Simple Harmonic Motion. Analytical solution: Equation of motion (EoM) Force on the pendulum constants determined by initial conditions. The period of.

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Presentation transcript:

Simple Harmonic Motion

Analytical solution: Equation of motion (EoM) Force on the pendulum constants determined by initial conditions. The period of the SHO is given by

t i+1 =t i +  t Set  t,  0,  0, l, g, iterate sample code Run t for a few period (T) to see the oscillatory behavior

You may use the Mathematica command Series[Cos[x],{x,0,2}] to obtain the Taylor series expansion of cos  at  = 0. This is amount to making the assumption that   0.

The oscillation amplitude increases with time  Euler method is not suitable for oscillatory motion (but may be good for projectile motion which is non-periodic) The peculiar effect of the numerical solution can also be investigated from the energy of the oscillator when Euler method is applied: E ≈ (1/2)m l 2 [  2 + (g/l)  2 ] (with   0  ) Descretise the equation by applying Euler method, E i+1 = E i + (1/2)mgl 2 [  i 2 + (g/l)  i 2 ](  t) 2  E increases with i  this is an undesirable result.

In the Euler method:  i+1 is calculated based on previous values  i and  i So is  i+1 is calculated based on previous values  i and  i In the Euler-Cromer method:  i+1 is calculated based on previous values  i and  i but  i+1 is calculated based on present values  i+1 and previous value  i sample code 3.2.2

Because it conserver energy over each complete period of motion.

For a pendulum, instantaneous velocity v =  l = l (d  /dt) Hence, f d = - kl (d  /dt). The net force on the forced pendulum along the tangential direction Drag force on a moving object, f d = - kv fdfd l  - kl (d  /dt). r E.o.M

Underdamped regime (small damping). Still oscillate, but amplitude decay slowly over many period before dying totally. Overdamped regime (very large damping), decay slowly over several period before dying totally.  is dominated by exponential term. Critically damped regime, intermediate between under- and overdamping case.

sample code 3.2.3

This is generated with NDSolve sample code 3.2.4

- kl (d  /dt) + F D sin(  D t)  D frequency of the applied force

Resonance happens when

sample code 3.2.5

Consider a generic second order differential equation. It can be numerically solved using second order Runge-Kutta method. First, split the second order DE into two first order parts:

Set initial conditions: Calculate

We have seen previously that energy as calculated using Euler method is unstable. Now try to calculate E again, using the values of  i and  i as calculated using RK2. You will have to do this in the HA3. E i+1