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OAF095 AIRFOIL (oaf095-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: OAF095 AIRFOIL (oaf095-il)
Reynolds number: 1,000,000
Max Cl/Cd: 131.18 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-oaf095-il-1000000.txt
Download as CSV file: xf-oaf095-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: OAF095 AIRFOIL                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7967   0.10559   0.10364  -0.0135   1.0000   0.0121
 -14.250  -0.8402   0.09276   0.09066  -0.0211   1.0000   0.0120
 -14.000  -0.8687   0.08331   0.08110  -0.0272   1.0000   0.0120
 -13.750  -0.8965   0.07433   0.07202  -0.0334   1.0000   0.0119
 -13.500  -0.9240   0.06585   0.06343  -0.0397   1.0000   0.0119
 -13.250  -0.9552   0.05690   0.05438  -0.0471   1.0000   0.0118
 -13.000  -0.9781   0.04603   0.04335  -0.0604   1.0000   0.0117
 -12.750  -0.9717   0.03376   0.03080  -0.0808   1.0000   0.0118
 -12.500  -0.9416   0.02689   0.02364  -0.0939   1.0000   0.0121
 -12.250  -0.9142   0.02465   0.02125  -0.0979   1.0000   0.0125
 -12.000  -0.8864   0.02296   0.01943  -0.1006   1.0000   0.0129
 -11.750  -0.8583   0.02160   0.01793  -0.1028   1.0000   0.0133
 -11.500  -0.8299   0.02054   0.01675  -0.1044   1.0000   0.0136
 -11.250  -0.8009   0.01873   0.01476  -0.1070   1.0000   0.0142
 -11.000  -0.7717   0.01754   0.01349  -0.1088   1.0000   0.0148
 -10.750  -0.7425   0.01681   0.01270  -0.1100   1.0000   0.0154
 -10.500  -0.7132   0.01617   0.01199  -0.1110   1.0000   0.0161
 -10.250  -0.6842   0.01563   0.01138  -0.1118   1.0000   0.0168
 -10.000  -0.6530   0.01522   0.01089  -0.1129   0.9971   0.0172
  -9.750  -0.6185   0.01396   0.00954  -0.1155   0.9930   0.0186
  -9.500  -0.5856   0.01346   0.00899  -0.1170   0.9875   0.0195
  -9.250  -0.5531   0.01302   0.00849  -0.1183   0.9821   0.0205
  -9.000  -0.5236   0.01269   0.00808  -0.1188   0.9748   0.0212
  -8.750  -0.4946   0.01197   0.00727  -0.1194   0.9680   0.0226
  -8.500  -0.4672   0.01161   0.00688  -0.1195   0.9604   0.0240
  -8.250  -0.4400   0.01136   0.00657  -0.1194   0.9538   0.0253
  -8.000  -0.4124   0.01114   0.00629  -0.1193   0.9470   0.0263
  -7.750  -0.3842   0.01060   0.00567  -0.1195   0.9411   0.0284
  -7.500  -0.3552   0.01030   0.00534  -0.1198   0.9349   0.0302
  -7.250  -0.3272   0.01010   0.00509  -0.1198   0.9287   0.0319
  -7.000  -0.2979   0.00971   0.00464  -0.1201   0.9230   0.0344
  -6.750  -0.2686   0.00943   0.00433  -0.1204   0.9167   0.0372
  -6.250  -0.2102   0.00891   0.00375  -0.1209   0.9047   0.0442
  -6.000  -0.1812   0.00874   0.00352  -0.1211   0.8984   0.0477
  -5.750  -0.1516   0.00846   0.00325  -0.1214   0.8921   0.0547
  -5.500  -0.1220   0.00824   0.00302  -0.1217   0.8848   0.0624
  -5.250  -0.0928   0.00806   0.00283  -0.1219   0.8780   0.0713
  -5.000  -0.0630   0.00788   0.00266  -0.1222   0.8707   0.0812
  -4.750  -0.0337   0.00771   0.00249  -0.1224   0.8641   0.0930
  -4.500  -0.0038   0.00754   0.00234  -0.1228   0.8572   0.1041
  -4.250   0.0258   0.00741   0.00221  -0.1230   0.8503   0.1158
  -4.000   0.0555   0.00727   0.00210  -0.1233   0.8437   0.1288
  -3.750   0.0851   0.00716   0.00200  -0.1236   0.8365   0.1426
  -3.500   0.1147   0.00707   0.00191  -0.1238   0.8298   0.1555
  -3.250   0.1443   0.00700   0.00183  -0.1240   0.8223   0.1664
  -3.000   0.1738   0.00692   0.00176  -0.1242   0.8154   0.1790
  -2.750   0.2036   0.00683   0.00170  -0.1245   0.8076   0.1916
  -2.500   0.2331   0.00678   0.00164  -0.1247   0.8001   0.2041
  -2.250   0.2628   0.00671   0.00159  -0.1249   0.7919   0.2182
  -2.000   0.2923   0.00667   0.00155  -0.1251   0.7844   0.2325
  -1.750   0.3220   0.00661   0.00152  -0.1254   0.7764   0.2479
  -1.500   0.3515   0.00658   0.00150  -0.1256   0.7689   0.2627
  -1.250   0.3811   0.00654   0.00149  -0.1258   0.7606   0.2790
  -1.000   0.4105   0.00652   0.00148  -0.1260   0.7521   0.2949
  -0.750   0.4399   0.00651   0.00148  -0.1262   0.7420   0.3093
  -0.500   0.4694   0.00650   0.00148  -0.1263   0.7322   0.3249
  -0.250   0.4987   0.00652   0.00150  -0.1265   0.7232   0.3400
   0.000   0.5282   0.00651   0.00152  -0.1267   0.7138   0.3554
   0.250   0.5575   0.00652   0.00155  -0.1268   0.7039   0.3714
   0.500   0.5867   0.00656   0.00158  -0.1270   0.6915   0.3869
   0.750   0.6158   0.00660   0.00161  -0.1271   0.6774   0.4013
   1.000   0.6450   0.00663   0.00165  -0.1272   0.6641   0.4157
   1.250   0.6742   0.00667   0.00170  -0.1273   0.6507   0.4315
   1.500   0.7033   0.00672   0.00175  -0.1275   0.6364   0.4475
   1.750   0.7324   0.00679   0.00182  -0.1276   0.6202   0.4638
   2.000   0.7613   0.00688   0.00189  -0.1277   0.6014   0.4815
   2.250   0.7902   0.00696   0.00198  -0.1278   0.5823   0.5014
   2.500   0.8190   0.00706   0.00207  -0.1279   0.5604   0.5242
   2.750   0.8478   0.00718   0.00219  -0.1281   0.5377   0.5539
   3.000   0.8764   0.00731   0.00233  -0.1282   0.5094   0.5960
   3.250   0.9051   0.00742   0.00252  -0.1285   0.4777   0.6742
   3.500   0.9261   0.00706   0.00267  -0.1268   0.4440   1.0000
   3.750   0.9531   0.00759   0.00290  -0.1268   0.3801   1.0000
   4.000   0.9792   0.00830   0.00324  -0.1267   0.3057   1.0000
   4.250   1.0050   0.00902   0.00361  -0.1266   0.2368   1.0000
   4.500   1.0310   0.00964   0.00396  -0.1264   0.1854   1.0000
   4.750   1.0569   0.01022   0.00431  -0.1262   0.1424   1.0000
   5.000   1.0831   0.01073   0.00465  -0.1260   0.1105   1.0000
   5.250   1.1092   0.01122   0.00499  -0.1258   0.0860   1.0000
   5.500   1.1354   0.01166   0.00532  -0.1255   0.0692   1.0000
   5.750   1.1616   0.01206   0.00566  -0.1253   0.0576   1.0000
   6.000   1.1878   0.01245   0.00600  -0.1250   0.0495   1.0000
   6.250   1.2136   0.01287   0.00638  -0.1246   0.0426   1.0000
   6.500   1.2395   0.01324   0.00673  -0.1243   0.0383   1.0000
   6.750   1.2650   0.01368   0.00716  -0.1239   0.0344   1.0000
   7.000   1.2907   0.01404   0.00752  -0.1235   0.0318   1.0000
   7.250   1.3147   0.01464   0.00810  -0.1228   0.0284   1.0000
   7.500   1.3404   0.01495   0.00844  -0.1224   0.0271   1.0000
   7.750   1.3652   0.01535   0.00885  -0.1220   0.0254   1.0000
   8.000   1.3886   0.01594   0.00943  -0.1212   0.0234   1.0000
   8.250   1.4120   0.01648   0.01002  -0.1205   0.0223   1.0000
   8.500   1.4360   0.01691   0.01048  -0.1199   0.0214   1.0000
   8.750   1.4594   0.01738   0.01099  -0.1191   0.0204   1.0000
   9.000   1.4818   0.01794   0.01155  -0.1183   0.0194   1.0000
   9.250   1.5004   0.01892   0.01258  -0.1169   0.0181   1.0000
   9.500   1.5231   0.01936   0.01306  -0.1161   0.0177   1.0000
   9.750   1.5446   0.01991   0.01366  -0.1151   0.0171   1.0000
  10.000   1.5652   0.02050   0.01430  -0.1140   0.0165   1.0000
  10.250   1.5851   0.02112   0.01496  -0.1128   0.0160   1.0000
  10.500   1.6036   0.02182   0.01569  -0.1114   0.0154   1.0000
  10.750   1.6182   0.02282   0.01674  -0.1095   0.0148   1.0000
  11.000   1.6265   0.02421   0.01823  -0.1066   0.0143   1.0000
  11.250   1.6426   0.02482   0.01890  -0.1048   0.0140   1.0000
  11.500   1.6547   0.02557   0.01973  -0.1025   0.0138   1.0000
  11.750   1.6660   0.02638   0.02061  -0.1001   0.0134   1.0000
  12.000   1.6764   0.02733   0.02163  -0.0978   0.0131   1.0000
  12.250   1.6859   0.02840   0.02277  -0.0956   0.0128   1.0000
  12.500   1.6951   0.02957   0.02401  -0.0935   0.0125   1.0000
  12.750   1.7038   0.03082   0.02532  -0.0915   0.0122   1.0000
  13.000   1.7108   0.03229   0.02685  -0.0895   0.0120   1.0000
  13.250   1.7144   0.03410   0.02875  -0.0874   0.0117   1.0000
  13.500   1.7122   0.03655   0.03132  -0.0851   0.0114   1.0000
  13.750   1.7024   0.03988   0.03480  -0.0826   0.0112   1.0000
  14.000   1.7087   0.04171   0.03673  -0.0814   0.0111   1.0000
  14.250   1.7129   0.04381   0.03893  -0.0803   0.0110   1.0000
  14.500   1.7159   0.04607   0.04130  -0.0792   0.0108   1.0000
  14.750   1.7179   0.04855   0.04388  -0.0783   0.0107   1.0000
  15.000   1.7185   0.05125   0.04670  -0.0776   0.0105   1.0000
  15.250   1.7184   0.05409   0.04965  -0.0770   0.0103   1.0000
  15.500   1.7164   0.05725   0.05292  -0.0766   0.0102   1.0000
  15.750   1.7141   0.06057   0.05636  -0.0765   0.0100   1.0000
  16.000   1.7100   0.06427   0.06016  -0.0766   0.0099   1.0000
  16.250   1.7053   0.06815   0.06416  -0.0769   0.0098   1.0000
  16.500   1.6989   0.07245   0.06857  -0.0776   0.0096   1.0000
  16.750   1.6909   0.07715   0.07338  -0.0785   0.0095   1.0000
  17.000   1.6815   0.08221   0.07856  -0.0798   0.0095   1.0000
  17.250   1.6703   0.08769   0.08416  -0.0814   0.0094   1.0000
  17.500   1.6576   0.09360   0.09019  -0.0834   0.0093   1.0000
  17.750   1.6433   0.09996   0.09669  -0.0858   0.0093   1.0000
  18.000   1.6279   0.10668   0.10353  -0.0886   0.0092   1.0000
  18.250   1.6104   0.11395   0.11094  -0.0918   0.0092   1.0000
  18.500   1.5923   0.12161   0.11873  -0.0955   0.0091   1.0000
  18.750   1.5735   0.12961   0.12687  -0.0996   0.0091   1.0000
  19.000   1.5544   0.13787   0.13526  -0.1041   0.0091   1.0000
  19.250   1.5348   0.14647   0.14400  -0.1091   0.0090   1.0000
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