9—Vector Calculus 1 252y
xθk+1nˆk
bθkˆy
ˆxyb/ 2(b/2) sinθThe 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 0yk
bˆx.ab
2∆θknˆkThe value ofykat the angleθkis
yk=b
2+
b
2sinθk, soyk
b=
1
2
[1 + sinθk]Put the pieces together and you have
v 01
2
[
1 + sinθk]
xˆ.ab
2∆θk[
ˆxcosθk+yˆsinθk]
=v 01
2
[
1 + sinθk]
ab
2∆θkcosθkThe total flow is the sum of these overkand then the limit as∆θk→ 0.
lim
∆θk→ 0∑
kv 01
2
[
1 + sinθk]
ab
2∆θkcosθk=∫π/ 2−π/ 2v 01
2
[
1 + sinθ]
ab
2dθcosθFinally 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 0ab
4∫π/ 2−π/ 2cosθ=v 0ab
4sinθ∣
∣
∣
∣
π/ 2−π/ 2=v 0ab
2