Moment of inertia of hemispherical shell

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Homework Help Overview

The problem involves calculating the moment of inertia of a hemispherical shell about the z-axis, given a specific mass distribution defined by a surface density function. The original poster expresses confusion regarding the relationship between the total mass and the moment of inertia, particularly why the expected result differs from their initial calculation.

Discussion Character

  • Exploratory, Assumption checking, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss the integration of the mass distribution in spherical coordinates and the implications of using the correct distance from the rotational axis in the moment of inertia formula. There is also a question regarding the units of the surface density constant, σ0.

Discussion Status

Some participants have made progress in understanding the integration process and the necessary adjustments for calculating the moment of inertia. However, there remains a lack of consensus on the correct approach to integrating certain terms, particularly regarding the integration of sin^5(φ).

Contextual Notes

Participants are working under the constraints of a homework problem, which may limit the information available and the methods they can use. There is an ongoing exploration of the assumptions related to the geometry and mass distribution of the hemispherical shell.

mishima
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Homework Statement


The distribution of mass on the hemispherical shell:

z=(R2-x2-y2)1/2

is given by

σ(x,y,z)=(σ0/R2)(x2+y2)

where σ0 is a constant. Find the moment of inertia about the z-axis of the hemispherical shell.

Homework Equations


I=∫r2dm


The Attempt at a Solution


r2 is just R2. ∫dm in spherical coordinates is:

σ0R2∫∫sin3θ dθ d(phi)

with boundaries 0 to pi/2 for θ, and 0 to 2pi for phi. The completed definite integral representing the total mass is then:

(4pi/3) σ0R2.

I feel pretty confident about that, since it is given in the back of the book as the first step in the problem. What I don't understand is why the moment of inertia is anything more than just this value times another R2 to give:

(4pi/3) σ0R4.

The answer is supposed to be:

(16pi/15) σ0R4.

So, I'm guessing there's something more to the calculation of moment of inertia. I've been looking through the different derivations of moments but can't see how to get the right factor. I could use a hint.
 
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Oh, I understand why I can't do it that way. r in the moment of inertia formula is measured from the center of mass and is not equal to R in this case.
 
What are the units of sigma0?
 
None given, but the sigma function is a mass per area so I guess it represents an average mass density, or "baseline" mass density that then varies according to the more general function.
 
Yay, got it.

∫∫r2σdA

r in the formula for moment of inertia can be put into spherical coordinates and integrated over the whole hemisphere (also in spherical).

σ0R4∫∫sin5dθ d(phi)

The first integral makes the 8/15 factor needed and the second of course is 2 pi. I guess this was a fairly simple problem after all.
 
mishima said:
Oh, I understand why I can't do it that way. r in the moment of inertia formula is measured from the center of mass and is not equal to R in this case.

I follow this, but do you mean to say rotational axis, not center of mass? The center of mass would be a point. If r is distance from the rotational axis then we can let r=p*sin[itex]\phi[/itex], or in this case r=R*sin[itex]\phi[/itex].

mishima said:
Yay, got it.

∫∫r2σdA

r in the formula for moment of inertia can be put into spherical coordinates and integrated over the whole hemisphere (also in spherical).

σ0R4∫∫sin5dθ d(phi)

The first integral makes the 8/15 factor needed and the second of course is 2 pi. I guess this was a fairly simple problem after all.

I follow this and it makes sense, but when I integrated sin^5[itex]\phi[/itex], I got

-5 Cos[x] 5 Cos[3 x] Cos[5 x]
--------- + ----------- - ----------
8....48....80

which, when integrated from [o,∏/2], equals zero.
 

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