^3}{3}\right]_0^2 = \frac{\sqrt{21}}{8}\left(40 - 24 + \frac{8}{3}\right) = \frac{7\sqrt{21}}{3} \end{aligned}

Region D bounded by x + 2y = 4 in the xy-plane

Scalar surface integral can also be used to find the area of a given surface SS. This is when f(x,y,z)=1f(x,y,z) = 1 and the integral ∬Sf(x,y,z) dS=∬SdS\iint_S f(x,y,z)\,dS = \iint_S dS simply 'sums-up' all the elements' small area to give the area of the entire surface SS. The following examples demonstrate this application.

Example 13.5​

Find the area of the surface z=x2+y2z = \sqrt{x^2+y^2} over the region bounded by x2+y2=1x^2+y^2 = 1

Solution

z=f(x,y)z = f(x,y)

A(S)=∬R∗1+(∂f∂x)2+(∂f∂y)2dx dyA(S) = \iint_{R^*} \sqrt{1 + \left(\frac{\partial f}{\partial x}\right)^2 + \left(\frac{\partial f}{\partial y}\right)^2} dx\,dy

So we now find ∂f∂x\dfrac{\partial f}{\partial x} and ∂f∂y\dfrac{\partial f}{\partial y} and determine 1+(∂f∂x)2+(∂f∂y)2\sqrt{1 + \left(\dfrac{\partial f}{\partial x}\right)^2 + \left(\dfrac{\partial f}{\partial y}\right)^2} which is

f(x,y)=(x2+y2)1/2∴∂f∂x=12(x2+y2)−1/22x=xx2+y2f(x,y) = (x^2+y^2)^{1/2} \qquad \therefore \frac{\partial f}{\partial x} = \frac{1}{2}(x^2+y^2)^{-1/2}2x = \frac{x}{\sqrt{x^2+y^2}}

∂f∂y=12(x2+y2)−1/22y=yx2+y2\frac{\partial f}{\partial y} = \frac{1}{2}(x^2+y^2)^{-1/2}2y = \frac{y}{\sqrt{x^2+y^2}}

∴1+(∂f∂x)2+(∂f∂y)2=1+x2+y2x2+y2=2\therefore \sqrt{1 + \left(\frac{\partial f}{\partial x}\right)^2 + \left(\frac{\partial f}{\partial y}\right)^2} = \sqrt{1 + \frac{x^2+y^2}{x^2+y^2}} = \sqrt{2}

A(S)=∬R∗1+(∂f∂x)2+(∂f∂y)2dx dy=2∬Rdx dyA(S) = \iint_{R^*} \sqrt{1 + \left(\frac{\partial f}{\partial x}\right)^2 + \left(\frac{\partial f}{\partial y}\right)^2} dx\,dy = \sqrt{2}\iint_R dx\,dy

But R is bounded by x2+y2=1x^2+y^2 = 1, i.e. a circle, centre the origin and radius 1. ∴area=π\therefore area = \pi

A(S)=2∬Rdx dy=2πA(S) = \sqrt{2}\iint_R dx\,dy = \sqrt{2}\pi

Example 13.6​

Find the area of the surface SS of the paraboloid z=x2+y2z = x^2+y^2 cut off by the cone z=2x2+y2z = 2\sqrt{x^2+y^2}

Paraboloid cut off by the cone, and the section in the yz-plane

Solution

We can find the point of intersection AA by considering the yy-zz plane i.e. x=0x = 0. Then, coordinates of AA are A(2,4)A(2, 4).

The projection of the surface SS on the xx-yy plane is

x2+y2=4x^2+y^2 = 4

Cylinder and paraboloid with the projection region R

A(S)=∬R∗1+(∂f∂x)2+(∂f∂y)2dx dyA(S) = \iint_{R^*} \sqrt{1 + \left(\frac{\partial f}{\partial x}\right)^2 + \left(\frac{\partial f}{\partial y}\right)^2} dx\,dy

For this we use the equation of the surface SS. The information from the projection RR on the xx-yy plane will later provide the limits of the two stages of integration.

For the time being, then

A(S)=∬R∗1+4x2+4y2 dx dyA(S) = \iint_{R^*} \sqrt{1 + 4x^2 + 4y^2}\,dx\,dy

using Cartesian coordinates, we could integrate with respect to yy from y=0y = 0 to y=4−x2y = \sqrt{4-x^2} and then with respect to xx from x=0x = 0 to x=2x = 2. Finally we should multiply by four to cover all four quadrants

Circle of radius 2 with the vertical strip y = sqrt(4 - x squared)

i.e. A(S)=4∫x=02∫y=04−x21+4x2+4y2 dy dx\text{i.e. } A(S) = 4\int_{x=0}^{2}\int_{y=0}^{\sqrt{4-x^2}} \sqrt{1+4x^2+4y^2}\,dy\,dx

but how do we carry out the actual integration? It becomes a lot easier if we use polar coordinates. The same integral in polar coordinates is

A(S)=∫θ=02π∫r=021+4r2 r dr dθA(S) = \int_{\theta=0}^{2\pi}\int_{r=0}^{2}\sqrt{1+4r^2}\,r\,dr\,d\theta

A(S)=∫θ=02π∫r=02(1+4r2)1/2 r dr dθ=∫02π[112(1+4r2)3/2]02dθ=112∫02π{173/2−1}dθ=5.7577 [θ]02π=36.18\begin{aligned} A(S) &= \int_{\theta=0}^{2\pi}\int_{r=0}^{2}(1+4r^2)^{1/2}\,r\,dr\,d\theta = \int_0^{2\pi}\left[\frac{1}{12}(1+4r^2)^{3/2}\right]_0^2 d\theta \\ &= \frac{1}{12}\int_0^{2\pi}\{17^{3/2} - 1\}d\theta = 5.7577\,[\theta]_0^{2\pi} = 36.18 \end{aligned}

13.3 Some Properties of Surface Integral​

In this section, we discuss some properties of surface integral that are relevant to solving the integral. In particular, we look into these two matters: (i) the orientation of a given surface, and (ii) the continuity of a surface.

13.3.1 Orientation of Surfaces​

From (8) and (8*), we see that the value of the integral depends on the choice of the unit normal vector n\mathbf{n}. We express this by saying that such an integral is an integral over an oriented surface SS, that is, over a surface SS on which we have chosen one of the two possible unit normal vectors in a continuous fashion.

If we change the orientation of SS, as illustrated by Figure 13.7, this means that we replace n\mathbf{n} with −n-\mathbf{n}. Then each component of n\mathbf{n} is multiplied by -1. This gives a negative to the original value of the surface integral.

Figure 13.7: Orientation of a Surface

Figure 13.7: Orientation of a Surface
Change of Orientation in a Surface Integral

The replacement of n\mathbf{n} by −n-\mathbf{n} (hence of N\mathbf{N} by −N-\mathbf{N}) corresponds to the multiplication of the integral in (8) by -1

Example 13.7​

From Example 13.1, for the surface SS represented by r=[u,u2,v]\mathbf{r} = [u, u^2, v], 0≤u≤20 \leq u \leq 2, 0≤v≤30 \leq v \leq 3. If we consider the normal vector along the opposite direction:

Solution

N=rv×ru=[0,0,1]×[1,2u,0]=[−2u,1,0]\mathbf{N} = \mathbf{r}_v \times \mathbf{r}_u = [0, 0, 1] \times [1, 2u, 0] = [-2u, 1, 0]

F⋅N=[3v2,6,6uv]⋅[−2u,1,0]=6−6uv2\mathbf{F}\cdot\mathbf{N} = [3v^2, 6, 6uv]\cdot[-2u, 1, 0] = 6 - 6uv^2

Note that this integrand is now the negative of that in Example 13.1. Consequently, it is obvious that the integration also gives the negative of the value obtained in Example 13.1:

∬SF⋅N du dv=∫03∫02(6−6uv2) du dv=∫03(12−12v2) dv=−72\iint_S \mathbf{F}\cdot\mathbf{N}\,du\,dv = \int_0^3\int_0^2 (6 - 6uv^2)\,du\,dv = \int_0^3 (12 - 12v^2)\,dv = -72

However, the orientation of a surface (the required direction of the unit normal vector) does not affect a scalar surface integral. This is because ∬Sf(x,y,z) dS=∬Sf(u,v)∣∂r∂u×∂r∂v∣du dv\displaystyle\iint_S f(x,y,z)\,dS = \iint_S f(u,v)\left|\frac{\partial\mathbf{r}}{\partial u} \times \frac{\partial\mathbf{r}}{\partial v}\right| du\,dv, so even though ru×rv=−(rv×ru)\mathbf{r}_u \times \mathbf{r}_v = -(\mathbf{r}_v \times \mathbf{r}_u), the magnitudes are the same. In fact, we do not speak of orientation of the given surface when solving a scalar surface integral. Therefore, this is also sometimes known as surface integral without regard to orientation.

13.3.2 Continuity of Surfaces​

This property is similar to that of a line integral. Its concept can be conveniently expressed by: ∬f(x,y,z) dS=∬f(x,y,z) dS1+∬f(x,y,z) dS2\iint f(x,y,z)\,dS = \iint f(x,y,z)\,dS_1 + \iint f(x,y,z)\,dS_2 for ease of understanding. This means, when the integration is to be carried out over a surface SS which is a composite of two (or more) surfaces, e.g. S1S_1 and S2S_2, the surface integral can be obtained by summing all the component surface integrals. This is true as long as the piecewise surface is continuous.

This property is usually applicable in situations involving closed surfaces, for example, as illustrated below:

Example 13.8​

Evaluate the surface integral ∬S(z2) dS\displaystyle\iint_S (z^2)\,dS, where SS is the total area of the cone x2+y2≤z≤2\sqrt{x^2+y^2} \leq z \leq 2

Cone with lateral surface S1 and base S2

Solution

S1S_1: surface of the cone

S2S_2: base (cover) of the cone

S1=∬S1z2 dS1=2∬x2+y2 dx dyS_1 = \iint_{S_1} z^2\,dS_1 = \sqrt{2}\iint x^2+y^2\,dx\,dy

Change to polar coordinate

=2∫02π∫02r2 r dr dθ=82 π= \sqrt{2}\int_0^{2\pi}\int_0^2 r^2\,r\,dr\,d\theta = 8\sqrt{2}\,\pi

S2S_2 – base of the cone at z=2z = 2

S2=∬S222 dS2=4∬S2dS2∬dS2=area of the base=πr2=π(22)=4πS_2 = \iint_{S_2} 2^2\,dS_2 = 4\iint_{S_2} dS_2 \qquad \iint dS_2 = \text{area of the base} = \pi r^2 = \pi(2^2) = 4\pi

=4∬S2dS2=4(4π)=16π= 4\iint_{S_2} dS_2 = 4(4\pi) = 16\pi

Total Surface Integral =S1+S2=82π+16π= S_1 + S_2 = 8\sqrt{2}\pi + 16\pi

As a final remark, note that this property is applicable to both scalar surface integrals and vector surface integrals.