Perturbed circular orbit under central force motion?

AI Thread Summary
The discussion revolves around a confusion regarding the derivation of an equation in Kleppner and Kolenkow's "Introduction to Mechanics," specifically in the context of central force motion. The user initially struggles with understanding how to apply the second derivative of the effective potential energy, U_{eff}, and the substitution of a previously derived value for angular momentum, l. After some reflection and clarification, the user realizes the mistake of not substituting the value of l earlier in the process. The conversation highlights the common learning experience of grappling with complex mechanics concepts and ultimately finding clarity. The exchange emphasizes the importance of careful calculation and the learning process in physics.
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I am self studying Kleppner and Kolenkow's an Introduction to mechanics. But i have one doubt about how they got into the equation no 3 of the example problem 9.3 in Central Force Motion.
Please clarify my doubt.
 
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I suggest you quote it or give a link.
 
Here i have attached the photo graph of that page.
mathman said:
I suggest you quote it or give a link.
 

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Seems pretty straight forward. Differentiate U_{eff} twice, evaluate it at r=r_0 and replace l by the one we obtained earlier. This should equal k, which is related to beta.
 
diegzumillo said:
Seems pretty straight forward. Differentiate U_{eff} twice, evaluate it at r=r_0 and replace l by the one we obtained earlier. This should equal k, which is related to beta.
Omg. I am so dumb. I just calculated the second derivative and then used to sit brooding over what to do next without plugging the value of l from equation 1. I am feeling embarrassed.

Anyway,,, thank you. I got it. Better late than never.
 
No problem :) This is just the peeking-over-the-shoulder effect.
 
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