9—Vector Calculus 1 252
y
x
θk+1
nˆk
b
θk
ˆy
ˆx
y
b/ 2
(b/2) sinθ
The velocity field is the same as before,~v(x,y,z) =v 0 ˆxy/b, so the contribution to the flow rate through this
piece of the surface is
~vk.∆A~k=v 0
yk
b
ˆx.a
b
2
∆θknˆk
The value ofykat the angleθkis
yk=
b
2
+
b
2
sinθk, so
yk
b
=
1
2
[1 + sinθk]
Put the pieces together and you have
v 0
1
2
[
1 + sinθk
]
xˆ.a
b
2
∆θk
[
ˆxcosθk+yˆsinθk
]
=v 0
1
2
[
1 + sinθk
]
a
b
2
∆θkcosθk
The total flow is the sum of these overkand then the limit as∆θk→ 0.
lim
∆θk→ 0
∑
k
v 0
1
2
[
1 + sinθk
]
a
b
2
∆θkcosθk=
∫π/ 2
−π/ 2
v 0
1
2
[
1 + sinθ
]
a
b
2
dθcosθ
Finally you can do the two terms of the integral: Look at the second term first. You can of course start grinding
away and find the right trigonometric formula to do the integral, OR, you can sketch a graph of the integrand,
sinθcosθ, on the interval −π/ 2 < θ < π/ 2 and write the answer down by inspection. The first part of the
integral is
v 0
ab
4
∫π/ 2
−π/ 2
cosθ=v 0
ab
4
sinθ
∣
∣
∣
∣
π/ 2
−π/ 2
=v 0
ab
2