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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 "blinc.dat" is a simple ascii file where mean and velocity
fluctuations are reported for a station of the incoming boundary.
Data are taken at the station x=43.6 where the main properties are

Mach = 2.28      (Mach number)
delta* = 0.497   (displacement thickness)
theta = 0.140    (momentum thickness)
Re_theta = 2344  (Reynolds number based on theta)
Re_tau = 466     (friction Reynolds number)
H = 3.55         (shape factor)
cf = 2.56E-03    (skin friction coefficient)

The reference length is the boundary layer thickness at the inlet.
The file can be read as

**************************************************************
                        FORTRAN CODE
**************************************************************
       open(unit=12,file='blinc.dat',form='formatted')
       do j=1,jj
        read(12,*) (a(j),l,l=1,12)
       enddo
       close  (12)
**************************************************************

where jj=153 (data are reported up to y/delta99 = 1.2).
The array a contains the following variables

 m  variable
------------
 1  y/delta99
 2  y+ 
 3  u
 4  uvd+ (Van-Driest transformed mean streamwise velocity)
 5  urms (root-mean-square of streamwise velocity fluctuations)
 6  vrms (root-mean-square of wall-normal velocity fluctuations)
 7  wrms (root-mean-square of spanwise velocity fluctuations)
 8  u'v' (shear stress)
 9  urms+
10  vrms+
11  wrms+
12  sqrt(rho/rhow) (square root of the ratio between the mean density and the wall density)

The reference velocity is taken to be the free-stream values.