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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
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