Relativistic Doppler Effect.

This lecture was delivered to the final year honors class of 3 year science degree students on 15 November 2017 as part of the Classical Dynamics paper.

Relativistic Doppler effect. 

There is an apparent shift in the observed frequency of any electromagnetic wave (light) when there is any relative motion between the source of light and the observer. This can be easily determined by using the 4-vector formulation of theory of relativity.

Lets discuss the details of this phenomena under two situations.

A. Source is at rest and observer is in motion. 

Lets us consider two inertial frames S and S’. S’ is moving wrt S, along the x-axis with speed v = \beta c where the observer is at rest in S’ frame but the source is at rest in the  S frame.

Doppler effect 1

Let the source emit a radiation of energy E = h {\nu}_0, which makes an angle \theta wrt x-axis. So the momentum is given by p = \frac{E}{c}=\frac{h\nu_0}{c}. The p_x component of the momentum is therefore p_x=p \cos \theta = \frac{h\nu_0}{c} \cos\theta . Lets consider the x, y, z and t components through the indices 1, 2, 3 and 0. i.e. x ≡ 1, y ≡ 2 ,z ≡ 3 and t ≡ 0.

Then the Lorentz transformation for the 4-momentum p^{\mu} is given by:

\boxed{p^{\mu}{'}=\Lambda^{\mu}_{\nu}\hspace{2pt} p^{\nu}} 

where p^{\mu}{'} is the contravariant 4-vector in S’ frame and p^{\nu} is the same in the S frame. 

\Lambda^{\mu}_{\nu} is the Lorentz transformation matrix element — \mu for row and \nu for column.

p^{\mu}{'} \equiv ({p^0}', {p^1}', {p^2}', {p^3}')=(\frac{h\nu_0}{c},p_x,p_y,p_z) 

\vec{p}=(p_x,p_y,p_z) is the 3-momentum.

\Lambda^{\mu}_{\nu} = \begin{pmatrix}\gamma & - \gamma \beta & 0 & 0\\ - \gamma \beta & \gamma & 0 &0 \\0 & 0 & 1 &0 \\0 & 0 & 0 & 1\end{pmatrix}

so that

\begin{pmatrix} {p^0}' \\ {p^1}' \\ {p^2}' \\ {p^3}'\end{pmatrix} = \begin{pmatrix}\gamma & - \gamma \beta & 0 & 0\\ - \gamma \beta & \gamma & 0 &0 \\0 & 0 & 1 &0 \\0 & 0 & 0 & 1\end{pmatrix}=\begin{pmatrix} p^0 \\ p^1 \\ p^2 \\ p^3 \end{pmatrix}

The “time” or zeroth component is then {p^0}'=\gamma(p^0 - \beta p^1), where p^1=p_x =p \cos \theta=\frac{h \nu_0}{c} \cos \theta .

So that; \frac{h {\nu}\hspace{2pt}'}{c}= \gamma (\frac{h \nu_0 }{c}- \beta \frac{h \nu_0 }{c} \cos \theta) = \gamma \frac{h \nu_0 }{c}(1- \beta \cos \theta) .

So, \boxed{\nu\hspace{2pt}' = \frac{\nu_0 1- \beta \cos \theta)}{\sqrt{1-\beta^2}}}

Thus observed frequency depends on angle \theta  and motion of of observer.

There are 3 situations to discuss.

Case i.

Light is emitted at \theta =0^0.

Motion of observer is to the right — i.e. receding observer. So \cos \theta =1.

\nu \hspace{2pt}' = \frac{\nu_0 (1-\beta)}{\sqrt{1-\beta^2}} =\nu_0 \sqrt{\frac{1-\beta}{1+\beta}}.

So \boxed{\nu \hspace{2pt}' = \nu_0 \sqrt{\frac{1-\beta}{1+\beta}}}..

\nu \hspace{2pt}' < \nu_0

Case ii.

Light emitted at an angle \theta = \pi as S’ moves towards source. \cos \theta =-1.

\nu \hspace{2pt}' = \frac{\nu_0 (1+\beta)}{\sqrt{1-\beta^2}} =\nu_0 \sqrt{\frac{1+\beta}{1-\beta}}.

So \boxed{\nu \hspace{2pt}' =\nu_0 \sqrt{\frac{1+\beta}{1-\beta}}}..

\nu \hspace{2pt}' > \nu_0

Case i and ii are known as longitudinal Doppler effect.

Case iii.

Light is emitted at an angle \theta = 90^0. Observer is moving towards source.

So, \boxed{\nu \hspace{2pt}' = \frac{\nu_0}{\sqrt{1-\beta^2}}}.

Case iii is known as transverse Doppler effect.

B. Observer is at rest and source is moving.

Lets consider an observer to be at rest in the S frame while the source is at rest in the S’ frame and S’ frame is moving wrt S frame with speed given by \beta = \frac{v}{c} , as before.

We need to find the inverse transformation: p = \Lambda ^{-1} p\hspace{2pt}' where

\Lambda^{-1} = \begin{pmatrix}\gamma & \gamma \beta & 0 & 0\\ \gamma \beta & \gamma & 0 &0 \\0 & 0 & 1 &0 \\0 & 0 & 0 & 1\end{pmatrix}

and

\begin{pmatrix} p^0 \\ p^1 \\ p^2 \\ p^3 \end{pmatrix} = \begin{pmatrix}\gamma & \gamma \beta & 0 & 0\\ \gamma \beta & \gamma & 0 &0 \\0 & 0 & 1 &0 \\0 & 0 & 0 & 1\end{pmatrix} = \begin{pmatrix} {p^0}' \\ {p^1}' \\ {p^2}' \\ {p^3}'\end{pmatrix} 

Now time component is:  p^0 = \gamma (p^0\hspace{1pt}'+\beta p^1 \hspace{1pt}')

\frac{h\nu}{c} = \gamma (\frac{h\nu_0}{c} + \beta \frac{h\nu_0}{c} \cos \theta \hspace{1pt}')= \gamma \frac{h\nu_0}{c}(1+\beta \cos \theta \hspace{1pt}')

So, \boxed{\nu = \frac{\nu_0 (1+\beta \cos \theta \hspace{1pt}')}{\sqrt{1-\beta^2}}}  where

  • \nu: observed frequency — in unprimed, i.e. S-frame.
  • \nu_0: emitted frequency — in primed, i.e. S’-frame.
  • \theta \hspace{1pt} ': angle made by emitted light with x’ axis, which is parallel to x-axis.

As before there are 3 situations to discuss specially.

Case i. source is approaching observer, \theta \hspace{1pt} ' = 0

\nu = \frac{\nu_0(1+\beta)}{\sqrt{1-\beta^2}} \hspace{1pt} '

\boxed{\nu = \nu_0 \sqrt{\frac{1+\beta}{1-\beta}}}

\nu \hspace{2pt} > \nu_0

Case ii. source is receding away from observer, \theta \hspace{1pt} ' = \pi

\nu = \frac{\nu_0(1-\beta)}{\sqrt{1-\beta^2}} \hspace{1pt} '

\boxed{\nu = \nu_0\sqrt{\frac{1-\beta}{1+\beta}}}

\nu \hspace{2pt} < \nu_0

Case iii. source is in transverse motion wrt observer, \theta \hspace{1pt} ' = 0

\boxed{\nu= \frac{\nu_0}{\sqrt{1-\beta^2}}}

i and ii are known as longitudinal Doppler effect and iii is known as transverse Doppler effect as before.

We see that for relative approach of source and observer apparent or observed frequency increases. Its known as BLUE SHIFT.

Similarly for recession between source and observer there is apparent decrease in source frequency known as RED SHIFT. 



Categories: basic physics, classical dynamics, Courses I developed, Doppler Shift, Lectures & Presentations, Physics, Relativity, relativity theory, Teaching, Vectors

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