Airfoil: MH45
Builder: C. Fox
Comment: clean

Number of Reynolds #'s:
 4 

Average Reynolds #:
 61400 
Number of angles of attack:
 33 
 alpha /   Cl   /  Cm
 -6.14  -0.419  -0.0060
 -4.73  -0.295  -0.0060
 -3.19  -0.165  -0.0060
 -1.62   0.040  -0.0060
 -0.06   0.254  -0.0060
  1.46   0.396  -0.0060
  2.98   0.521  -0.0060
  4.52   0.653  -0.0060
  6.03   0.778  -0.0060
  7.59   0.902  -0.0060
  9.10   1.004  -0.0060
 10.65   1.088  -0.0060
 12.12   1.119  -0.0060
 13.54   0.774  -0.0060
 15.07   0.783  -0.0060
 16.58   0.857  -0.0060
 18.11   0.893  -0.0060
 16.85   0.887  -0.0060
 15.25   0.828  -0.0060
 13.81   0.786  -0.0060
 12.23   0.740  -0.0060
 10.79   0.850  -0.0060
  9.32   0.993  -0.0060
  7.82   0.904  -0.0060
  6.23   0.779  -0.0060
  4.79   0.659  -0.0060
  3.18   0.524  -0.0060
  1.65   0.396  -0.0060
  0.12   0.259  -0.0060
 -1.40   0.060  -0.0060
 -2.99  -0.150  -0.0060
 -4.49  -0.275  -0.0060
 -6.09  -0.402  -0.0060
Tabulated from data in file MS00111.DAT & reduced using program Q01.00L

Average Reynolds #:
 102100 
Number of angles of attack:
 33 
 alpha /   Cl   /  Cm
 -6.20  -0.463  -0.0060
 -4.58  -0.326  -0.0060
 -2.99  -0.154  -0.0060
 -1.41   0.074  -0.0060
  0.18   0.213  -0.0060
  1.49   0.328  -0.0060
  3.18   0.483  -0.0060
  4.68   0.629  -0.0060
  6.18   0.772  -0.0060
  7.68   0.905  -0.0060
  9.25   1.013  -0.0060
 10.69   1.090  -0.0060
 12.37   1.104  -0.0060
 13.90   1.069  -0.0060
 15.24   0.806  -0.0060
 16.87   0.831  -0.0060
 18.23   0.878  -0.0060
 16.62   0.822  -0.0060
 15.09   0.782  -0.0060
 13.70   0.800  -0.0060
 12.19   0.842  -0.0060
 10.68   1.091  -0.0060
  9.22   1.010  -0.0060
  7.64   0.894  -0.0060
  6.09   0.761  -0.0060
  4.57   0.615  -0.0060
  3.08   0.472  -0.0060
  1.64   0.340  -0.0060
  0.05   0.202  -0.0060
 -1.57   0.057  -0.0060
 -3.08  -0.164  -0.0060
 -4.60  -0.323  -0.0060
 -6.09  -0.444  -0.0060
Tabulated from data in file JG00113.DAT & reduced using program Q01.00L

Average Reynolds #:
 203700 
Number of angles of attack:
 33 
 alpha /   Cl   /  Cm
 -6.13  -0.450  -0.0060
 -4.65  -0.304  -0.0060
 -3.08  -0.162  -0.0060
 -1.63  -0.028  -0.0060
 -0.02   0.166  -0.0060
  1.50   0.319  -0.0060
  3.26   0.506  -0.0060
  4.66   0.652  -0.0060
  6.12   0.800  -0.0060
  7.74   0.946  -0.0060
  9.27   1.065  -0.0060
 10.67   1.146  -0.0060
 12.26   1.132  -0.0060
 13.68   1.097  -0.0060
 15.30   1.049  -0.0060
 16.74   0.953  -0.0060
 18.23   0.871  -0.0060
 16.63   0.951  -0.0060
 15.14   0.930  -0.0060
 13.26   0.908  -0.0060
 12.13   1.133  -0.0060
 10.74   1.142  -0.0060
  9.31   1.063  -0.0060
  7.65   0.931  -0.0060
  6.14   0.793  -0.0060
  4.55   0.633  -0.0060
  3.04   0.474  -0.0060
  1.52   0.314  -0.0060
  0.01   0.162  -0.0060
 -1.50  -0.021  -0.0060
 -3.11  -0.168  -0.0060
 -4.62  -0.305  -0.0060
 -6.11  -0.452  -0.0060
Tabulated from data in file JG00115.DAT & reduced using program Q01.00L

Average Reynolds #:
 304900 
Number of angles of attack:
 33 
 alpha /   Cl   /  Cm
 -6.81  -0.536  -0.0060
 -3.94  -0.267  -0.0060
 -2.97  -0.173  -0.0060
 -1.45  -0.023  -0.0060
  0.16   0.168  -0.0060
  1.46   0.311  -0.0060
  3.04   0.489  -0.0060
  4.50   0.644  -0.0060
  6.26   0.825  -0.0060
  7.68   0.959  -0.0060
  9.35   1.099  -0.0060
 10.77   1.177  -0.0060
 12.31   1.145  -0.0060
 13.68   1.115  -0.0060
 15.34   1.074  -0.0060
 16.38   1.079  -0.0060
 18.09   0.957  -0.0060
 16.73   1.053  -0.0060
 15.28   1.069  -0.0060
 13.76   1.112  -0.0060
 12.22   1.161  -0.0060
 10.75   1.175  -0.0060
  9.26   1.089  -0.0060
  7.66   0.955  -0.0060
  6.13   0.808  -0.0060
  4.61   0.651  -0.0060
  3.11   0.489  -0.0060
  1.48   0.308  -0.0060
  0.01   0.147  -0.0060
 -1.55  -0.036  -0.0060
 -3.15  -0.196  -0.0060
 -4.77  -0.350  -0.0060
 -6.25  -0.486  -0.0060
Tabulated from data in file JG00117.DAT & reduced using program Q01.00L

File mh45.lft created on 12-05-1997 at 15:25:50 using program FORMAT