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OAF128 AIRFOIL (oaf128-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: OAF128 AIRFOIL (oaf128-il)
Reynolds number: 200,000
Max Cl/Cd: 55.53 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-oaf128-il-200000-n5.txt
Download as CSV file: xf-oaf128-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: OAF128 AIRFOIL                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -1.0174   0.12102   0.11651   0.0313   1.0000   0.0253
 -15.500  -1.0529   0.10880   0.10405   0.0236   1.0000   0.0253
 -15.250  -1.0790   0.09920   0.09424   0.0175   1.0000   0.0253
 -15.000  -1.1011   0.09103   0.08587   0.0124   1.0000   0.0254
 -14.750  -1.1201   0.08375   0.07840   0.0079   1.0000   0.0255
 -14.500  -1.1353   0.07731   0.07179   0.0039   1.0000   0.0256
 -14.250  -1.1417   0.07262   0.06702   0.0014   1.0000   0.0257
 -14.000  -1.1475   0.06800   0.06232  -0.0012   1.0000   0.0259
 -13.750  -1.1526   0.06349   0.05771  -0.0038   1.0000   0.0261
 -13.500  -1.1567   0.05910   0.05323  -0.0065   1.0000   0.0263
 -13.250  -1.1596   0.05487   0.04889  -0.0092   1.0000   0.0266
 -13.000  -1.1611   0.05087   0.04477  -0.0119   1.0000   0.0268
 -12.750  -1.1613   0.04712   0.04089  -0.0144   1.0000   0.0271
 -12.500  -1.1608   0.04369   0.03732  -0.0166   1.0000   0.0275
 -12.250  -1.1610   0.04070   0.03418  -0.0180   1.0000   0.0278
 -12.000  -1.1546   0.03834   0.03165  -0.0187   1.0000   0.0282
 -11.750  -1.1435   0.03633   0.02948  -0.0190   1.0000   0.0286
 -11.500  -1.1293   0.03453   0.02751  -0.0191   1.0000   0.0291
 -11.250  -1.1133   0.03287   0.02575  -0.0192   1.0000   0.0296
 -11.000  -1.0955   0.03136   0.02421  -0.0193   1.0000   0.0302
 -10.750  -1.0758   0.03000   0.02278  -0.0195   1.0000   0.0308
 -10.500  -1.0546   0.02874   0.02144  -0.0197   1.0000   0.0317
 -10.250  -1.0322   0.02756   0.02016  -0.0198   1.0000   0.0327
 -10.000  -1.0088   0.02644   0.01892  -0.0200   1.0000   0.0338
  -9.750  -0.9853   0.02529   0.01774  -0.0204   1.0000   0.0348
  -9.500  -0.9605   0.02428   0.01668  -0.0207   1.0000   0.0361
  -9.250  -0.9349   0.02333   0.01564  -0.0210   1.0000   0.0375
  -9.000  -0.9089   0.02237   0.01462  -0.0214   1.0000   0.0389
  -8.750  -0.8823   0.02148   0.01370  -0.0218   1.0000   0.0407
  -8.500  -0.8549   0.02071   0.01284  -0.0222   1.0000   0.0432
  -8.250  -0.8275   0.01987   0.01200  -0.0227   1.0000   0.0459
  -8.000  -0.7993   0.01915   0.01123  -0.0231   1.0000   0.0494
  -7.750  -0.7710   0.01840   0.01048  -0.0236   1.0000   0.0538
  -7.500  -0.7423   0.01771   0.00980  -0.0241   1.0000   0.0602
  -7.250  -0.7133   0.01707   0.00920  -0.0246   1.0000   0.0696
  -7.000  -0.6841   0.01648   0.00866  -0.0252   1.0000   0.0813
  -6.750  -0.6547   0.01596   0.00819  -0.0257   1.0000   0.0942
  -6.500  -0.6250   0.01550   0.00776  -0.0262   1.0000   0.1067
  -6.250  -0.5952   0.01506   0.00735  -0.0267   1.0000   0.1186
  -6.000  -0.5653   0.01464   0.00697  -0.0273   1.0000   0.1308
  -5.750  -0.5352   0.01425   0.00663  -0.0278   1.0000   0.1436
  -5.500  -0.5049   0.01389   0.00634  -0.0284   1.0000   0.1578
  -5.250  -0.4745   0.01356   0.00608  -0.0290   1.0000   0.1736
  -4.750  -0.4108   0.01313   0.00571  -0.0306   0.9309   0.2100
  -4.500  -0.3836   0.01300   0.00559  -0.0301   0.8956   0.2252
  -4.250  -0.3573   0.01288   0.00546  -0.0294   0.8659   0.2391
  -4.000  -0.3307   0.01278   0.00532  -0.0288   0.8385   0.2539
  -3.750  -0.3034   0.01268   0.00517  -0.0283   0.8124   0.2690
  -3.500  -0.2757   0.01260   0.00503  -0.0279   0.7869   0.2844
  -3.250  -0.2477   0.01253   0.00489  -0.0276   0.7622   0.3001
  -3.000  -0.2192   0.01247   0.00476  -0.0274   0.7380   0.3155
  -2.750  -0.1902   0.01242   0.00464  -0.0273   0.7151   0.3308
  -2.500  -0.1610   0.01237   0.00454  -0.0273   0.6935   0.3457
  -2.250  -0.1317   0.01234   0.00445  -0.0273   0.6731   0.3600
  -2.000  -0.1022   0.01231   0.00436  -0.0273   0.6537   0.3741
  -1.750  -0.0725   0.01230   0.00429  -0.0274   0.6358   0.3887
  -1.500  -0.0428   0.01229   0.00424  -0.0276   0.6197   0.4051
  -1.250  -0.0130   0.01228   0.00421  -0.0277   0.6036   0.4219
  -1.000   0.0167   0.01227   0.00417  -0.0278   0.5870   0.4360
  -0.750   0.0465   0.01228   0.00412  -0.0279   0.5694   0.4488
  -0.250   0.1062   0.01229   0.00408  -0.0283   0.5368   0.4750
   0.000   0.1361   0.01230   0.00408  -0.0284   0.5242   0.4878
   0.250   0.1660   0.01233   0.00408  -0.0286   0.5118   0.5017
   0.500   0.1959   0.01234   0.00411  -0.0288   0.4991   0.5175
   0.750   0.2258   0.01234   0.00415  -0.0289   0.4877   0.5350
   1.000   0.2555   0.01237   0.00419  -0.0291   0.4768   0.5539
   1.250   0.2853   0.01237   0.00426  -0.0292   0.4649   0.5740
   1.500   0.3150   0.01240   0.00433  -0.0294   0.4538   0.5957
   1.750   0.3443   0.01240   0.00442  -0.0294   0.4427   0.6212
   2.000   0.3735   0.01241   0.00453  -0.0294   0.4321   0.6519
   2.250   0.4020   0.01243   0.00463  -0.0292   0.4211   0.6856
   2.500   0.4303   0.01242   0.00476  -0.0290   0.4095   0.7216
   2.750   0.4579   0.01244   0.00488  -0.0285   0.3988   0.7599
   3.000   0.4844   0.01246   0.00497  -0.0278   0.3850   0.8012
   3.250   0.5097   0.01246   0.00502  -0.0268   0.3677   0.8450
   3.500   0.5335   0.01243   0.00502  -0.0255   0.3505   0.8965
   3.750   0.5612   0.01233   0.00495  -0.0251   0.3348   1.0000
   4.000   0.5915   0.01256   0.00510  -0.0255   0.3194   1.0000
   4.250   0.6216   0.01279   0.00528  -0.0259   0.3042   1.0000
   4.500   0.6516   0.01305   0.00547  -0.0263   0.2889   1.0000
   4.750   0.6815   0.01333   0.00567  -0.0267   0.2733   1.0000
   5.000   0.7111   0.01362   0.00591  -0.0270   0.2574   1.0000
   5.250   0.7406   0.01395   0.00616  -0.0273   0.2416   1.0000
   5.500   0.7699   0.01430   0.00644  -0.0277   0.2264   1.0000
   5.750   0.7990   0.01468   0.00676  -0.0280   0.2113   1.0000
   6.000   0.8279   0.01507   0.00710  -0.0283   0.1958   1.0000
   6.250   0.8567   0.01548   0.00746  -0.0285   0.1788   1.0000
   6.500   0.8851   0.01594   0.00785  -0.0288   0.1607   1.0000
   6.750   0.9132   0.01646   0.00828  -0.0291   0.1439   1.0000
   7.000   0.9411   0.01702   0.00877  -0.0293   0.1301   1.0000
   7.250   0.9687   0.01759   0.00930  -0.0295   0.1195   1.0000
   7.500   0.9960   0.01818   0.00986  -0.0297   0.1115   1.0000
   7.750   1.0229   0.01881   0.01047  -0.0298   0.1046   1.0000
   8.000   1.0498   0.01939   0.01108  -0.0298   0.0993   1.0000
   8.250   1.0760   0.02005   0.01173  -0.0299   0.0945   1.0000
   8.500   1.1019   0.02072   0.01242  -0.0299   0.0905   1.0000
   8.750   1.1278   0.02135   0.01311  -0.0298   0.0866   1.0000
   9.000   1.1525   0.02212   0.01386  -0.0297   0.0833   1.0000
   9.250   1.1771   0.02285   0.01465  -0.0296   0.0804   1.0000
   9.500   1.2016   0.02356   0.01543  -0.0294   0.0775   1.0000
   9.750   1.2250   0.02436   0.01625  -0.0291   0.0749   1.0000
  10.000   1.2470   0.02529   0.01720  -0.0288   0.0727   1.0000
  10.250   1.2699   0.02607   0.01808  -0.0284   0.0703   1.0000
  10.500   1.2916   0.02692   0.01901  -0.0280   0.0681   1.0000
  10.750   1.3119   0.02787   0.02000  -0.0275   0.0662   1.0000
  11.000   1.3304   0.02897   0.02112  -0.0269   0.0645   1.0000
  11.250   1.3495   0.02994   0.02223  -0.0263   0.0627   1.0000
  11.500   1.3670   0.03099   0.02338  -0.0256   0.0609   1.0000
  11.750   1.3826   0.03213   0.02459  -0.0247   0.0594   1.0000
  12.000   1.3950   0.03344   0.02594  -0.0237   0.0581   1.0000
  12.250   1.4052   0.03486   0.02745  -0.0226   0.0569   1.0000
  12.500   1.4115   0.03638   0.02912  -0.0212   0.0557   1.0000
  12.750   1.4167   0.03822   0.03109  -0.0204   0.0545   1.0000
  13.000   1.4217   0.04030   0.03328  -0.0201   0.0534   1.0000
  13.250   1.4261   0.04263   0.03570  -0.0203   0.0524   1.0000
  13.500   1.4294   0.04521   0.03835  -0.0207   0.0516   1.0000
  13.750   1.4314   0.04804   0.04125  -0.0213   0.0508   1.0000
  14.000   1.4330   0.05111   0.04451  -0.0222   0.0498   1.0000
  14.250   1.4332   0.05439   0.04796  -0.0232   0.0488   1.0000
  14.500   1.4322   0.05789   0.05158  -0.0244   0.0480   1.0000
  14.750   1.4300   0.06158   0.05539  -0.0258   0.0472   1.0000
  15.000   1.4269   0.06543   0.05934  -0.0273   0.0465   1.0000
  15.250   1.4230   0.06941   0.06340  -0.0288   0.0459   1.0000
  15.500   1.4185   0.07342   0.06747  -0.0303   0.0453   1.0000
  15.750   1.4110   0.07803   0.07222  -0.0322   0.0447   1.0000
  16.000   1.4004   0.08321   0.07760  -0.0344   0.0441   1.0000
  16.250   1.3894   0.08864   0.08320  -0.0369   0.0434   1.0000
  16.500   1.3781   0.09432   0.08904  -0.0397   0.0428   1.0000
  16.750   1.3667   0.10016   0.09502  -0.0426   0.0422   1.0000
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