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OAF095 AIRFOIL (oaf095-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: OAF095 AIRFOIL (oaf095-il)
Reynolds number: 500,000
Max Cl/Cd: 93.21 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-oaf095-il-500000-n5.txt
Download as CSV file: xf-oaf095-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.6892   0.11434   0.11184  -0.0100   1.0000   0.0130
 -13.500  -0.7796   0.09096   0.08821  -0.0232   1.0000   0.0127
 -13.250  -0.8083   0.08126   0.07842  -0.0295   1.0000   0.0127
 -13.000  -0.8351   0.07237   0.06943  -0.0358   1.0000   0.0126
 -12.750  -0.8616   0.06384   0.06081  -0.0424   1.0000   0.0126
 -12.500  -0.8893   0.05517   0.05203  -0.0498   1.0000   0.0125
 -12.250  -0.9023   0.04421   0.04088  -0.0648   1.0000   0.0125
 -12.000  -0.8878   0.03323   0.02958  -0.0836   1.0000   0.0127
 -11.750  -0.8582   0.02785   0.02387  -0.0940   1.0000   0.0131
 -11.500  -0.8308   0.02560   0.02139  -0.0978   1.0000   0.0136
 -11.250  -0.8030   0.02352   0.01914  -0.1012   1.0000   0.0141
 -11.000  -0.7750   0.02207   0.01758  -0.1035   1.0000   0.0147
 -10.750  -0.7467   0.02091   0.01630  -0.1052   1.0000   0.0152
 -10.500  -0.7184   0.01987   0.01514  -0.1067   1.0000   0.0159
 -10.250  -0.6863   0.01888   0.01401  -0.1088   0.9935   0.0166
 -10.000  -0.6536   0.01802   0.01299  -0.1107   0.9869   0.0172
  -9.750  -0.6207   0.01700   0.01189  -0.1129   0.9813   0.0181
  -9.500  -0.5891   0.01634   0.01115  -0.1144   0.9749   0.0192
  -9.250  -0.5578   0.01574   0.01045  -0.1156   0.9689   0.0203
  -9.000  -0.5281   0.01521   0.00980  -0.1164   0.9619   0.0212
  -8.750  -0.4986   0.01454   0.00905  -0.1173   0.9555   0.0224
  -8.500  -0.4700   0.01404   0.00849  -0.1178   0.9485   0.0236
  -8.250  -0.4418   0.01364   0.00800  -0.1180   0.9421   0.0251
  -8.000  -0.4132   0.01327   0.00753  -0.1183   0.9356   0.0263
  -7.750  -0.3846   0.01276   0.00696  -0.1187   0.9292   0.0281
  -7.500  -0.3560   0.01238   0.00653  -0.1190   0.9231   0.0299
  -7.250  -0.3273   0.01207   0.00613  -0.1193   0.9166   0.0318
  -6.750  -0.2693   0.01137   0.00533  -0.1199   0.9043   0.0369
  -6.500  -0.2405   0.01112   0.00499  -0.1200   0.8979   0.0394
  -6.250  -0.2112   0.01079   0.00464  -0.1204   0.8919   0.0435
  -6.000  -0.1819   0.01055   0.00435  -0.1207   0.8851   0.0475
  -5.750  -0.1529   0.01028   0.00405  -0.1209   0.8789   0.0529
  -5.500  -0.1232   0.01005   0.00379  -0.1213   0.8720   0.0592
  -5.250  -0.0940   0.00983   0.00355  -0.1215   0.8652   0.0675
  -5.000  -0.0644   0.00961   0.00334  -0.1218   0.8583   0.0764
  -4.750  -0.0350   0.00942   0.00313  -0.1221   0.8509   0.0859
  -4.500  -0.0057   0.00927   0.00295  -0.1223   0.8433   0.0952
  -4.250   0.0237   0.00911   0.00278  -0.1225   0.8348   0.1064
  -4.000   0.0532   0.00895   0.00263  -0.1228   0.8268   0.1181
  -3.750   0.0827   0.00882   0.00250  -0.1230   0.8191   0.1307
  -3.500   0.1123   0.00870   0.00239  -0.1233   0.8117   0.1441
  -3.250   0.1417   0.00861   0.00228  -0.1235   0.8039   0.1567
  -3.000   0.1712   0.00852   0.00219  -0.1237   0.7963   0.1688
  -2.750   0.2007   0.00844   0.00210  -0.1239   0.7886   0.1810
  -2.500   0.2302   0.00836   0.00203  -0.1241   0.7814   0.1939
  -2.250   0.2597   0.00829   0.00197  -0.1244   0.7737   0.2066
  -2.000   0.2892   0.00824   0.00192  -0.1246   0.7665   0.2182
  -1.750   0.3187   0.00819   0.00188  -0.1248   0.7584   0.2320
  -1.500   0.3482   0.00815   0.00185  -0.1250   0.7506   0.2458
  -1.250   0.3775   0.00813   0.00183  -0.1251   0.7422   0.2592
  -1.000   0.4070   0.00810   0.00183  -0.1253   0.7347   0.2750
  -0.750   0.4364   0.00808   0.00183  -0.1255   0.7269   0.2902
  -0.500   0.4658   0.00807   0.00185  -0.1257   0.7191   0.3061
  -0.250   0.4950   0.00807   0.00187  -0.1258   0.7101   0.3226
   0.000   0.5243   0.00808   0.00189  -0.1260   0.6994   0.3383
   0.250   0.5534   0.00810   0.00193  -0.1261   0.6889   0.3523
   0.500   0.5825   0.00813   0.00197  -0.1262   0.6791   0.3657
   0.750   0.6117   0.00815   0.00202  -0.1263   0.6692   0.3801
   1.000   0.6407   0.00820   0.00208  -0.1264   0.6572   0.3934
   1.250   0.6695   0.00827   0.00213  -0.1265   0.6405   0.4063
   1.500   0.6982   0.00836   0.00220  -0.1265   0.6218   0.4197
   1.750   0.7269   0.00845   0.00228  -0.1266   0.6042   0.4342
   2.250   0.7839   0.00868   0.00248  -0.1266   0.5616   0.4695
   2.500   0.8121   0.00885   0.00261  -0.1267   0.5328   0.4922
   2.750   0.8401   0.00905   0.00277  -0.1267   0.5007   0.5181
   3.000   0.8678   0.00931   0.00296  -0.1267   0.4639   0.5457
   3.250   0.8952   0.00962   0.00318  -0.1267   0.4191   0.5782
   3.500   0.9213   0.01015   0.00351  -0.1266   0.3508   0.6228
   3.750   0.9469   0.01069   0.00393  -0.1265   0.2821   0.6992
   4.000   0.9638   0.01071   0.00420  -0.1241   0.2321   1.0000
   4.250   0.9895   0.01133   0.00458  -0.1239   0.1852   1.0000
   4.500   1.0153   0.01191   0.00496  -0.1237   0.1468   1.0000
   4.750   1.0410   0.01245   0.00533  -0.1234   0.1167   1.0000
   5.000   1.0669   0.01294   0.00569  -0.1232   0.0940   1.0000
   5.250   1.0927   0.01341   0.00607  -0.1229   0.0771   1.0000
   5.500   1.1184   0.01387   0.00645  -0.1225   0.0645   1.0000
   5.750   1.1442   0.01429   0.00683  -0.1222   0.0556   1.0000
   6.000   1.1698   0.01470   0.00723  -0.1218   0.0488   1.0000
   6.250   1.1949   0.01517   0.00765  -0.1214   0.0428   1.0000
   6.500   1.2202   0.01558   0.00807  -0.1210   0.0387   1.0000
   6.750   1.2448   0.01608   0.00854  -0.1205   0.0350   1.0000
   7.000   1.2697   0.01650   0.00900  -0.1200   0.0325   1.0000
   7.250   1.2937   0.01700   0.00950  -0.1194   0.0298   1.0000
   7.500   1.3174   0.01752   0.01004  -0.1187   0.0276   1.0000
   7.750   1.3412   0.01800   0.01056  -0.1181   0.0259   1.0000
   8.000   1.3642   0.01855   0.01113  -0.1173   0.0244   1.0000
   8.250   1.3859   0.01923   0.01181  -0.1164   0.0228   1.0000
   8.500   1.4084   0.01976   0.01241  -0.1155   0.0218   1.0000
   8.750   1.4303   0.02033   0.01303  -0.1146   0.0207   1.0000
   9.000   1.4514   0.02095   0.01369  -0.1136   0.0196   1.0000
   9.250   1.4711   0.02167   0.01443  -0.1124   0.0187   1.0000
   9.500   1.4895   0.02249   0.01530  -0.1111   0.0180   1.0000
   9.750   1.5084   0.02319   0.01608  -0.1097   0.0174   1.0000
  10.000   1.5262   0.02395   0.01691  -0.1083   0.0168   1.0000
  10.250   1.5429   0.02472   0.01776  -0.1067   0.0162   1.0000
  10.500   1.5584   0.02551   0.01861  -0.1049   0.0156   1.0000
  10.750   1.5717   0.02637   0.01952  -0.1028   0.0151   1.0000
  11.000   1.5799   0.02743   0.02064  -0.1001   0.0146   1.0000
  11.250   1.5881   0.02860   0.02189  -0.0975   0.0142   1.0000
  11.500   1.5980   0.02972   0.02311  -0.0953   0.0139   1.0000
  11.750   1.6071   0.03095   0.02445  -0.0932   0.0136   1.0000
  12.000   1.6156   0.03228   0.02589  -0.0912   0.0133   1.0000
  12.250   1.6235   0.03372   0.02743  -0.0893   0.0130   1.0000
  12.500   1.6308   0.03526   0.02907  -0.0875   0.0127   1.0000
  12.750   1.6374   0.03691   0.03081  -0.0858   0.0124   1.0000
  13.000   1.6435   0.03866   0.03266  -0.0843   0.0121   1.0000
  13.250   1.6486   0.04056   0.03466  -0.0828   0.0119   1.0000
  13.500   1.6521   0.04269   0.03688  -0.0815   0.0116   1.0000
  13.750   1.6529   0.04517   0.03946  -0.0802   0.0114   1.0000
  14.000   1.6500   0.04814   0.04254  -0.0791   0.0112   1.0000
  14.250   1.6515   0.05072   0.04526  -0.0782   0.0110   1.0000
  14.500   1.6522   0.05347   0.04816  -0.0775   0.0109   1.0000
  14.750   1.6508   0.05655   0.05137  -0.0770   0.0107   1.0000
  15.000   1.6481   0.05988   0.05485  -0.0767   0.0105   1.0000
  15.250   1.6439   0.06351   0.05862  -0.0766   0.0104   1.0000
  15.500   1.6382   0.06746   0.06272  -0.0768   0.0102   1.0000
  15.750   1.6318   0.07170   0.06710  -0.0773   0.0101   1.0000
  16.000   1.6241   0.07631   0.07186  -0.0782   0.0100   1.0000
  16.250   1.6154   0.08124   0.07693  -0.0794   0.0099   1.0000
  16.500   1.6052   0.08655   0.08239  -0.0809   0.0098   1.0000
  16.750   1.5937   0.09228   0.08827  -0.0828   0.0097   1.0000
  17.000   1.5810   0.09842   0.09456  -0.0851   0.0096   1.0000
  17.250   1.5670   0.10496   0.10125  -0.0878   0.0096   1.0000
  17.500   1.5516   0.11195   0.10840  -0.0910   0.0095   1.0000
  17.750   1.5352   0.11942   0.11602  -0.0946   0.0095   1.0000
  18.000   1.5180   0.12732   0.12407  -0.0987   0.0094   1.0000
  18.250   1.4996   0.13566   0.13257  -0.1033   0.0094   1.0000
  18.500   1.4804   0.14447   0.14153  -0.1085   0.0094   1.0000
  18.750   1.4607   0.15374   0.15096  -0.1141   0.0093   1.0000
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