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            DATA FROM DNS OF IMPINGING SHOCK WAVE BOUNDARY
                      LAYER INTERACTION (M = 2.28)
                         06 / 12 / 2010
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The parameters of the simulation are

Free-stream Mach number ====> M = 2.28
Reynolds number based on the inlet BL thickness ====> Re = 16750.
Incidence angle of the shock generator ====> phi = 8 degree
gamma = 1.4

The file "stat.dat" is a simple ascii file where wall properties
(and boundary layer thicknesses) are reported as a function of
the streamwise coordinate. It can be read as

**************************************************************
                        FORTRAN CODE
**************************************************************
       open(unit=12,file='stat.dat',form='formatted')
       do i=1,nx
        read(12,*) (a(i,l),l=1,13)
       enddo
       close  (12)
**************************************************************

where array a contains the following variables

 m  variable
------------
 1  x
 2  cf (skin friction)
 3  pw (mean wall pressure)
 4  pwrms (root-mean-square of wall pressure fluctuations)
 5  utau (friction velocity)
 6  deltav (viscous length-scale)
 7  delta99 (boundary layer thickness)
 8  delta*  (displacement thickness)
 9  theta   (momentum thickness)
10  delta*inc (incompressible displacement thickness)
11  thatainc (incompressible momentum thickness)
12  H (shape factor)
13  Hinc (incompressible shape factor)

The reference length is the boundary layer thickness at the inlet.
The reference pressure and velocity are taken to be the free-stream values.