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Calculus 2nd Edition Rogawski

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308 CHAPTER 6 APPLICATIONS OF THE INTEGRAL<br />

Why is this formula true? Let’s fix an observation point P in the tube and ask: Which fluid<br />

particles flow past P in a 1-min interval? A particle travels v centimeters each minute, so<br />

it flows past P during this minute if it is located not more than v centimeters to the left of<br />

P (assuming the fluid flows from left to right). Therefore, the column of fluid flowing past<br />

P in a 1-min interval is a cylinder of radius R, length v, and volume πR 2 v (Figure 9).<br />

v cm<br />

FIGURE 9 The column of fluid flowing past<br />

P in one unit of time is a cylinder of<br />

volume πR 2 v.<br />

P<br />

R<br />

In reality, the fluid particles do not all travel at the same velocity because of friction.<br />

However, for a slowly moving fluid, the flow is laminar, by which we mean that the<br />

velocity v(r) depends only on the distance r from the center of the tube. The particles at<br />

the center of the tube travel most quickly, and the velocity tapers off to zero near the walls<br />

of the tube (Figure 10).<br />

FIGURE 10 Laminar flow: Velocity of fluid<br />

increases toward the center of the tube.<br />

r<br />

P<br />

R<br />

v(r i )<br />

Ring of<br />

width r,<br />

Area ≈ 2πr i r<br />

If the flow is laminar, we can express the flow rate Q as an integral. We divide<br />

the circular cross-section of the tube into N thin concentric rings of width r = R/N<br />

(Figure 11). The area of the ith ring is approximately 2πr i r and the fluid particles<br />

flowing past this ring have velocity that is nearly constant with value v(r i ). Therefore, we<br />

can approximate the flow rate Q i through the ith ring by<br />

FIGURE 11 In a laminar flow, the fluid<br />

particles passing through a thin ring at<br />

distance r i from the center all travel at<br />

nearly the same velocity v(r i ).<br />

r i<br />

Q i ≈ cross-sectional area × velocity ≈ (2πr i r)v(r i )<br />

We obtain<br />

N∑<br />

N∑<br />

Q = Q i ≈ 2π r i v(r i )r<br />

i=1<br />

i=1<br />

The sum on the right is a right-endpoint approximation to the integral 2π<br />

Once again, we let N tend to ∞ to obtain the formula<br />

∫ R<br />

0<br />

rv(r) dr.<br />

Flow rate Q = 2π<br />

∫ R<br />

0<br />

rv(r) dr 5<br />

Note the similarity of this formula and its derivation to that of population with a radial<br />

density function.<br />

The French physician Jean Poiseuille<br />

(1799–1869) discovered the law of<br />

laminar flow that cardiologists use to study<br />

blood flow in humans. Poiseuille’s Law<br />

highlights the danger of cholesterol buildup<br />

in blood vessels: The flow rate through a<br />

blood vessel of radius R is proportional to<br />

R 4 , so if R is reduced by one-half, the flow<br />

is reduced by a factor of 16.<br />

EXAMPLE 6 Laminar Flow According to Poiseuille’s Law, the velocity of blood<br />

flowing in a blood vessel of radius R cm is v(r) = k(R 2 − r 2 ), where r is the distance<br />

from the center of the vessel (in centimeters) and k is a constant. Calculate the flow rate<br />

Q as function of R, assuming that k = 0.5 (cm-s) −1 .<br />

Solution By Eq. (5),<br />

Q = 2π<br />

∫ R<br />

0<br />

(0.5)r(R 2 − r 2 )dr = π<br />

) ∣ (R 2 r2<br />

2 − r4 ∣∣∣<br />

R<br />

= π 4 0 4 R4 cm 3 /s<br />

Note that Q is proportional to R 4 (this is true for any value of k).

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