Canonical definition of Angular Momentum,

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The discussion focuses on the definition and calculation of angular momentum for a solid body rotating around a fixed axis. The angular momentum is expressed as an integral involving the position vector and the velocity of mass elements. The user seeks clarification on simplifying a specific term in the angular momentum equation when the center of mass is on the axis of rotation. There is confusion regarding the application of trigonometric functions in the derivation, particularly when considering the rotation of the body. The user references a derivation from a book but is uncertain about the transition between equations and the implications of the body's rotation.
guv
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Let's start with an arbitrary solid body rotating around a fixed axis of rotation with angular velocity ##\vec \omega## in the ## \hat z## direction. For simplicity, let's say the origin O is on the axis of rotation. Take a look at the picture I sketched in the next post. Tried my best to be clear about the notations I used in my derivation.

By definition, $$\vec L = \int_{\Omega} \vec r \times (dm \; \vec v) = \int_{\Omega} \vec r \times (\vec \omega \times \vec r) dm$$

Where ##\vec r## is is position position vector of dm from origin O and ##\Omega## is the domain of integration (the entire solid body).

If the angle between axis of rotation and position vector is ##\theta## (imagine ##\hat z## points upward from O, ##\vec r## points to the upper right from O), then
$$\vec L = \int r^2 \omega sin(\theta) dm \hat L$$

where ##\hat L## is a unit vector from dm perpendicular from ##\vec r## (imagine this unit vector from dm going upper left from dm)

We can decompose this ##\hat L## into its z direction component and a radial component.
$$\vec L = \int r^2 \omega sin^2\theta \hat z dm + \int r^2 \omega sin\theta cos\theta (-\hat p) dm$$

Here is ##\hat p## is a unit vector pointing outward from dm perpendicular to axis of rotation.

If ##\omega## is a constant, then
$$\int r^2 \omega sin^2\theta \hat z dm = \omega \int r^2 sin^2\theta dm \hat z = I_{zz} \omega \hat z$$

This is the z component of the angular moment since the ##\vec \omega = (0, 0, \omega)##.

My problem is I couldn't really simply ##\int r^2 \omega sin\theta cos\theta (-\hat p) dm## into 0 when center of mass is on the axis of rotation. Can someone help? Thanks,

guv
 
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sketch55ce836b7da65.png
 
The Center of Mass ##\vec R_{cm}## is defined by ##\int_{\Omega} (\vec r - \vec R_{cm}) \; dm \equiv 0##.

My question is inspired by the derivation in Louis Brand's "Vector Analysis" book, p.176-177 when the author jumps from eq. (2) to eq. (3). I couldn't complete this derivation.
 
Is the body rotating?? In that case doesn't sin\theta and cos\theta becomes sin pi/2 and cos pi/2? so one of the trigonometric ratio becomes 0. Not sure though, got to think. Better wait for someone else's reply.
 

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