Sunday, September 22, 2013

Michelsons Interferometer

Michelson Interferometer:

The Michelson interferometer  was invented in the year 1893 by Albert Michelson, to measure a standard meter in units of the wavelength of the red line of the cadmium spectrum. With an optical interferometer, one can measure distances directly in terms of wavelength of light used, by counting the interference fringes that move when one or the other of two mirrors are moved. In the Michelson interferometer, coherent beams are obtained by splitting a beam of light that originates from a single source with a partially reflecting mirror called a beam splitter. The resulting reflected and transmitted waves are then re-directed by ordinary mirrors to a screen where they superimpose to create fringes. This is known as interference by division of amplitude. This interferometer, used in 1817 in the famous Michelson- Morley experiment, demonstrated the non-existence of an electromagnetic-wave-carrying ether, thus paving the way for the Special theory of Relativity.

A simplified diagram of a Michelson interferometer is shown in the fig: 1.

Light from a monochromatic source S is divided by a beam splitter (BS), which is oriented at an angle 45° to the beam, producing two beams of equal intensity. The transmitted beam (T) travels to mirror M2 and it is reflected back to G1. 50% of the returning beam is then reflected by the beam splitter and strikes the screen, E. The reflected beam (R) travels to mirror M1, where it is reflected. 50% of this beam passes straight through beam splitter and reaches the screen.





 



                                                                                                                              Fig. 2

                                                                                                                                                                                    
                                                                                                                                                                                
                                                                                                                                                                                    

Since the reflecting surface of the beam splitter G1 is the surface on the lower right, the light ray starting from the source S and undergoing reflection at the mirror M1 passes through the beam splitter twice. The optical path length through the glass plate depends on its index of refraction, which causes an optical path difference between the two beams. To compensate for this, a glass plate G2 of the same thickness and index of refraction as that of BS is introduced between M2 and G1. The recombined beams interfere and produce fringes at the screen E. The relative phase of the two beams determines whether the interference will be constructive or destructive. By adjusting the inclination of M1 and M2, one can produce circular fringes, straight-line fringes, or curved fringes. This lab uses circular fringes, shown in Fig. 2.

From the screen, an observer sees M1 directly and the virtual image M2' of the mirror M2, formed by reflection in the beam splitter, as shown in Fig. 3. This means that one of the interfering beams comes from M1 and the other beam appears to come from the virtual image M2'. If the two arms of the interferometer are equal in length, M2' coincides with M1. If they do not coincide, let the distance between them be d, and consider a light ray from a point S. It will be reflected by both M2' and M1, and the observer will see two virtual images, S1 due to reflection at M2', and S2 due to reflection at M1. These virtual images will be separated by a distance 2d. If θ is the angle with which the observer looks into the system, the path difference between the two beams is 2dcosθ. When the light that comes from M2 undergoes reflection at G1, a phase change of π occurs, which corresponds to a path difference of λ/2. 

 Fig. 3     



Therefore, the total path difference between the two beams is,
     

The condition for constructive interference is then,
                                                                                                                                                                                                                                                                                                                                                                        
For a given mirror separation d, a given wavelength λ, and order m, the angle of inclination θ  is a constant, and the fringes are circular. They are called fringes of equal inclination, or Haidinger fringes. If M2' coincides with M1, d = 0, and the path difference between the interfering beams will be λ/2. This corresponds to destructive interference, so the center of the field will be dark.

If one of the mirrors is moved through a distance λ/4, the path difference changes by λ/2 and a maximum is obtained. If the mirror is moved through another λ/4, a minimum is obtained; moving it by another λ/4, again a maximum is obtained and so on. Because d is multiplied by cosθ, as d increases, new rings appear in the center faster than the rings already present at the periphery disappear, and the field becomes more crowded with thinner rings toward the outside. If d decreases, the rings contract, become wider and more sparsely distributed, and disappear at the center.

For destructive interference, the total path difference must be an integer number of wavelengths plus a half wavelength, 
   
If the images S1 and S2 from the two mirrors are exactly the same distance away, d=0 and there is no dependance on θ. This means that only one fringe is visible, the zero order destructive interfrence fringe, where
  
and the observer sees a single, large, central dark spot with no surrounding rings.

Measurement of wavelength:

Using the Michelson interferometer, the wavelength of light from a monochromatic source can be determined. If M1 is moved forward or backward, circular fringes appear or disappear at the centre. The mirror is moved through a known distance d and the number N of fringes appearing or disappearing at the centre is counted. For one fringe to appear or disappear, the mirror must be moved through a distance of λ/2. Knowing this, we can write,
                                                                                                    
so that the wavelength is,    
                                                                                                   




Applications

1. The Michelson - Morley experiment is the best known application of Michelson Interferometer.

2. They are used for the detection of gravitational waves.

3. Michelson Interferometers are widely used in astronomical Interferometry. 


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