Damped Oscillation Flashcards
Introduction to Damped Oscillation
Simple Harmonic Motion (SHM) is conventionally categorized as free oscillation.
In physical reality, free oscillations rarely sustain indefinitely; they decay over time due to various resistive or dissipative forces that steadily diminish the total energy of the mechanical system.
The inclusion of damping forces alters system dynamics in multiple ways, including the potential elimination of oscillatory behavior altogether, causing the system to return to equilibrium without oscillating.
Damped motion is categorized based on the mathematical relationship between the natural frequency of vibration and the damping factor .
Simple Harmonic Motion Primer
Definition 1: A particle executes Simple Harmonic Motion (SHM) if the net force acting upon it is directly proportional to its displacement relative to a designated origin and acts in the direction opposite to that displacement.
The governing differential equation of motion for SHM is:
In this formulation, represents the particle mass, denotes particle position as a function of time , represents instantaneous velocity, represents instantaneous acceleration, and is a constant stiffness parameter.
The differential equation can be expressed in canonical form as:
Here, is a constant parameter representing the natural frequency of the system, defined by .
Remark 1 (Linearity and Homogeneity):
Linearity: If and are two distinct solutions to , their linear combination (where and are arbitrary constants) is also a valid solution.
Homogeneity: The equation contains no non-zero terms independent of or its time derivatives. Consequently, the zero solution represents a valid trivial solution.
Derivation of the General Solution:
Substituting a trial exponential solution yields and .
Substitution into the canonical equation yields:
Because for all , the characteristic equation is , yielding complex roots
The general mathematical solution is:
Remark 2 (Physical Reality Condition):
Since measures real physical displacement, must equal its complex conjugate , yielding:
Differentiating with respect to time gives:
Summing these two equations yields . Because for all , , confirming that and are complex conjugates.
Writing (where and are real constants) yields the physical displacement form:
Determination of Integration Constants via Initial Conditions:
Case I (, ):
The first condition implies , while the second gives . The physical solution is:
Case II (, ):
The second condition implies , while the first gives . The physical solution is:

Definition 2: A non-trivial solution is classified as oscillatory if it intersects the -axis more than once within a specified time interval, and non-oscillatory if it intersects the -axis at most once within that interval.
Definition 3: Because , free SHM is periodic with time period T = \frac{2\text{\pi}}{\omega_0}, where represents the natural frequency.
Theorem 1 (Energy Conservation in SHM): The differential equation conserves the total mechanical energy
Proof: Multiplying by gives . Multiplying by mass yields:
For , the energy constant equals . Dividing energy by yields the normalized trajectory:
Remark 3 (Phase Space Representation):
The coordinate system defined by plotting displacement against velocity constitutes the Phase Space of the dynamical system.
The equation describes an ellipse in phase space. A closed trajectory in phase space signifies periodic motion.

Origin Dependency and Influence of Constant Forces:
SHM representation depends on the chosen origin. For example, describes simple harmonic oscillation centered at with frequency .
Under an additional constant force (acceleration unit), the equation of motion becomes:
Here, remains unchanged, but the equilibrium position shifts from to (such as a hanging spring-mass system in gravity where ).
Definition 4 (Time Average): The time average of a time-dependent physical quantity over period is defined as:
Remark 4 (Standard Harmonic Time Averages):
Constitutive Differential Equation of Damped Motion
In the presence of damping forces, the total mechanical energy decreases over time:
Assuming the resistive damping force is directly proportional to velocity, (where is a constant), the rate of energy loss equals dissipated power :
Remark 5 (Damping Factor):
The parameter is defined as the damping factor.
Dimensional analysis: , matching the dimensions of frequency.
Theorem 2 (Classification of Damped Solutions): The solutions of under initial conditions and are classified as:
Non-oscillatory when
Oscillatory when
Proof: Substituting the trial function into the differential equation:
Substitution into yields:
Because for all , the reduced equation for is:
Analysis of Overdamping (Large Damping: )
When , define .
The auxiliary equation becomes , yielding .
The general displacement function is:
Applying initial conditions and :
Solving for integration constants and yields:
The complete displacement equation is:
Time Axis Intersections: Setting determines when the path crosses the equilibrium axis:
Sub-case Analysis:
Case (a) (, ):
- Solving gives as the sole axis crossing.
Case (b) (, ):
- Evaluating yields . Because is negative, the displacement curve never intersects the -axis for 

Case (c) (Arbitrary Initial Conditions , ):
- If ( and share the same sign, meaning the particle is pushed away from origin), the logarithmic argument is strictly less than , yielding (no physical crossing for ).
- If (particle is projected back toward origin):
- If , exists. The particle crosses the origin once before asymptotic return as
- If or , no positive real solution for exists.
- Expressed in terms of initial velocity :



Turning Point Dynamics:
For Case (a), setting gives:
Case (b) exhibits no turning point. Highly damped non-oscillatory behavior of this type is described as dead beat.
Analysis of Critical Damping ()
When , .
The general displacement function is:
Applying initial conditions and gives and , yielding:
Time Axis Intersections: Setting yields:
Specific Cases:
For , : , crossing the time axis only at
For , : , yielding (no positive intersection).


Parametric Crossing Conditions:
For () and :
- Positivity of requires .
For and ():
- Positivity of requires .



Turning Point Analysis: For and :
Critical damping provides the fastest rate of decay to equilibrium without overshoot or oscillation.
Analysis of Weak Damping ()
When , define
The differential equation for becomes , with general solution .
Applying initial conditions and :
Solving for and yields:
Substituting and into produces:
In this expression, amplitude envelope and phase angle are defined by:
Specific Initial Condition Examples:
Case 1 (, ):
Case 2 (, ):


Quasi-Periodicity and Extrema Characteristics:
Zero-crossings occur at time intervals separated by . The quasi-period is .
The time interval between a maximum and the subsequent minimum is , though extrema do not fall precisely halfway between zero-crossings.
Extrema occur when :
In the limit as , .
Energy, Power Dissipation, and Characteristics of Weakly Damped Oscillations
Energy Derivation under Weak Damping ():
Writing displacement as , where is the time-decaying amplitude.
The total instantaneous energy expands to:
Over one quasi-period , assuming changes negligibly over single cycles (), time averaging yields:
The cycle-averaged total energy is:
In this expression, and

Power Dissipation:
Instantaneous power dissipated by resistive force:
Cycle-averaged dissipated power over :
Logarithmic Decrement:
Consider displacement peaks at quarter-period offsets

Absolute amplitude values at successive half-period intervals:
Ratio of successive amplitudes:
For consecutive peaks:
Definition 5: Logarithmic decrement is the natural logarithm of the ratio of two successive amplitudes separated by a half period :
Relaxation Time:
Definition 6: Relaxation time is the time required for the amplitude to decay to of its initial magnitude.
Remark 9: Relationship between logarithmic decrement and relaxation time :
Quality Factor (-Value):
From , multiplying both sides by yields:
Definition 7: Quality factor is defined physically as:
Solved Worked Examples and Practice Problems
Problem 1: The governing differential equation of a damped system is given by
(i) Find damping factor and natural frequency for :
Divide equation by :
- Comparing with gives and .
(ii) Find conditions on for large, critical, and weak damping:
Large damping ():
Critical damping ():
Weak damping ():
(iii) Find for if and :
Weakly damped general solution:
Here .
Applying initial conditions: , and .
Displacement function:
(iv) Repeat (iii) for initial conditions and :
, and 3 = -\gamma A + \tilde{\omega} B \implies 3 = -(0.001)(5) + 5 B \implies B = \frac{3.005}{5} = 0.601$.\n - Solution: x(t) = e^{-0.001 t}\left[5 \cos(5t) + 0.601 \sin(5t)\right].\n\n- **Problem 2:** A massless string suspended from a rigid rod carries a mass of 200\,\text{g}0.2\,\text{s}30\,\text{s}. Calculate (a) relaxation time, (b) quality factor, and (c) logarithmic decrement.\n - **Solution:**\n - **(a) Relaxation Time:** Using A(t) = A(0)e^{-\gamma t}\gamma t = \ln\left(\frac{A(0)}{A(t)} ight)t = 30\,\text{s}\frac{A(0)}{A(30)} = 2:\n\n\gamma (30) = \ln(2) \implies \gamma = \frac{\ln(2)}{30} \approx 0.023\,\text{s}^{-1}\n\n\tau = \frac{1}{\gamma} = \frac{30}{\ln(2)} \approx 43.28\,\text{s}\n\n - **(b) Quality Factor:** Natural frequency \omega_0 = \frac{2\pi}{T} = \frac{2\pi}{0.2} = 31.4\,\text{s}^{-1}.\n\nQ = \frac{\tilde{\omega}}{2\gamma} = \frac{\sqrt{\omega_0^2 - \gamma^2}}{2\gamma} \approx \frac{31.4}{2 \times 0.023} \approx 683\n\n - **(c) Logarithmic Decrement:**\n\n\lambda = \frac{\gamma \tilde{T}}{2} = \frac{\gamma \pi}{\tilde{\omega}} \approx \frac{0.023 \times \pi}{31.4} \approx 0.0025\n\n- **Problem 3:** A critically damped mechanical system is displaced by distance x_0x(t) = x_0(1 + \omega_0 t)e^{-\omega_0 t}.\n - **Solution:**\n - For critical damping (\gamma = \omega_0x(t) = e^{-\gamma t}(A t + B).\n - Applying x(0) = x_0 \implies B = x_0\n - Applying v(0) = 0 = \left[-\gamma e^{-\gamma t}(A t + B) + e^{-\gamma t} A\right]{t=0} = -\gamma B + A \implies A = \gamma B = \gamma x_0 = \omega_0 x_0\n - Substituting constants yields:\n\nx(t) = x_0(1 + \omega_0 t)e^{-\omega_0 t}\n\n- **Problem 4:** A weakly damped oscillator has mass m\alpha\lambda. Calculate the stiffness force and resistive force.\n - **Solution:**\n - Given damped frequency \tilde{\omega} = \alpha\lambda = \frac{\gamma \pi}{\alpha} \implies \gamma = \frac{\lambda \alpha}{\pi}.\n - Natural frequency relation: \omega_0^2 = \tilde{\omega}^2 + \gamma^2 = \alpha^2 + \frac{\lambda^2 \alpha^2}{\pi^2} = \alpha^2\left(1 + \frac{\lambda^2}{\pi^2}\right).\n - Stiffness force parameter:\n\nk x = m \omega_0^2 x = m \alpha^2 \left(1 + \frac{\lambda^2}{\pi^2}\right) x\n\n - Resistive damping force parameter:\n\n2 m \gamma v = \frac{2 m \lambda \alpha v}{\pi}\n\n- **Problem 5:** The ratio between frequency \tilde{\omega}\omega_0r : 1\frac{\tilde{\omega}}{\omega_0} = r).\n - **(i) Logarithmic decrement \lambdaQ:**\n - Damping factor \gamma = \sqrt{\omega_0^2 - \tilde{\omega}^2} = \omega_0 \sqrt{1 - r}\n - Logarithmic decrement:\n\n\lambda = \frac{\gamma \pi}{\tilde{\omega}} = \frac{\pi \sqrt{1 - r}}{r}\n\n - Quality factor:\n\nQ = \frac{\tilde{\omega}}{2\gamma} = \frac{r}{2\sqrt{1 - r}}\n\n - **(ii) System energy and time taken to reduce to \frac{1}{e}x{\text{max}}:**\n - Energy expression:\n\nE(t) = \frac{1}{2} m \omega_0^2 x_{\text{max}}^2 e^{-2\gamma t} = \frac{1}{2} m \omega_0^2 x_{\text{max}}^2 e^{-2\omega_0 \sqrt{1 - r} t}\n\n - Time t_1\frac{1}{e} initial energy:\n\n\frac{E(t_1)}{E(0)} = \frac{1}{e} = e^{-2\gamma t_1} \implies t_1 = \frac{1}{2\gamma} = \frac{1}{2\omega_0 \sqrt{1 - r}}\n\n - **(iii) Energy loss during the first cycle:**\n - Time for one cycle t = \frac{2\pi}{\tilde{\omega}}. Energy remaining after first cycle:\n\nE\left(\frac{2\pi}{\tilde{\omega}}\right) = E(0) e^{-\frac{4\pi \gamma}{\tilde{\omega}}}\n\n - Energy lost during first cycle:\n\n\Delta E = E(0) - E\left(\frac{2\pi}{\tilde{\omega}}\right) = E(0)\left(1 - e^{-\frac{4\pi}{r}\sqrt{1-r}}\right)\omega_0\gammam\ddot{x} = -k xmx(t)t\dot{x} = \frac{dx}{dt}\ddot{x} = \frac{d^2 x}{dt^2}k > 0\ddot{x} = -\omega_0^2 x\omega0 > 0\omega0 = \sqrt{\frac{k}{m}}x1(t)x2(t)x(t) = c1 x1(t) + c2 x2(t)c1c2xx(t) = 0x(t) = e^{\lambda t}\dot{x}(t) = \lambda e^{\lambda t}\ddot{x}(t) = \lambda^2 e^{\lambda t}(\lambda^2 + \omega_0^2) e^{\lambda t} = 0e^{\lambda t}\lambda^2 + \omega0^2 = 0\lambda = \pm i\omega0x(t) = c1 e^{i\omega0 t} + c2 e^{-i\omega0 t}x(t)x(t)x^*(t)c1c2c1 = c2^*c1 = A e^{-i\theta}A\thetax(t) = 2A \cos(\omega0 t - \theta)v(0) = v0x(0) = 0x(t) = \left(\frac{v0}{\omega0}\right) \sin(\omega0 t)x(0) = x0v(0) = 0x(t) = x0 \cos(\omega_0 t)E\frac{d}{dt}\left(\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega0^2 x^2\right) = 0\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega0^2 x^2 = \text{constant}\left(\frac{\dot{x}}{\omega0 x0}\right)^2 + \left(\frac{x}{x_0}\right)^2 = 1x(t)\dot{x}(t)g(t)T\langle g(t) \rangle = \frac{1}{T} \int_0^T g(t)\,dt\langle \cos(\omega0 t \pm \phi) \rangle = \langle \sin(\omega0 t \pm \phi) \rangle = 0\langle \cos^2(\omega0 t \pm \phi) \rangle = \langle \sin^2(\omega0 t \pm \phi) \rangle = \frac{1}{2}F_{\text{damping}} = \Gamma \dot{x}P = \Gamma \dot{x}^2\frac{d}{dt}\left(\frac{1}{2}m\dot{x}^2 + \frac{1}{2}m\omega_0^2 x^2\right) = -\Gamma \dot{x}^2\ddot{x} + 2\gamma \dot{x} + \omega_0^2 x = 0\gamma = \frac{\Gamma}{2m}\text{s}^{-1}\gamma > \omega_0\gamma = \omega_0\gamma < \omega_0e^{-\gamma t}$$.