Objectives:
- 1.
- Know when Stokes’ theorem can help compute a flux integral.
- 2.
- Understand when a flux integral is surface independent.
- 3.
- Be able to compute flux integrals using Stokes’ theorem or surface independence.
Recap Video
Here is a video highlights the main points of the section.
_
Here is a second video which gives the steps for using Stokes’ theorem to compute a flux integral.
_
Example Video
Here is an example of finding the “anti-curl” of a vector field.
The following videos show a worked example of using Stokes’ theorem to compute a flux integral. We compute the answer in two ways, one in each video.If and is the portion of inside the cylinder , oriented outward,
evaluate .
- Approach 1: Anti-curling. _
- Approach 2: Surface independence. _
Problems
Suppose and is the portion of where , oriented with outward normals.
Evaluate .
There are two ways to go about solving a problem like this, so we
will go through both.
- (a)
- Approach 1: Use Stokes’ theorem directly. Stokes’ theorem says
In this case, the boundary is the curve in the plane . If is oriented
outward, then is oriented clockwisecounterclockwise
when viewed from above. We can parametrize the curve as
for so that
Then
and
Thus,
- (b)
- Approach 2: Use surface independence. Here we want the flux of , which is the curl of some vector field (namely ), which means the flux integral is surface independent. We can change the surface to be whatever we want as long as is kept the same. As we saw in the above approach, is the circle in the plane , oriented counterclockwise when viewed from above. Also note that This looks ugly, but it works out nicely in the end. A convenient surface to pick is the disc in the plane , call this . Since is oriented counterclockwise, we need to be oriented with upwarddownward normals. Now we compute the flux. We can parametrize the surface as with domain . Then and which is the correctincorrect normal vector. Notice (which looks much more reasonable), and the flux becomes
Let , and let be the portion of where , oriented with outward normals.
Evaluate .
This flux integral is slightly unpleasant to do directly from the
formula, so we can look for an easier way. Notice that and that the
components of have continuous partials, so we can conclude:
is
conservative for some
Therefore, Stokes’ theorem and its consequences apply. Finding such a is a
lengthy process, so we will use surface independence instead. A good surface
to pick is the disc in the plane , call this . We must figure out the orientation.
To do this, notice that being oriented with outward normals means that is counterclockwiseclockwise
when viewed from above. The new surface has the same boundary, so if is
clockwise, then should be oriented with upwarddownward
normals. With this orientation,
Parametrize the new surface as
in the domain given by . Then
which is the correctincorrect
normal. So we will take the normal to be . Therefore, the flux over is
The first part following problem is not applicable in Math 120 Fall 2019. You
can assume and evaluate the rest.
With the same and as in the previous problem, evaluate by finding
a such that and computing a line integral instead.
If and is the portion of with , oriented outward, then .
Since and the
components of have continuous partials everywhere, we know is the
curl of a vector field. This means we can use surface independence.
Change the surface to in the plane (call this ), oriented upwarddownward
. You can parametrize this as
in the domain given by . Then
which is the correct normal. Then
The flux is therefore
Let and let be the portion of with , oriented with outward normals,
coupled with the disc in the plane , oriented with normals pointing in the
positive -direction. Then .
Since is the curl of some vector field, we can
either parametrize the boundary and use normal Stokes’, or use surface
independence. If we use surface independence, we can change the surface to
the disc in the plane , oriented with normals pointing in the positive
-direction. Parametrize this surface as for . Then , which is the right normal.
Since , we get
The flux of the curl becomes