15.6 Surface Integrals
The rest of this unit will focus on surface integrals and their applications. The type of problems will be concerned with fluid flow across surfaces in R3.
Let z = g(x,y) be some surface S and R be its projection (like its 'shadow')
in the xy plane. Suppose further that g, gx and gy are
continuous at all points in R and that there is a function f that is defined
at all points on the surface S. If we cut R up into small rectangles, and
project those rectangles upward to S, it would form a partition of S. We could
pick a point in each sub-region of S and form the sum
where
DSi is the surface area
of the piece and
f(xi,yi,zi) is the function evaluated at
some point within Si. Note that
where DAi
is the area of the rectangle in R underneath Si . If we let the
norm of the partition of R be such that ||D||
approaches 0, then we define the 'surface integral of S' to be
Theorem 15.10 Evaluating a Surface Integral
Let S be a surface with equation z = g(x,y) and let R be it's projection (shadow) in the xy plane. If g, gx and gy are all continuous on R and f is continuous on S, then the surface integral of f over S is
Ex 1 Evaluate the surface integral given if S is
the surface 2x - 2y + z = 10 where
and
.
If we write the planar equation as z = g(x,y) =
10 - 2x + 2y, we can see that gx= -2 and gy = 2, so
we know that our integral can be written as below, given the above x and y
limits:
or
more simply
,
you should verify this yields 216 yourself, here is Mathcad's result:
What the calculation found is the mass of the section of plane shown in the picture if it's density at (x,y,z) is given by x - 2y + z.
Ex 1-A Try to get the same result as in Ex 1 if we use a different axes, say let the region R be the shadow in the yz plane.
First, x = g(y,z) = 5 + y - z/2 so gy
= 1 and gz = -1/2. We also need y and z limits of integration.
The y limits remain the same. Note y=0 and x=0 forces z=10, x=2 and y=4 forces
z=14 so, our z limits appear to be
.
The integral will be
simplifying
to
or
even more simply
which
you should verify is also 216.
Ex 2 A cone shaped
lamina S is given by
as
shown in the picture below: At each point (x,y,z) on the cone,
the density is proportional to the distance between the point and the z axis.
Find the mass of the lamina.
To solve this, we need a density function, which
based on the information given, would be
since
the part under the radical is the distance to the z axis. Also, we need integration
limits from the region in the xy plane that is the shadow of the surface S.
R can be defined as
(if
you don't see this, let z = 0 in the cone equation) The integral now would
look like
whose integrand algebraically simplifies
to
which
would make for a tough integral. However, if we switch to polar coordinates,
it becomes the following, (and note the simple limits of integration as well!)
I used Mathcad to evaluate this, but you should verify we get the answer given
here:
or
.
Suppose our surface is defined parametrically like those in lesson 5 of
this unit. That is, suppose
defines
a surface S defined over some region D (the shadow) in the uv plane. It can
be shown that the surface integral of f(x,y,z) over S is given by the formula:
Note the similarity to the line integral over a path C described by a vector valued function r(t) in a vector field f(x,y,z) given here and discussed in Unit V lesson 2:
Ex 3 Let S be the first octant portion of
the cylinder y2+z2=9 where
.
Evaluate the integral
over the given surface in parametric form.
Now
describes
our surface in parametric form.
Note
and
,
and we have
and
so
and
our surface integral has become
and
then evaluates as 12p +
36. You should verify this result. A sketch of the surface is given below.
Orientation of a Surface
If we have what is called an oriented surface, it can be used to represent problems involving fluid flow. (Keep in mind, the fluid may be liquid or gas which may behave as a fluid under certain conditions.) A surface S is called orientable if a unit normal vector N can be defined at every non-boundary point of S in such a way that the set of normal vectors varies continuously over all S. If this is possible, then S is called an oriented surface. Note further that an orientable surface has two distinct sides. Ellipsoids, paraboloids, planes and most surfaces we have studied are orientable. A Mobius strip is not, since it has but one side. Here is a drawing of a Mobius strip. If you look at it carefully, you can see that you can draw a continuous line around the entire strip without removing your pencil, hence it has but one side.
Suppose we have a surface z = g(x,y) If we examine the function of three
variables constructed from g, G(x,y,z) = z - g(x,y), we can orient the surface
by use of the unit vector in the direction of the gradient vector
at
any point on the surface. Of course since we have a two sides surface, the
downward orientation would be
.
Note a simpler form for each of these is
and
.
If a smooth surface S is given in parametric form by the vector valued function
, then unit normal
vectors can be given by
and
.
If a fluid has a continuous velocity vector field F and a an imaginary
surface S is submerged in the fluid, then the volume of fluid crossing the
surface S per unit of time is called the flux of F across S. If
we cut the surface S into small units in the usual way, we can assume that
F is nearly constant across DS.
The amount of fluid crossing DS per
unit of time is approximated by the volume of a column of height F.N
(the vector field's component normal to the surface) and base DS,
i.e. the amount of volume of the fluid crossing this portion of the surface
is
. Adding all of
these up for a surface S to get the amount of fluid for the entire surface
gets us the flux integral.
Def Flux Integral
Let F=Mi+Nj+Pk where M, N, and P have continuous
first partial derivatives on a surface S oriented by a unit normal vector
N. The flux integral of F across S is given by
If the fluid is not uniformly dense, and r(x,y,z)
is the density of the fluid at (x,y,z) then the integral
represents the total mass of fluid crossing the surface S per time unit.
Theorem 15.11 Evaluating a Flux Integral
Let S be an oriented surface given by z = g(x,y) and R be the projection of S (shadow) onto the xy plane. Then the flux integrals (oriented upwards and downwards respectively) are
Ex 4 Set up the integral to find the flux of F through S Where N is the 'upper' unit normal vector to S where F = xi+yj and S is the plane 2x + 3y + z = 6 in the first octant.
First z = 6 - 2x - 3y and gx = -2, gy
= -3, so F.N = (xi+yj).(2i+3j+k) = 2x+3y.
Now we need to find limits of integration and an order of integration, so
we need to find the region R in the xy plane. If z = 0, we have 2x+3y=6 or
y=(-2/3)x+2. Look at the picture below to see the triangular region R under
the surface. The required integral is
.
What would the result be if we used the lower unit normal vector to orient
S?
What does this say about the actual result regarding
the meaning of flux?
Suppose the oriented surface is given by the vector valued function
.
Then we can define the flux integral as
Ex 5 Find the flux over the portion of the sphere S given by x2+y2+z2= 16 lying in the first octant where the force field F = xi+yj+zk. Assume the sphere is oriented with N outward.
Writing the surface parametrically, we have r(u,v)=4sin(u)cos(v)i+4sin(u)sin(v)j+4cos(u)k (See the conversion formula to spherical coordinates if necessary), which gives us ru(u,v)=4cos(u)cos(v)i+4cos(u)sin(v)j-4sin(u)k and rv(u,v)=-4sin(u)sin(v)i+4sin(u)cos(v)j.
So our integral is now
Ex 5A Do the above problem without the parametric
representation of the sphere. (Note in Theorem 15.11 above that the integrand
can be written as
or
)
With an integrand such as this
, a switch to polar coordinates would be wise.