Finding the centre of mass of a hemispherical shell

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SUMMARY

The discussion focuses on methods to find the center of mass (COM) of a hemispherical shell. Two primary methods are highlighted: the first involves using the surface area ratio to derive the mass element, leading to a COM of R/2; the second method utilizes volume integration with a variable radius, ultimately simplifying to the same result. Additionally, a third method is presented, which projects an area element from the x-y plane onto the hemisphere, confirming the COM at R/2 through surface mass density calculations.

PREREQUISITES
  • Understanding of integration in cylindrical and spherical coordinates
  • Familiarity with surface area and volume elements in physics
  • Knowledge of mass density concepts
  • Basic principles of center of mass calculations
NEXT STEPS
  • Study the derivation of center of mass for different geometric shapes
  • Learn advanced integration techniques in spherical coordinates
  • Explore applications of surface mass density in physics problems
  • Investigate the implications of varying density in center of mass calculations
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Physics students, educators, and anyone interested in advanced mechanics, particularly in calculating the center of mass for complex shapes like hemispherical shells.

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Homework Statement


Hey everyone,
I'm studying for my physics and came across a question for the COM of a hemisphere. However, I was wondering what methods there are to find the COM of a hemispherical shell instead. Any insight would be very much appreciated! =)
After much of tearing Google apart in order to find a solution, I found 2, but was wondering if there were any more methods (I always like to find as many solutions as possible because it really helps me understand).

Homework Equations


I just learned integration in cylindrical and spherical coordinates, so I kinda know that:
x_\textrm {COM}=\frac{\int x dm}{\int dm}
dA = r^2 \sin\theta\ d\theta\ d\phi
dV = r^2 \sin\theta\ dr\ d\theta\ d\phi
where \theta is the polar angle, and \phi is the angle about the equator (I learned it this way, but I think most people use \phi as the polar angle instead)

The Attempt at a Solution


The 2 methods I found were:
1. Expressing dA as a ratio of the total SA, and this would be equal to the ratio of dm/M; i.e. that \frac{dA}{2\pi r^2} = \frac{dm}{M} (OMG this TeXnology is so cool!)
ANYWAY so with this, you would be able to
  • find dm
  • find that z=r \cos \theta, where z is the axis passing through the apex and centre of the hemisphere.
and plug it all into the equation, giving R/2. YAY!

2. A bit more complicated but really nifty way was to call big radius R, and the one on the closer side of the shell \kappa R, where 0\leq k\leq 1.
Then
\textrm {Total Volume} = \frac{2}{3}\pi R^3 (1-{\kappa}^3)
Once again, z=r \cos \theta and dV = r^2 \sin\theta\ dr\ d\theta\ d\phi \Rightarrow dm = \rho r^2 \sin\theta\ dr\ d\theta\ d\phi where \rho is density. From here, you can place into the formula, and end up with
\frac{3R(1-{\kappa}^4)}{8(1-{\kappa}^3)}.
Now, as 1-{\kappa}^4 = (1-\kappa)(1+\kappa+{\kappa}^2+{\kappa}^3) and 1-{\kappa}^3 = (1-\kappa)(1+\kappa+{\kappa}^2), you can simplify this.
For a spherical shell, you just take \lim_{\substack{x \rightarrow 1}}, and that gives you R/2 again!
 
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Those methods look good.

For fun, here's another way. Consider the figure below:
1656956429281.png

Let ##dA_{xy}## be an element of area under the hemisphere on the x-y plane. If you project that area up onto the curved surface of the hemisphere, you get a patch on the hemisphere with area ##dA_H = \large \frac{dA_{xy}}{\cos \theta}##, where ##\theta## is the angle between the normal vector ##\hat n## on the hemisphere and the z-axis. The z-coordinate of the patch is ##z = R \cos \theta##.

Let ##\sigma## denote the uniform surface mass density of the hemisphere. Then, $$z_{\rm cm} = \frac{1}{M} \int{z \, dm} = \frac{1}{M} \int {z \, \sigma \, dA_H} = \frac{\sigma}{M} \int(R \cos \theta) \frac{dA_{xy}}{\cos \theta} = \frac{\sigma}{M} R \int dA_{xy} = \frac{\sigma}{M} R \left(\pi R^2\right)$$

Using ##\sigma = \large \frac{M}{2 \pi R^2}## gives the result ##z_{\rm cm} = R/2.##
 
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