Consider a forced single degree-of-freedom system governed by \(\rm \ddot x(t) + 2 ζ ω_n \dot x (t) + ω_n^2 x(t) = ω_n^2 \cos (ω t)\), where ζ and ωn are the damping ratio and undamped natural frequency of the system, respectively, while ω is the forcing frequency. The amplitude of the forced steady state response of this system is given by [(1 − r2)2 + (2ζr)2]-1/2, where 𝑟 = ω/ω n. The peak amplitude of this response occurs at a frequency ω = ωp. If ωd denotes the damped natural frequency of this system, which one of the following options is true?
The question asks us to determine the correct relationship between three important frequencies in a forced single degree-of-freedom system:
Let's first define the relevant frequencies based on standard vibration theory:
Undamped Natural Frequency (\(\omega_n\)):
From the given differential equation \(\rm \ddot x(t) + 2 \zeta \omega_n \dot x (t) + \omega_n^2 x(t) = \omega_n^2 \cos (\omega t)\), the undamped natural frequency is directly identified as \(\omega_n\).
Damped Natural Frequency (\(\omega_d\)):
The damped natural frequency is given by the formula:
\[ \omega_d = \omega_n \sqrt{1 - \zeta^2} \]
Here, \(\zeta\) is the damping ratio. For a system to oscillate (underdamped), \(\zeta\) must be less than 1 (\(\zeta < 1\)).
Peak Amplitude Frequency (\(\omega_p\)):
This is the frequency at which the amplitude of the steady-state response is maximum. The problem provides the amplitude of the forced steady-state response as:
\[ A = [(1 - r^2)^2 + (2\zeta r)^2]^{-1/2} \]
where \(r = \omega/\omega_n\). To find the frequency at which this amplitude is maximum, we need to find the value of \(r\) that maximizes \(A\). Maximizing \(A\) is equivalent to minimizing its denominator, \(f(r) = (1 - r^2)^2 + (2\zeta r)^2\).
To find the value of \(r\) that minimizes \(f(r)\), we differentiate \(f(r)\) with respect to \(r\) and set the derivative to zero:
Let \(f(r) = (1 - r^2)^2 + (2\zeta r)^2\)
Expand the terms:
\[ f(r) = (1 - 2r^2 + r^4) + (4\zeta^2 r^2) \] \[ f(r) = r^4 + (4\zeta^2 - 2)r^2 + 1 \]
Now, differentiate \(f(r)\) with respect to \(r\):
\[ \frac{df(r)}{dr} = 4r^3 + 2(4\zeta^2 - 2)r \]
Set the derivative to zero to find the critical points:
\[ 4r^3 + (8\zeta^2 - 4)r = 0 \] \[ 4r(r^2 + 2\zeta^2 - 1) = 0 \]
Since \(r = \omega/\omega_n\), and for a non-zero resonant frequency, \(r \neq 0\), we consider the second factor:
\[ r^2 + 2\zeta^2 - 1 = 0 \] \[ r^2 = 1 - 2\zeta^2 \]
Since \(r = \omega_p/\omega_n\) at peak amplitude, let's denote this specific \(r\) as \(r_p\):
\[ r_p = \sqrt{1 - 2\zeta^2} \]
Substituting \(r_p = \omega_p/\omega_n\):
\[ \frac{\omega_p}{\omega_n} = \sqrt{1 - 2\zeta^2} \] \[ \omega_p = \omega_n \sqrt{1 - 2\zeta^2} \]
For \(\omega_p\) to be a real frequency, the term inside the square root must be non-negative: \(1 - 2\zeta^2 \ge 0\), which implies \(\zeta^2 \le 1/2\), or \(\zeta \le 1/\sqrt{2}\) (\(\approx 0.707\)). If \(\zeta\) is greater than \(1/\sqrt{2}\), the maximum amplitude occurs at \(\omega = 0\) (static deflection).
We have \(\omega_d = \omega_n \sqrt{1 - \zeta^2}\).
For any real damped system, the damping ratio \(\zeta\) is positive (\(\zeta > 0\)) and typically less than 1 for underdamped systems. Therefore, \(\zeta^2 > 0\).
This implies:
\[ 1 - \zeta^2 < 1 \] \[ \sqrt{1 - \zeta^2} < 1 \]
Multiplying by \(\omega_n\) (which is positive):
\[ \omega_n \sqrt{1 - \zeta^2} < \omega_n \] \[ \omega_d < \omega_n \]
We have \(\omega_p = \omega_n \sqrt{1 - 2\zeta^2}\) and \(\omega_d = \omega_n \sqrt{1 - \zeta^2}\).
Since \(\zeta > 0\), it follows that \(2\zeta^2 > \zeta^2\).
This means:
\[ 1 - 2\zeta^2 < 1 - \zeta^2 \]
Taking the square root (and assuming \(\zeta \le 1/\sqrt{2}\) so that both terms are real):
\[ \sqrt{1 - 2\zeta^2} < \sqrt{1 - \zeta^2} \]
Multiplying by \(\omega_n\):
\[ \omega_n \sqrt{1 - 2\zeta^2} < \omega_n \sqrt{1 - \zeta^2} \] \[ \omega_p < \omega_d \]
Combining the inequalities we derived:
Therefore, the overall relationship is:
\[ \omega_p < \omega_d < \omega_n \]
This relationship holds true for underdamped systems with damping ratios \(\zeta \le 1/\sqrt{2}\), which is the usual context for such problems to have a distinct resonant peak.
| Frequency Type | Formula | Description |
|---|---|---|
| Undamped Natural Frequency (\(\omega_n\)) | \(\omega_n\) | Inherent frequency without damping. |
| Damped Natural Frequency (\(\omega_d\)) | \(\omega_n \sqrt{1 - \zeta^2}\) | Frequency of free oscillation with damping. |
| Peak Amplitude Frequency (\(\omega_p\)) | \(\omega_n \sqrt{1 - 2\zeta^2}\) | Forcing frequency at which steady-state amplitude is maximum. |
Based on our derivation and comparison, the correct option is \(\omega_p < \omega_d < \omega_n\).
Which method is used to find the natural frequencies of a system with multi degrees of freedom?
The ratio of the amplitude of the steady-state response of forced vibrations to the static deflection under the action of a static force is known as
When the frequency of the forced vibration is equal to the frequency of the free vibration, this condition is called ______.
The amplitude of the steady-state reaction divided by the static deflection under force application is known as _______.
The amplitude ratio of two successive oscillations of a damped vibratory system is