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OAF128 AIRFOIL (oaf128-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: OAF128 AIRFOIL (oaf128-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.39 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-oaf128-il-1000000.txt
Download as CSV file: xf-oaf128-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.3157   0.08341   0.07994   0.0150   1.0000   0.0173
 -16.250  -1.3327   0.07718   0.07362   0.0118   1.0000   0.0173
 -16.000  -1.3499   0.07099   0.06732   0.0086   1.0000   0.0174
 -15.750  -1.3665   0.06494   0.06117   0.0055   1.0000   0.0174
 -15.500  -1.3818   0.05901   0.05513   0.0022   1.0000   0.0175
 -15.250  -1.3949   0.05332   0.04933  -0.0010   1.0000   0.0175
 -15.000  -1.4049   0.04794   0.04383  -0.0044   1.0000   0.0176
 -14.750  -1.4113   0.04286   0.03863  -0.0079   1.0000   0.0177
 -14.500  -1.4137   0.03821   0.03385  -0.0117   1.0000   0.0178
 -14.250  -1.4163   0.03402   0.02952  -0.0151   1.0000   0.0179
 -14.000  -1.4138   0.03122   0.02659  -0.0168   1.0000   0.0180
 -13.750  -1.4009   0.02958   0.02485  -0.0171   1.0000   0.0182
 -13.500  -1.3842   0.02826   0.02344  -0.0172   1.0000   0.0184
 -13.250  -1.3649   0.02715   0.02225  -0.0172   1.0000   0.0186
 -13.000  -1.3439   0.02620   0.02122  -0.0172   1.0000   0.0188
 -12.750  -1.3279   0.02437   0.01929  -0.0174   1.0000   0.0192
 -12.500  -1.3072   0.02310   0.01796  -0.0175   1.0000   0.0195
 -12.250  -1.2838   0.02216   0.01698  -0.0176   1.0000   0.0198
 -12.000  -1.2593   0.02137   0.01615  -0.0178   1.0000   0.0202
 -11.750  -1.2341   0.02064   0.01537  -0.0179   1.0000   0.0205
 -11.500  -1.2083   0.01995   0.01464  -0.0180   1.0000   0.0209
 -11.250  -1.1820   0.01931   0.01394  -0.0182   1.0000   0.0213
 -11.000  -1.1552   0.01872   0.01330  -0.0184   1.0000   0.0217
 -10.750  -1.1279   0.01822   0.01275  -0.0185   1.0000   0.0220
 -10.500  -1.1018   0.01721   0.01168  -0.0189   1.0000   0.0227
 -10.250  -1.0742   0.01658   0.01104  -0.0192   1.0000   0.0233
 -10.000  -1.0462   0.01608   0.01051  -0.0195   1.0000   0.0239
  -9.750  -1.0178   0.01561   0.01001  -0.0197   1.0000   0.0246
  -9.500  -0.9892   0.01520   0.00956  -0.0200   1.0000   0.0252
  -9.250  -0.9606   0.01466   0.00899  -0.0203   1.0000   0.0261
  -9.000  -0.9318   0.01413   0.00845  -0.0207   1.0000   0.0271
  -8.750  -0.9027   0.01373   0.00804  -0.0210   1.0000   0.0281
  -8.500  -0.8734   0.01338   0.00767  -0.0212   1.0000   0.0291
  -8.250  -0.8440   0.01289   0.00716  -0.0216   1.0000   0.0305
  -8.000  -0.8145   0.01250   0.00677  -0.0220   1.0000   0.0321
  -7.750  -0.7848   0.01219   0.00645  -0.0223   1.0000   0.0337
  -7.500  -0.7549   0.01174   0.00602  -0.0227   1.0000   0.0365
  -7.250  -0.7250   0.01137   0.00567  -0.0231   1.0000   0.0399
  -7.000  -0.6949   0.01098   0.00531  -0.0236   1.0000   0.0455
  -6.750  -0.6646   0.01054   0.00495  -0.0241   1.0000   0.0560
  -6.500  -0.6343   0.01008   0.00462  -0.0247   1.0000   0.0734
  -6.250  -0.6039   0.00975   0.00437  -0.0252   1.0000   0.0881
  -6.000  -0.5747   0.00965   0.00429  -0.0252   0.9468   0.0992
  -5.750  -0.5494   0.00956   0.00417  -0.0243   0.9117   0.1090
  -5.500  -0.5220   0.00944   0.00401  -0.0240   0.8852   0.1180
  -5.250  -0.4936   0.00934   0.00385  -0.0238   0.8588   0.1266
  -5.000  -0.4646   0.00921   0.00368  -0.0238   0.8340   0.1366
  -4.750  -0.4351   0.00905   0.00351  -0.0239   0.8095   0.1506
  -4.500  -0.4054   0.00891   0.00336  -0.0241   0.7847   0.1678
  -4.250  -0.3756   0.00882   0.00323  -0.0243   0.7597   0.1826
  -4.000  -0.3456   0.00874   0.00311  -0.0245   0.7349   0.1952
  -3.750  -0.3155   0.00863   0.00298  -0.0248   0.7117   0.2078
  -3.500  -0.2852   0.00853   0.00286  -0.0251   0.6895   0.2230
  -3.250  -0.2550   0.00842   0.00276  -0.0254   0.6681   0.2441
  -2.750  -0.1944   0.00830   0.00260  -0.0260   0.6233   0.2795
  -2.500  -0.1641   0.00825   0.00253  -0.0263   0.6030   0.2961
  -2.250  -0.1337   0.00821   0.00248  -0.0266   0.5860   0.3120
  -2.000  -0.1034   0.00818   0.00244  -0.0269   0.5685   0.3258
  -1.750  -0.0731   0.00817   0.00239  -0.0271   0.5512   0.3389
  -1.250  -0.0125   0.00813   0.00234  -0.0276   0.5247   0.3637
  -1.000   0.0178   0.00814   0.00232  -0.0279   0.5123   0.3748
  -0.750   0.0481   0.00814   0.00231  -0.0281   0.4999   0.3867
  -0.500   0.0784   0.00813   0.00231  -0.0284   0.4881   0.3990
  -0.250   0.1087   0.00814   0.00231  -0.0286   0.4765   0.4114
   0.250   0.1693   0.00814   0.00233  -0.0291   0.4561   0.4403
   0.500   0.1996   0.00813   0.00234  -0.0294   0.4456   0.4536
   0.750   0.2298   0.00816   0.00236  -0.0296   0.4352   0.4663
   1.000   0.2601   0.00818   0.00239  -0.0298   0.4251   0.4804
   1.250   0.2903   0.00818   0.00242  -0.0301   0.4157   0.4954
   1.500   0.3206   0.00823   0.00246  -0.0304   0.4029   0.5105
   1.750   0.3508   0.00827   0.00249  -0.0306   0.3871   0.5265
   2.000   0.3810   0.00831   0.00254  -0.0309   0.3719   0.5447
   2.250   0.4112   0.00833   0.00260  -0.0311   0.3594   0.5663
   2.500   0.4414   0.00838   0.00266  -0.0314   0.3470   0.5896
   2.750   0.4715   0.00843   0.00274  -0.0317   0.3333   0.6148
   3.000   0.5017   0.00846   0.00282  -0.0320   0.3200   0.6448
   3.250   0.5317   0.00848   0.00292  -0.0322   0.3064   0.6829
   3.500   0.5616   0.00853   0.00304  -0.0325   0.2915   0.7269
   3.750   0.5912   0.00858   0.00317  -0.0326   0.2767   0.7683
   4.000   0.6205   0.00866   0.00330  -0.0327   0.2610   0.8082
   4.250   0.6490   0.00875   0.00344  -0.0326   0.2452   0.8492
   4.500   0.6762   0.00882   0.00357  -0.0322   0.2316   0.8934
   4.750   0.6987   0.00865   0.00351  -0.0306   0.2209   1.0000
   5.000   0.7288   0.00886   0.00366  -0.0309   0.2091   1.0000
   5.250   0.7587   0.00909   0.00383  -0.0312   0.1970   1.0000
   5.500   0.7886   0.00933   0.00400  -0.0315   0.1824   1.0000
   5.750   0.8183   0.00962   0.00419  -0.0318   0.1635   1.0000
   6.000   0.8478   0.01002   0.00444  -0.0322   0.1408   1.0000
   6.250   0.8772   0.01040   0.00472  -0.0325   0.1222   1.0000
   6.500   0.9064   0.01077   0.00500  -0.0328   0.1086   1.0000
   6.750   0.9357   0.01111   0.00528  -0.0331   0.0996   1.0000
   7.000   0.9648   0.01146   0.00558  -0.0333   0.0920   1.0000
   7.250   0.9939   0.01174   0.00584  -0.0335   0.0874   1.0000
   7.500   1.0227   0.01211   0.00616  -0.0337   0.0821   1.0000
   7.750   1.0517   0.01235   0.00642  -0.0339   0.0791   1.0000
   8.000   1.0803   0.01270   0.00674  -0.0340   0.0754   1.0000
   8.250   1.1089   0.01304   0.00708  -0.0342   0.0722   1.0000
   8.500   1.1374   0.01332   0.00737  -0.0343   0.0699   1.0000
   8.750   1.1656   0.01368   0.00771  -0.0344   0.0670   1.0000
   9.000   1.1936   0.01408   0.00811  -0.0345   0.0644   1.0000
   9.250   1.2217   0.01436   0.00842  -0.0346   0.0627   1.0000
   9.500   1.2495   0.01471   0.00876  -0.0346   0.0605   1.0000
   9.750   1.2765   0.01522   0.00926  -0.0346   0.0579   1.0000
  10.000   1.3041   0.01554   0.00962  -0.0346   0.0566   1.0000
  10.250   1.3315   0.01588   0.00997  -0.0346   0.0550   1.0000
  10.500   1.3584   0.01629   0.01038  -0.0346   0.0532   1.0000
  10.750   1.3840   0.01692   0.01101  -0.0345   0.0510   1.0000
  11.000   1.4109   0.01724   0.01137  -0.0344   0.0500   1.0000
  11.250   1.4373   0.01762   0.01178  -0.0343   0.0486   1.0000
  11.500   1.4630   0.01808   0.01225  -0.0342   0.0471   1.0000
  11.750   1.4873   0.01876   0.01293  -0.0340   0.0454   1.0000
  12.000   1.5125   0.01922   0.01344  -0.0337   0.0444   1.0000
  12.250   1.5376   0.01965   0.01391  -0.0335   0.0432   1.0000
  12.500   1.5618   0.02018   0.01446  -0.0332   0.0419   1.0000
  12.750   1.5845   0.02086   0.01515  -0.0328   0.0406   1.0000
  13.000   1.6064   0.02159   0.01593  -0.0323   0.0394   1.0000
  13.250   1.6295   0.02210   0.01649  -0.0319   0.0385   1.0000
  13.500   1.6515   0.02270   0.01713  -0.0314   0.0374   1.0000
  13.750   1.6718   0.02344   0.01789  -0.0308   0.0364   1.0000
  14.000   1.6881   0.02450   0.01897  -0.0298   0.0352   1.0000
  14.250   1.7067   0.02524   0.01978  -0.0290   0.0344   1.0000
  14.500   1.7236   0.02603   0.02064  -0.0280   0.0337   1.0000
  14.750   1.7376   0.02696   0.02164  -0.0268   0.0329   1.0000
  15.000   1.7468   0.02812   0.02285  -0.0252   0.0322   1.0000
  15.250   1.7465   0.02993   0.02473  -0.0234   0.0316   1.0000
  15.500   1.7441   0.03259   0.02748  -0.0230   0.0309   1.0000
  15.750   1.7475   0.03509   0.03008  -0.0233   0.0304   1.0000
  16.000   1.7522   0.03762   0.03271  -0.0239   0.0299   1.0000
  16.250   1.7542   0.04065   0.03584  -0.0249   0.0294   1.0000
  16.500   1.7530   0.04418   0.03948  -0.0261   0.0289   1.0000
  16.750   1.7480   0.04830   0.04369  -0.0277   0.0284   1.0000
  17.000   1.7389   0.05298   0.04848  -0.0294   0.0281   1.0000
  17.250   1.7252   0.05831   0.05391  -0.0314   0.0278   1.0000
  17.500   1.7070   0.06426   0.05998  -0.0337   0.0275   1.0000
  17.750   1.6846   0.07084   0.06669  -0.0362   0.0272   1.0000
  18.000   1.6590   0.07795   0.07392  -0.0390   0.0270   1.0000
  18.250   1.6331   0.08535   0.08144  -0.0421   0.0268   1.0000
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