Discontinuous condition
-two flows with different velocities
1, Basic Equations
2, Add Perturbation
3, Boundary Conditions
4, Solutions
5, Analysis
6, Transmission of Energy



1, Basic Equations
At first, we consider a two-layer system, with perturbation added at the interface between two fluids with different velocities. We'll try to derive the momentum equations of fluid under the assumptions we mentioned before. Under those conditions,the momentum equations become:

                  equation1-momentum equations
For barotropic motions (ρ ≡ ρ(p)) like that we study, the momentum equations lead to:

        equation2
in which q=eq3,and eq.4, which is the vorticity.For a irrotational system, the right hand side of the equations become 0. Then the equations lead to:

            eq5
which are the Bernoulli equations.

2, Add Perturbation

Then we add a perturbation to the system, which can be characterized by two-dimensional velocity potential functions eq6 within each region:

         eq7

After a lot of math(for more details,please see Lew Gramer Sec 4), we get the unsteady Bernoulli Equation:

          eq8

3, Boundary Conditions

There are four boundary conditions:

           equation9

            equation10symbol1=equation11=equation10symbol2  on z=symbol3 and P1=P1  on z=symbol3

Using these boundary conditions, after some math( see Kundu Sec 11.3), we can get
          equation12

which is eq. 11.9 in Kundu and

           equation13

which is eq. 11.13 in Kundu.

4, Solutions

Now assume that the solutions for symbol1,symbol2 have exponential form, namely,

            equation14
  
Plug those forms into the equations we got using the boundary conditions( see Kundu Sec. 11.3), we can get the solutions for c are:

            equation15

5, Analysis

Given the solutions for c, we can analyze the stability of the system.  Obviously, when

            equation16

the system is unstable. This means that when the velocity difference is large enough, density difference is small enough, or wave number k is large enough, the system is unstable.

1), When U1=U2, the solutions get simplified,

             equation17

      which means when equation18, the system is unstable. That's called Rayleigh-Taylor instability.

2), When equation19, the interface becomes a vortex sheet. The solution becomes

            equation20
      Which means that vortex sheet is always unstable to disturbances of  any wavelength.

3), Generally speaking, for a given velocity difference, no matter how small it is, there always exist 
      a wave number k that makes the system unstable.  In another word, for short wave disturbances,
      the system is always unstable.

      We can use the figure below to illustrate the whole progress. (Figure from Kundu)
                                                figure-kundu

6, Transmission of Energy
The source of energy to generate the K-H instability is derived from the kinetic energy of the two steams. This progress can be illustrated by the figure below.(Figure from Gramer)
                         figure2_gramer
From the figure we can get:
The potential energy of the initial state

            symbol4equation21

The potential energy of the final state

             equation22

             equation23
The kinetic energy

             equation24
             equation25
             equation26
Therefore, the kinetic energy of the system decreases while the potential energy increases.