Airfoil: SD7003
Builder: M. Allen
Comment: clean

Number of Reynolds #'s:
 4 

Average Reynolds #:
 61200 
Number of angles of attack:
 33 
 alpha /   Cl   /  Cm
 -6.28  -0.422  -0.0350
 -4.82  -0.312  -0.0350
 -2.95  -0.167  -0.0350
 -1.60  -0.063  -0.0350
 -0.07   0.083  -0.0350
  1.62   0.326  -0.0350
  3.04   0.486  -0.0350
  4.64   0.623  -0.0350
  6.10   0.749  -0.0350
  7.70   0.883  -0.0350
  9.14   0.985  -0.0350
 10.77   1.029  -0.0350
 12.19   0.966  -0.0350
 13.51   0.906  -0.0350
 15.34   0.867  -0.0350
 16.77   0.882  -0.0350
 18.31   0.878  -0.0350
 16.55   0.888  -0.0350
 14.93   0.904  -0.0350
 13.59   0.916  -0.0350
 12.20   0.955  -0.0350
 10.71   1.032  -0.0350
  9.03   0.959  -0.0350
  7.68   0.865  -0.0350
  6.01   0.732  -0.0350
  4.52   0.603  -0.0350
  3.08   0.477  -0.0350
  1.48   0.293  -0.0350
 -0.01   0.080  -0.0350
 -1.61  -0.073  -0.0350
 -3.26  -0.209  -0.0350
 -4.63  -0.320  -0.0350
 -6.34  -0.463  -0.0350
Tabulated from data in file JG00168.DAT & reduced using program Q01.00L

Average Reynolds #:
 102200 
Number of angles of attack:
 33 
 alpha /   Cl   /  Cm
 -6.32  -0.465  -0.0350
 -4.77  -0.329  -0.0350
 -3.19  -0.179  -0.0350
 -1.51  -0.045  -0.0350
  0.04   0.113  -0.0350
  1.35   0.328  -0.0350
  3.15   0.491  -0.0350
  4.44   0.615  -0.0350
  6.22   0.787  -0.0350
  7.56   0.903  -0.0350
  9.29   1.025  -0.0350
 10.59   1.086  -0.0350
 12.19   0.968  -0.0350
 13.57   0.931  -0.0350
 15.17   0.919  -0.0350
 16.63   0.950  -0.0350
 18.29   0.936  -0.0350
 16.49   0.927  -0.0350
 14.90   0.954  -0.0350
 13.56   0.943  -0.0350
 12.04   0.949  -0.0350
 10.69   1.086  -0.0350
  9.10   1.010  -0.0350
  7.71   0.911  -0.0350
  5.93   0.758  -0.0350
  4.50   0.618  -0.0350
  3.07   0.477  -0.0350
  1.52   0.340  -0.0350
 -0.00   0.101  -0.0350
 -1.58  -0.051  -0.0350
 -3.23  -0.186  -0.0350
 -4.74  -0.324  -0.0350
 -6.18  -0.453  -0.0350
Tabulated from data in file JG00170.DAT & reduced using program Q01.00L

Average Reynolds #:
 203400 
Number of angles of attack:
 33 
 alpha /   Cl   /  Cm
 -6.27  -0.453  -0.0350
 -4.67  -0.302  -0.0350
 -2.83  -0.124  -0.0350
 -1.70  -0.023  -0.0350
  0.05   0.169  -0.0350
  1.56   0.322  -0.0350
  3.10   0.478  -0.0350
  4.64   0.635  -0.0350
  5.95   0.760  -0.0350
  7.53   0.905  -0.0350
  9.00   1.019  -0.0350
 10.54   1.110  -0.0350
 11.87   0.985  -0.0350
 14.00   0.981  -0.0350
 15.27   0.959  -0.0350
 16.68   0.943  -0.0350
 18.21   0.922  -0.0350
 16.44   0.956  -0.0350
 14.90   0.943  -0.0350
 13.18   0.965  -0.0350
 12.06   0.980  -0.0350
 10.53   1.109  -0.0350
  9.08   1.023  -0.0350
  7.59   0.910  -0.0350
  6.09   0.775  -0.0350
  4.58   0.628  -0.0350
  2.86   0.452  -0.0350
  1.38   0.299  -0.0350
 -0.15   0.139  -0.0350
 -1.65  -0.028  -0.0350
 -3.23  -0.171  -0.0350
 -4.81  -0.326  -0.0350
 -6.27  -0.462  -0.0350
Tabulated from data in file JG00172.DAT & reduced using program Q01.00L

Average Reynolds #:
 304600 
Number of angles of attack:
 33 
 alpha /   Cl   /  Cm
 -6.34  -0.473  -0.0350
 -4.33  -0.277  -0.0350
 -3.00  -0.145  -0.0350
 -1.71  -0.019  -0.0350
  0.28   0.179  -0.0350
  1.69   0.328  -0.0350
  3.28   0.498  -0.0350
  4.67   0.642  -0.0350
  6.11   0.783  -0.0350
  7.75   0.929  -0.0350
  9.04   1.033  -0.0350
 10.64   1.131  -0.0350
 11.68   1.073  -0.0350
 13.03   0.994  -0.0350
 15.33   0.965  -0.0350
 16.30   0.965  -0.0350
 17.79   0.928  -0.0350
 16.42   0.971  -0.0350
 14.83   0.954  -0.0350
 13.47   0.992  -0.0350
 11.82   1.051  -0.0350
 10.62   1.133  -0.0350
  9.19   1.048  -0.0350
  7.56   0.916  -0.0350
  5.89   0.762  -0.0350
  4.37   0.608  -0.0350
  2.96   0.459  -0.0350
  1.35   0.283  -0.0350
 -0.17   0.129  -0.0350
 -1.86  -0.047  -0.0350
 -3.21  -0.176  -0.0350
 -4.82  -0.340  -0.0350
 -6.45  -0.491  -0.0350
Tabulated from data in file MS00174.DAT & reduced using program Q01.00L

File sd7003.lft created on 12-05-1997 at 15:25:52 using program FORMAT