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Next, we need to find the total mass of the rectangle. Let ρ represent the density of the lamina (note that ρ is a constant). In this case, ρ is expressed in terms of mass per unit area. Thus, to find the total mass of the rectangle, we multiply the area of the rectangle by ρ . Then, the mass of the rectangle is given by ρ f ( x i * ) Δ x .

To get the approximate mass of the lamina, we add the masses of all the rectangles to get

m i = 1 n ρ f ( x i * ) Δ x .

This is a Riemann sum. Taking the limit as n gives the exact mass of the lamina:

m = lim n i = 1 n ρ f ( x i * ) Δ x = ρ a b f ( x ) d x .

Next, we calculate the moment of the lamina with respect to the x -axis. Returning to the representative rectangle, recall its center of mass is ( x i * , ( f ( x i * ) ) / 2 ) . Recall also that treating the rectangle as if it is a point mass located at the center of mass does not change the moment. Thus, the moment of the rectangle with respect to the x -axis is given by the mass of the rectangle, ρ f ( x i * ) Δ x , multiplied by the distance from the center of mass to the x -axis: ( f ( x i * ) ) / 2 . Therefore, the moment with respect to the x -axis of the rectangle is ρ ( [ f ( x i * ) ] 2 / 2 ) Δ x . Adding the moments of the rectangles and taking the limit of the resulting Riemann sum, we see that the moment of the lamina with respect to the x -axis is

M x = lim n i = 1 n ρ [ f ( x i * ) ] 2 2 Δ x = ρ a b [ f ( x ) ] 2 2 d x .

We derive the moment with respect to the y -axis similarly, noting that the distance from the center of mass of the rectangle to the y -axis is x i * . Then the moment of the lamina with respect to the y -axis is given by

M y = lim n i = 1 n ρ x i * f ( x i * ) Δ x = ρ a b x f ( x ) d x .

We find the coordinates of the center of mass by dividing the moments by the total mass to give x = M y / m and y = M x / m . If we look closely at the expressions for M x , M y , and m , we notice that the constant ρ cancels out when x and y are calculated.

We summarize these findings in the following theorem.

Center of mass of a thin plate in the xy -plane

Let R denote a region bounded above by the graph of a continuous function f ( x ) , below by the x -axis, and on the left and right by the lines x = a and x = b , respectively. Let ρ denote the density of the associated lamina. Then we can make the following statements:

  1. The mass of the lamina is
    m = ρ a b f ( x ) d x .
  2. The moments M x and M y of the lamina with respect to the x - and y -axes, respectively, are
    M x = ρ a b [ f ( x ) ] 2 2 d x and M y = ρ a b x f ( x ) d x .
  3. The coordinates of the center of mass ( x , y ) are
    x = M y m and y = M x m .

In the next example, we use this theorem to find the center of mass of a lamina.

Finding the center of mass of a lamina

Let R be the region bounded above by the graph of the function f ( x ) = x and below by the x -axis over the interval [ 0 , 4 ] . Find the centroid of the region.

The region is depicted in the following figure.

This figure is the graph of the curve f(x)=squareroot(x). It is an increasing curve in the first quadrant. Under the curve above the x-axis there is a shaded region. It starts at x=0 and is bounded to the right at x=4.
Finding the center of mass of a lamina.

Since we are only asked for the centroid of the region, rather than the mass or moments of the associated lamina, we know the density constant ρ cancels out of the calculations eventually. Therefore, for the sake of convenience, let’s assume ρ = 1 .

First, we need to calculate the total mass:

m = ρ a b f ( x ) d x = 0 4 x d x = 2 3 x 3 / 2 | 0 4 = 2 3 [ 8 0 ] = 16 3 .

Next, we compute the moments:

M x = ρ a b [ f ( x ) ] 2 2 d x = 0 4 x 2 d x = 1 4 x 2 | 0 4 = 4

and

M y = ρ a b x f ( x ) d x = 0 4 x x d x = 0 4 x 3 / 2 d x = 2 5 x 5 / 2 | 0 4 = 2 5 [ 32 0 ] = 64 5 .

Thus, we have

x = M y m = 64 / 5 16 / 3 = 64 5 · 3 16 = 12 5 and y = M x y = 4 16 / 3 = 4 · 3 16 = 3 4 .

The centroid of the region is ( 12 / 5 , 3 / 4 ) .

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Source:  OpenStax, Calculus volume 2. OpenStax CNX. Feb 05, 2016 Download for free at http://cnx.org/content/col11965/1.2
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