# File Name: cp0a.dat
# "Surface pressure distributions, cube normal to flow"                           
#                                        
# "AXIAL TOP SURFACE CENTRELINE (y=0, z/h=1.0)"                                   
#
# x/h=0.000 is centre of the front face.                                  
#
#
# SMALL TUNNEL                                    
#
# x/h|Uh  3.485   6.942   10.3    13.7    17.45
#         Cp      Cp      Cp      Cp      Cp
  0.000    0.716   0.719   0.753   0.737   0.723
  0.069   -1.041  -0.986  -0.977  -0.971  -0.965
  0.213   -1.106  -1.050  -1.049  -1.047  -1.045
  0.356   -1.033  -1.005  -1.003  -1.001  -1.000
  0.500   -0.819  -0.804  -0.807  -0.801  -0.800
  0.644   -0.631  -0.633  -0.618  -0.609  -0.610
  0.788   -0.474  -0.453  -0.444  -0.440  -0.434
  0.931   -0.381  -0.349  -0.337  -0.329  -0.322
#                                                 
# 
# LARGE TUNNEL                                            
# 
# x/h|Uh  4.22    8.45    12.7    16.9    21.1    25.4
#          Cp      Cp      Cp      Cp      Cp      Cp
  0.000    0.816   0.782   0.784   0.777   0.777   0.779
  0.069   -0.954  -0.945  -0.946  -0.956  -0.956  -0.956
  0.213   -1.049  -1.035  -1.052  -1.066  -1.066  -1.067
  0.356   -1.014  -1.028  -1.032  -1.047  -1.047  -1.044
  0.500   -0.834  -0.805  -0.811  -0.823  -0.823  -0.821
  0.644   -0.580  -0.597  -0.580  -0.600  -0.600  -0.602
  0.788   -0.407  -0.411  -0.397  -0.409  -0.409  -0.407
  0.931   -0.302  -0.285  -0.291  -0.273  -0.273  -0.300
#                                                 
# 
# FIELD                                           
# 
# x/h=0.000 is at z/h=0.587 on  the front face.                                           
# Phi range refers to range of allowable upstream flow angle used when averaging Cp 
# 
# x/h|Phi  +/-2 degrees      +/-10 degrees                            
#             Cp               Cp                              
  0.000      0.885            0.821                           
  0.054     -1.150           -1.113                          
  0.147     -1.220           -1.178                          
  0.239     -1.246           -1.197                          
  0.325     -1.239           -1.169                          
  0.410     -1.156           -1.069                          
  0.588     -0.891           -0.798
  0.751     -0.617           -0.552
  0.930     -0.432           -0.393