All Exams Test series for 1 year @ ₹349 only
Question

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 correct answer is ωp < ωd < ωn

Forced Single Degree-of-Freedom System Analysis

The question asks us to determine the correct relationship between three important frequencies in a forced single degree-of-freedom system:

  • Undamped Natural Frequency (\(\omega_n\)): This is the frequency at which the system would oscillate if there were no damping and no external forces. It is inherent to the system's mass and stiffness properties.
  • Damped Natural Frequency (\(\omega_d\)): This is the frequency at which the system oscillates when disturbed and allowed to vibrate freely under damped conditions (transient response).
  • Peak Amplitude Frequency (\(\omega_p\)): This is the forcing frequency at which the amplitude of the forced steady-state response reaches its maximum value. For damped systems, this is often referred to as the resonant frequency.

Understanding Key Frequencies in Damped Systems

Let's first define the relevant frequencies based on standard vibration theory:

  1. 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 \(\omega_n\).

  2. 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 (\(\zeta < 1\)).

  3. 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, \(f(r) = (1 - r^2)^2 + (2\zeta r)^2\).

Deriving Peak Amplitude Frequency (\(\omega_p\))

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).

Comparing Damped Natural Frequency (\(\omega_d\)) and Undamped Natural Frequency (\(\omega_n\))

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):

\[ \omega_n \sqrt{1 - \zeta^2} < \omega_n \] \[ \omega_d < \omega_n \]

Comparing Peak Amplitude Frequency (\(\omega_p\)) and Damped Natural Frequency (\(\omega_d\))

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 \(\omega_n\):

\[ \omega_n \sqrt{1 - 2\zeta^2} < \omega_n \sqrt{1 - \zeta^2} \] \[ \omega_p < \omega_d \]

Final Relationship Between Frequencies

Combining the inequalities we derived:

  • \(\omega_d < \omega_n\)
  • \(\omega_p < \omega_d\)

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 \(\omega_p < \omega_d < \omega_n\).

Was this answer helpful?

Important Questions from Forced Vibration

  1. Which method is used to find the natural frequencies of a system with multi degrees of freedom?

  2. 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

  3. When the frequency of the forced vibration is equal to the frequency of the free vibration, this condition is called ______.

  4. The amplitude of the steady-state reaction divided by the static deflection under force application is known as _______.

  5. The amplitude ratio of two successive oscillations of a damped vibratory system is

Need Expert Advice?

Start Your Preparation with Prepp Mobile App

Download the app from Google Play & App Store
Download the app from Google Play & App Store
Prepp Mobile App