Walczyk
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A mass m moves along the x-axis subject to an attractive force given by \frac {17} {2} \beta^2 m x and a retarding force given by 3 \beta m \dot{x}, where x is its distance from the origin and \beta is a constant. A driving force given by m A \cos{\omega t} where A is a constant, is applied to the particle along the x-axis. What value of \omega results in steady-state oscillations about the origin with maximum amplitude? What is the maximum amplitude?
Here's what I've done:
This is the differential equation I've come up with:
m \ddot{x} + 3 \beta m \dot{x} + \frac{17}{2} \beta^2 m x = m A \cos{\omega t}
I'm pretty sure these two steps are the correct ones to make, my textbooks uses this approach:
A \cos{\omega t} = A e^{i \omega t}
x(t) = A_2 e^{i(\omega t - \theta)
This is what I got after plugging in x(t) and solving the derivitives, and dropping the m term:
-A_2 \omega^2 e^{i(\omega t - \theta)} + A_2 3 i \beta \omega e^{i(\omega t - \theta)} + A_2 e^{i(\omega t - \theta)} = A e^{i \omega t}
This is after I eliminated e^{i \omega t} and moved e^{-i \theta}:
A_2(\frac {17} {2} \beta^2 - \omega^2 + 3 i \beta \omega) = A e^{i \theta}
These are the equations I got after applying Euler's identity:
A_2(\frac {17} {2} \beta^2 - \omega^2) = A \cos{\theta}
A_2 3 \beta \omega = A \sin{\theta}
I divided one equation by the other for \theta:
tan{\theta} = \frac {3 \beta \omega} {\frac {17} {2} \beta^2 - \omega^2}
I squared and added both equation's then solved for A^2_2:
A^2_2 = \frac {A^2} {\omega^4 - 8 \beta^2 \omega^2 + \frac {289} {4} \beta^4}
edit: I solved it on my own. Thanks for nothing!
Taking the derivitive of the last equation with respect to \omega:
A'_2(\omega) = A \omega (\omega^4 - 8 \beta \omega + \frac {289} {4} \beta^4)^{-3/2} (8 \beta^2 - 2 \omega^2)
Setting A'_2 = 0 and recognizing that \omega = 0 is an arbitrary solution 8 \beta^2 - 2 \omega^2 = 0.
Therefore \omega_r = 2 \beta.
For the second part of the problem I plug \omega_r into A_2(\omega):
A_2(\omega_r) = A(\frac {225} {4} \beta^4)^{\frac {-1} {2}}
The final result!:
A_2(\omega_r) = \frac {2 A} {15 \beta^2}
Here's what I've done:
This is the differential equation I've come up with:
m \ddot{x} + 3 \beta m \dot{x} + \frac{17}{2} \beta^2 m x = m A \cos{\omega t}
I'm pretty sure these two steps are the correct ones to make, my textbooks uses this approach:
A \cos{\omega t} = A e^{i \omega t}
x(t) = A_2 e^{i(\omega t - \theta)
This is what I got after plugging in x(t) and solving the derivitives, and dropping the m term:
-A_2 \omega^2 e^{i(\omega t - \theta)} + A_2 3 i \beta \omega e^{i(\omega t - \theta)} + A_2 e^{i(\omega t - \theta)} = A e^{i \omega t}
This is after I eliminated e^{i \omega t} and moved e^{-i \theta}:
A_2(\frac {17} {2} \beta^2 - \omega^2 + 3 i \beta \omega) = A e^{i \theta}
These are the equations I got after applying Euler's identity:
A_2(\frac {17} {2} \beta^2 - \omega^2) = A \cos{\theta}
A_2 3 \beta \omega = A \sin{\theta}
I divided one equation by the other for \theta:
tan{\theta} = \frac {3 \beta \omega} {\frac {17} {2} \beta^2 - \omega^2}
I squared and added both equation's then solved for A^2_2:
A^2_2 = \frac {A^2} {\omega^4 - 8 \beta^2 \omega^2 + \frac {289} {4} \beta^4}
edit: I solved it on my own. Thanks for nothing!
Taking the derivitive of the last equation with respect to \omega:
A'_2(\omega) = A \omega (\omega^4 - 8 \beta \omega + \frac {289} {4} \beta^4)^{-3/2} (8 \beta^2 - 2 \omega^2)
Setting A'_2 = 0 and recognizing that \omega = 0 is an arbitrary solution 8 \beta^2 - 2 \omega^2 = 0.
Therefore \omega_r = 2 \beta.
For the second part of the problem I plug \omega_r into A_2(\omega):
A_2(\omega_r) = A(\frac {225} {4} \beta^4)^{\frac {-1} {2}}
The final result!:
A_2(\omega_r) = \frac {2 A} {15 \beta^2}
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