Next: Flux Through Cylinders
Up: The flux Integral
Previous: Introduction
Now we need to find
and dS. If the surface S is defined by a
function, z=g(x,y) we can obtain a nice expression for
and dS.
For the normal vector to S at the point (x0,y0,g(x0,y0)) we
can use the normal vector to the tangent plane. Remember that the tangent
plane to g(x,y) at the point (x0,y0) is given by:
![\begin{displaymath}
z=g_{x}(x_{0},y_{0})\left( x-x_{0}\right) +g_{y}(x_{0},y_{0})\left(
y-y_{0}\right) +g(x_{0},y_{0})
\end{displaymath}](img52.gif)
or
-gx(x0,y0)x-gy(x0,y0)y+z=c
where c=-gx(x0,y0)x0-gy(x0,y0)y0+g(x0,y0). A
normal vector to the tangent plane is
![\begin{displaymath}
\vec{n}=-g_{x}(x_{0},y_{0})\hat{\imath}-g_{y}(x_{0},y_{0})\hat{j}+\hat{k}
\end{displaymath}](img53.gif)
If we normalize
to get a unit normal vector we get
![\begin{displaymath}
\hat{n}=\frac{-g_{x}(x_{0},y_{0})\hat{\imath}-g_{y}(x_{0},y_...
...t{k}}{\sqrt{g_{x}(x_{0},y_{0})^{2}+g_{y}(x_{0},y_{0})^{2}+1}}
\end{displaymath}](img54.gif)
So the normal vector as a function of
is
![\begin{displaymath}
\hat{n}=\frac{-g_{x}(x,y)\hat{\imath}-g_{y}(x,y)\hat{j}+\hat{k}}{\sqrt{g_{x}(x,y)^{2}+g_{y}(x,y)^{2}+1}}
\end{displaymath}](img56.gif)
The Area of the jth patch can be obtained by finding the vectors
,
which define the edges of the patch (one parallel to the xz-plane and one parallel to the yz-plane????). The area of the patch is
given by
. If we employ the tangent
plane approximation of g(x,y)we can see that
is the vector from (x0,y0,g(x0,y0)) to
or
![\begin{displaymath}
\vec{u}=\Delta x\hat{\imath}+g_{x}(x_{0},y_{0})\Delta x\hat{k}
\end{displaymath}](img60.gif)
Similarly
is the vector that points from (x0,y0,g(x0,y0)) to the point
or
![\begin{displaymath}
\vec{v}=\Delta y\hat{j}+g_{y}(x_{0},y_{0})\Delta y\hat{k}
\end{displaymath}](img62.gif)
Taking the cross product of
and
gives
![\begin{displaymath}
\vec{u}\times \vec{v} =\left\vert
\begin{array}
{lll}
\ha...
... \Delta y & g_{y}(x_{0},y_{0})\Delta y
\end{array}
\right\vert\end{displaymath}](img63.gif)
![\begin{displaymath}
=-g_{x}(x_{0},y_{0})\Delta x\Delta y\hat{\imath}-g_{y}(x_{0},y_{0})\Delta
x\Delta y\hat{j}+\Delta x\Delta y\hat{k}
\end{displaymath}](img64.gif)
Finally, the area of the jth patch is
![\begin{displaymath}
\Delta S_{j}=\left\Vert \vec{u}\times \vec{v}\right\Vert =\s...
...x}(x_{0},y_{0})^{2}+g_{y}(x_{0},y_{0})^{2}+1}\Delta x\Delta y
\end{displaymath}](img65.gif)
In the limit that
this becomes
![\begin{displaymath}
dS =\sqrt{g_{x}(x,y)^{2}+g_{y}(x,y)^{2}+1}dxdy\end{displaymath}](img67.gif)
![\begin{displaymath}
=\sqrt{g_{x}(x,y)^{2}+g_{y}(x,y)^{2}+1}d\end{displaymath}](img68.gif)
When we put these together we get
![\begin{displaymath}
d\vec{A} =\hat{n}dS=\frac{-g_{x}(x,y)\hat{\imath}-g_{y}(x,y)...
...^{2}+g_{y}(x,y)^{2}+1}}\sqrt{g_{x}(x,y)^{2}+g_{y}(x,y)^{2}+1}dA\end{displaymath}](img69.gif)
| ![\begin{displaymath}
d\vec{A} =\left( -g_{x}(x,y)\hat{\imath}-g_{y}(x,y)\hat{j}+\hat{k}\right)
dA
\end{displaymath}](img70.gif) |
(3) |
So we've represented the integral over the surface in terms of an integral
over the region R in the xy-plane over which S sits.
![\begin{displaymath}
\int_{S}\vec{F}\cdot d\vec{A}=\int_{S}\vec{F}\cdot \hat{n}dS...
...x,y)\hat{\imath}-g_{y}(x,y)\hat{j}+\hat{k}\right)
\right] dA
\end{displaymath}](img71.gif)
Where R is the ''shadow'' of S on the xy-plane.
Notes:
Example
- 1.
- Calculate the flux of the vector field
through the upper hemisphere of x2+y2+z2=4 that lies above the rectangle
,
, oriented upward.
Since the surface consists of the upper hemisphere we can solve the equation
of the sphere for
, so the surface is the
graph of a function and we can use
to find
.
![\begin{displaymath}
d\vec{A}=\left( \frac{x}{\sqrt{4-x^{2}-y^{2}}}\hat{\imath}+\frac{y}{\sqrt{4-x^{2}-y^{2}}}\hat{j}+\hat{k}\right) dxdy
\end{displaymath}](img81.gif)
The flux integral is
![\begin{displaymath}
\int_{S}\vec{F}\cdot d\vec{A}=\int_{R}\left( \frac{-xz}{\sqr...
...2}-y^{2}}}+\frac{yz^{3}}{y\sqrt{4-x^{2}-y^{2}}}+x\right) dydx
\end{displaymath}](img82.gif)
Where R is the rectangle
,
. Now
substitute
to eliminate the z dependence in the
integral. The integral reduces to
![\begin{displaymath}
\int_{-1}^{1}\int_{0.5}^{1}\left( -x+4-x^{2}-y^{2}+x\right) dydx\end{displaymath}](img84.gif)
![\begin{displaymath}
=\int_{-1}^{1}\int_{0.5}^{1}\left( 4-x^{2}-y^{2}\right) dydx=\frac{37}{12}
\end{displaymath}](img85.gif)
Next: Flux Through Cylinders
Up: The flux Integral
Previous: Introduction
Vector Calculus
8/21/1998