Airfoil: MH32
Builder: J. Tonnesen
Comment: clean

Number of Reynolds #'s:
 4 

Average Reynolds #:
 59500 
Number of angles of attack:
 11 
 alpha /   Cl   /  Cd   /  Spanwise Cd's >>>
 -4.26  -0.223   0.0309   0.0317   0.0296   0.0312   0.0311
 -2.25  -0.087   0.0200   0.0206   0.0193   0.0202   0.0200
 -0.71   0.050   0.0141   0.0130   0.0088   0.0182   0.0164
  0.75   0.187   0.0173   0.0165   0.0166   0.0183   0.0176
  2.39   0.463   0.0218   0.0212   0.0241   0.0213   0.0207
  3.83   0.650   0.0228   0.0216   0.0287   0.0200   0.0208
  5.45   0.791   0.0221   0.0197   0.0292   0.0184   0.0211
  6.99   0.920   0.0227   0.0214   0.0217   0.0235   0.0240
  8.52   1.025   0.0282   0.0319   0.0281   0.0255   0.0273
 10.03   1.109   0.0361   0.0358   0.0358   0.0361   0.0367
 11.56   1.167   0.0525   0.0484   0.0550   0.0550   0.0515
Tabulated from data in file JG00632.DAT & reduced using program Q02.00D

Average Reynolds #:
 99400 
Number of angles of attack:
 11 
 alpha /   Cl   /  Cd   /  Spanwise Cd's >>>
 -3.82  -0.236   0.0248   0.0247   0.0242   0.0261   0.0243
 -2.26  -0.088   0.0174   0.0174   0.0158   0.0180   0.0185
 -0.72   0.061   0.0142   0.0138   0.0139   0.0137   0.0154
  0.84   0.307   0.0169   0.0153   0.0155   0.0193   0.0176
  2.39   0.506   0.0172   0.0160   0.0167   0.0178   0.0182
  3.93   0.653   0.0161   0.0149   0.0173   0.0153   0.0168
  5.47   0.794   0.0163   0.0159   0.0170   0.0160   0.0163
  6.99   0.921   0.0191   0.0194   0.0188   0.0197   0.0184
  8.52   1.037   0.0257   0.0238   0.0244   0.0279   0.0266
 10.04   1.115   0.0365   0.0355   0.0363   0.0373   0.0367
 11.55   1.172   0.0510   0.0505   0.0484   0.0536   0.0514
Tabulated from data in file CL00634.DAT & reduced using program Q02.00D

Average Reynolds #:
 199100 
Number of angles of attack:
 11 
 alpha /   Cl   /  Cd   /  Spanwise Cd's >>>
 -3.77  -0.197   0.0186   0.0198   0.0196   0.0190   0.0161
 -2.23   0.013   0.0130   0.0116   0.0128   0.0134   0.0141
 -0.69   0.171   0.0109   0.0109   0.0111   0.0109   0.0106
  1.28   0.382   0.0096   0.0093   0.0098   0.0098   0.0097
  2.38   0.492   0.0098   0.0095   0.0101   0.0098   0.0100
  3.94   0.648   0.0104   0.0102   0.0106   0.0105   0.0104
  5.46   0.793   0.0122   0.0120   0.0124   0.0122   0.0124
  7.01   0.927   0.0153   0.0147   0.0152   0.0156   0.0158
  8.53   1.038   0.0207   0.0201   0.0194   0.0226   0.0206
 10.02   1.122   0.0282   0.0275   0.0273   0.0292   0.0287
 11.57   1.183   0.0386   0.0390   0.0376   0.0390   0.0390
Tabulated from data in file CL00636.DAT & reduced using program Q02.00D

Average Reynolds #:
 298800 
Number of angles of attack:
 11 
 alpha /   Cl   /  Cd   /  Spanwise Cd's >>>
 -3.77  -0.134   0.0154   0.0145   0.0144   0.0177   0.0148
 -2.22   0.031   0.0114   0.0101   0.0125   0.0132   0.0098
 -0.69   0.170   0.0082   0.0082   0.0080   0.0090   0.0075
  0.86   0.334   0.0070   0.0063   0.0075   0.0072   0.0071
  2.93   0.553   0.0078   0.0073   0.0084   0.0077   0.0079
  3.95   0.655   0.0088   0.0085   0.0090   0.0087   0.0090
  5.47   0.802   0.0112   0.0110   0.0110   0.0112   0.0115
  7.01   0.937   0.0140   0.0134   0.0141   0.0145   0.0140
  8.54   1.052   0.0190   0.0187   0.0184   0.0191   0.0198
 10.00   1.136   0.0249   0.0241   0.0243   0.0258   0.0254
 11.58   1.200   0.0340   0.0338   0.0334   0.0348   0.0342
Tabulated from data in file CL00638.DAT & reduced using program Q02.00D

File mh32.drg created on 09-12-1997 at 13:46:24 using program FORMAT