Euler's Equations, a freely rotating lamina

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The discussion focuses on proving that the magnitude of the angular velocity component in the plane of a freely rotating lamina remains constant, utilizing Euler's equations. It is established that with no external torques acting on the lamina, the angular velocities satisfy W1 and W2 equations derived from the equations of motion. The key point is to demonstrate that the time derivative of the sum of the squares of the angular velocities (ω1² + ω2²) is zero. A suggestion is made to use the relationship between the eigenvalues and the angular velocities to support the proof. The conclusion emphasizes that if the lamina rotates about a principal axis, the angular velocity components in the plane would be zero, confirming the constancy of the magnitude.
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Homework Statement


Consider a lamina rotating freely (no torques) about a point O of the lamina. Use Euler's equations to show that the component of \omega in the plane of the lamina has constant magnitude.

[Hint: Use the reults of Problems 10.23 and 10.30. According to Problem 10.30, if you choose the direction e3 normal to the plane of the lamina, e3 points along a principal axis. Then what you have to prove is that the time derivative of \omega_{1}^{2} + \omega_{2}^{2} is zero.]


Homework Equations


The result of 10.23 is that Izz = Ixx + Iyy
The result of 10.30 is that for a lamina rotating about a point O in the body, the axis through O and perpendicular to the plane is a principal axis.

Euler's equations, as given in my book, are
y1W1 - (y2 - y1)w2w3 = N1
y2W2 - (y3 - y1)w3w1 = N2
y3W3 - (y1 - y2)w1w2 = N3
where y is lambda, the eigenvalue, w is omega, W is omega dot, and N is the torque.

The Attempt at a Solution


If the lamina is rotating freely, the N1=N2=N3=0.
If I choose e3 to be normal to the plane of the lamina, then e3 points along a principal axis, and that means that

w3 = constant,
so
W3 = 0.

Those last two statements I'm not sure about.

However, I still know that I would like to prove that the time derivative of w1^2 + w2^2 = 0. That is,

2w1W1 + 2w2W2 = 0

And solving Euler's equations for W1 and W2, with N1,2,3 = 0, you have

W1 = ((y2-y3)/y1)w2w3
W2 = ((y3-y1)/y2)w3w1

Plugging these into 2w1W1 + 2w2W2 = 0 and doing algebra, I found that, if 2w1W1 + 2w2W2 = 0 is true, then

y2^2 - y2y3 + y1y3 - y1^2 = 0.

Which doesn't seem to necessarily be true.

Help? Thank you!
 
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I don't believe that you can assume that w3 is constant. The problem does not state that the lamina is rotating about a principal axis. Instead, use the result you quoted (\lambda_{3}=\lambda_{1}+\lambda_{2}) and use Euler's equations to show that

\omega_{1}\omega_{1}^{.}+\omega_{2}\omega_{2}^{.}=0

Also, if the lamina WERE rotating about its principal axis that is perpendicular to the surface then the angular velocity would always point along this direction in the absence of torques and\omega_{1} and \omega_{2} would be zero.
 
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Oops. Those dots were supposed to be above omega one and omega two. I'm sure you get the idea though.
 
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