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GOE 506 AIRFOIL (goe506-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 506 AIRFOIL (goe506-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81.1 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe506-il-1000000.txt
Download as CSV file: xf-goe506-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 506 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.5535   0.08664   0.08444  -0.0959   0.9905   0.0120
 -16.000  -0.5812   0.07682   0.07446  -0.1032   0.9884   0.0122
 -15.750  -0.6083   0.06773   0.06519  -0.1105   0.9863   0.0122
 -15.500  -0.6318   0.05934   0.05661  -0.1177   0.9843   0.0121
 -15.250  -0.6521   0.05214   0.04924  -0.1235   0.9799   0.0121
 -15.000  -0.6494   0.04784   0.04484  -0.1280   0.9759   0.0122
 -14.750  -0.6482   0.04282   0.03967  -0.1338   0.9728   0.0125
 -14.500  -0.6438   0.03832   0.03502  -0.1393   0.9688   0.0127
 -14.250  -0.6380   0.03418   0.03071  -0.1445   0.9631   0.0128
 -14.000  -0.6185   0.03146   0.02784  -0.1495   0.9597   0.0131
 -13.750  -0.6005   0.02862   0.02483  -0.1545   0.9556   0.0132
 -13.500  -0.5860   0.02546   0.02146  -0.1593   0.9499   0.0134
 -13.250  -0.5621   0.02347   0.01935  -0.1633   0.9454   0.0138
 -13.000  -0.5358   0.02243   0.01824  -0.1658   0.9406   0.0141
 -12.750  -0.5152   0.02163   0.01737  -0.1666   0.9345   0.0143
 -12.500  -0.4927   0.02076   0.01641  -0.1676   0.9292   0.0146
 -12.250  -0.4783   0.02018   0.01574  -0.1665   0.9234   0.0149
 -12.000  -0.4645   0.01967   0.01514  -0.1650   0.9176   0.0154
 -11.750  -0.4477   0.01905   0.01442  -0.1641   0.9125   0.0157
 -11.500  -0.4410   0.01851   0.01381  -0.1609   0.9070   0.0159
 -11.250  -0.4317   0.01800   0.01321  -0.1580   0.9015   0.0161
 -11.000  -0.4208   0.01735   0.01243  -0.1555   0.8961   0.0166
 -10.750  -0.4183   0.01683   0.01189  -0.1512   0.8909   0.0170
 -10.500  -0.4057   0.01642   0.01143  -0.1487   0.8856   0.0172
 -10.250  -0.3851   0.01620   0.01116  -0.1476   0.8809   0.0177
 -10.000  -0.3697   0.01587   0.01079  -0.1455   0.8766   0.0181
  -9.750  -0.3534   0.01550   0.01037  -0.1435   0.8722   0.0185
  -9.500  -0.3338   0.01522   0.01003  -0.1421   0.8680   0.0192
  -9.250  -0.3136   0.01487   0.00959  -0.1408   0.8633   0.0196
  -9.000  -0.2942   0.01468   0.00936  -0.1392   0.8587   0.0199
  -8.750  -0.2830   0.01385   0.00846  -0.1364   0.8537   0.0206
  -8.500  -0.2613   0.01357   0.00815  -0.1354   0.8492   0.0213
  -8.250  -0.2408   0.01333   0.00790  -0.1341   0.8446   0.0219
  -8.000  -0.2204   0.01305   0.00759  -0.1327   0.8393   0.0226
  -7.750  -0.1983   0.01278   0.00725  -0.1316   0.8342   0.0234
  -7.500  -0.1769   0.01255   0.00698  -0.1303   0.8287   0.0239
  -7.250  -0.1560   0.01226   0.00664  -0.1290   0.8231   0.0244
  -7.000  -0.1399   0.01162   0.00593  -0.1269   0.8180   0.0254
  -6.750  -0.1185   0.01136   0.00566  -0.1257   0.8129   0.0264
  -6.500  -0.0962   0.01113   0.00540  -0.1246   0.8072   0.0272
  -6.000  -0.0511   0.01068   0.00487  -0.1224   0.7959   0.0288
  -5.750  -0.0274   0.01055   0.00469  -0.1216   0.7896   0.0293
  -5.500  -0.0087   0.01006   0.00413  -0.1198   0.7838   0.0308
  -5.250   0.0137   0.00982   0.00386  -0.1187   0.7779   0.0319
  -5.000   0.0370   0.00964   0.00362  -0.1177   0.7726   0.0330
  -4.750   0.0608   0.00947   0.00342  -0.1169   0.7677   0.0340
  -4.500   0.0846   0.00933   0.00324  -0.1160   0.7618   0.0350
  -4.250   0.1071   0.00917   0.00301  -0.1148   0.7544   0.0364
  -4.000   0.1299   0.00899   0.00280  -0.1137   0.7475   0.0386
  -3.750   0.1523   0.00888   0.00264  -0.1125   0.7395   0.0407
  -3.500   0.1755   0.00876   0.00250  -0.1115   0.7319   0.0441
  -3.250   0.1941   0.00840   0.00227  -0.1096   0.7244   0.0894
  -3.000   0.2108   0.00787   0.00213  -0.1076   0.7171   0.1956
  -2.500   0.2560   0.00777   0.00205  -0.1053   0.7006   0.2228
  -2.250   0.2779   0.00776   0.00201  -0.1040   0.6918   0.2323
  -2.000   0.2992   0.00773   0.00198  -0.1026   0.6799   0.2406
  -1.750   0.3190   0.00774   0.00194  -0.1008   0.6647   0.2470
  -1.500   0.3345   0.00778   0.00192  -0.0981   0.6402   0.2545
  -1.250   0.3249   0.00812   0.00195  -0.0901   0.5676   0.2582
  -1.000   0.3212   0.00852   0.00209  -0.0835   0.5135   0.2635
  -0.750   0.3309   0.00873   0.00220  -0.0797   0.4857   0.2737
  -0.500   0.3451   0.00889   0.00231  -0.0770   0.4630   0.2871
  -0.250   0.3584   0.00906   0.00242  -0.0740   0.4397   0.3049
   0.000   0.3725   0.00923   0.00254  -0.0713   0.4143   0.3229
   0.250   0.3852   0.00943   0.00268  -0.0683   0.3890   0.3482
   0.500   0.4001   0.00957   0.00281  -0.0658   0.3712   0.3744
   0.750   0.4155   0.00967   0.00294  -0.0634   0.3579   0.4089
   1.000   0.4326   0.00970   0.00306  -0.0614   0.3491   0.4498
   1.250   0.4487   0.00975   0.00319  -0.0591   0.3414   0.4926
   1.500   0.4647   0.00969   0.00332  -0.0568   0.3361   0.5616
   1.750   0.4779   0.00962   0.00348  -0.0540   0.3308   0.6471
   2.000   0.4867   0.00947   0.00366  -0.0501   0.3263   0.7552
   2.250   0.6395   0.00944   0.00407  -0.0777   0.3167   0.9536
   2.500   0.6871   0.00977   0.00433  -0.0823   0.3116   0.9793
   2.750   0.7230   0.00997   0.00451  -0.0843   0.3090   0.9902
   3.000   0.7611   0.01019   0.00470  -0.0867   0.3066   0.9966
   3.250   0.8034   0.01039   0.00486  -0.0902   0.3034   0.9995
   3.500   0.8264   0.01056   0.00500  -0.0895   0.3007   1.0000
   3.750   0.8408   0.01072   0.00515  -0.0870   0.2984   1.0000
   4.000   0.8551   0.01092   0.00532  -0.0845   0.2954   1.0000
   4.250   0.8725   0.01107   0.00546  -0.0826   0.2936   1.0000
   4.500   0.8907   0.01121   0.00561  -0.0809   0.2921   1.0000
   4.750   0.9092   0.01137   0.00577  -0.0792   0.2900   1.0000
   5.000   0.9275   0.01154   0.00594  -0.0776   0.2871   1.0000
   5.250   0.9454   0.01175   0.00613  -0.0759   0.2846   1.0000
   5.500   0.9631   0.01198   0.00635  -0.0742   0.2819   1.0000
   5.750   0.9810   0.01224   0.00658  -0.0726   0.2786   1.0000
   6.000   1.0015   0.01241   0.00677  -0.0715   0.2769   1.0000
   6.250   1.0218   0.01260   0.00697  -0.0703   0.2731   1.0000
   6.500   1.0411   0.01284   0.00720  -0.0690   0.2686   1.0000
   6.750   1.0594   0.01314   0.00747  -0.0676   0.2632   1.0000
   7.000   1.0800   0.01336   0.00771  -0.0666   0.2598   1.0000
   7.250   1.0983   0.01369   0.00798  -0.0653   0.2508   1.0000
   7.500   1.1171   0.01402   0.00828  -0.0640   0.2398   1.0000
   8.000   1.1317   0.01581   0.00963  -0.0583   0.1732   1.0000
   8.250   1.1473   0.01634   0.01013  -0.0568   0.1664   1.0000
   8.500   1.1641   0.01683   0.01061  -0.0554   0.1627   1.0000
   8.750   1.1814   0.01730   0.01108  -0.0542   0.1603   1.0000
   9.000   1.1979   0.01782   0.01159  -0.0528   0.1570   1.0000
   9.250   1.2141   0.01837   0.01214  -0.0515   0.1535   1.0000
   9.500   1.2332   0.01877   0.01257  -0.0506   0.1520   1.0000
   9.750   1.2521   0.01918   0.01302  -0.0497   0.1502   1.0000
  10.000   1.2693   0.01969   0.01355  -0.0486   0.1478   1.0000
  10.250   1.2855   0.02028   0.01413  -0.0474   0.1447   1.0000
  10.500   1.3000   0.02096   0.01481  -0.0461   0.1404   1.0000
  10.750   1.3183   0.02143   0.01532  -0.0452   0.1378   1.0000
  11.000   1.3350   0.02200   0.01587  -0.0442   0.1305   1.0000
  11.250   1.3487   0.02277   0.01658  -0.0429   0.1181   1.0000
  11.500   1.3327   0.02542   0.01888  -0.0383   0.0653   1.0000
  11.750   1.3127   0.02852   0.02177  -0.0337   0.0215   1.0000
  12.000   1.3200   0.02986   0.02313  -0.0320   0.0180   1.0000
  12.250   1.3301   0.03103   0.02436  -0.0307   0.0168   1.0000
  12.500   1.3382   0.03238   0.02574  -0.0294   0.0156   1.0000
  12.750   1.3436   0.03399   0.02741  -0.0278   0.0143   1.0000
  13.000   1.3527   0.03534   0.02881  -0.0267   0.0140   1.0000
  13.250   1.3602   0.03685   0.03038  -0.0256   0.0134   1.0000
  13.500   1.3664   0.03850   0.03209  -0.0244   0.0129   1.0000
  13.750   1.3716   0.04029   0.03394  -0.0233   0.0124   1.0000
  14.000   1.3740   0.04239   0.03611  -0.0222   0.0121   1.0000
  14.250   1.3720   0.04497   0.03878  -0.0210   0.0116   1.0000
  14.500   1.3721   0.04742   0.04131  -0.0200   0.0113   1.0000
  14.750   1.3751   0.04966   0.04363  -0.0193   0.0112   1.0000
  15.000   1.3760   0.05220   0.04625  -0.0187   0.0109   1.0000
  15.250   1.3744   0.05510   0.04924  -0.0182   0.0107   1.0000
  15.500   1.3732   0.05805   0.05227  -0.0180   0.0105   1.0000
  15.750   1.3686   0.06149   0.05580  -0.0178   0.0102   1.0000
  16.000   1.3652   0.06493   0.05933  -0.0179   0.0101   1.0000
  16.250   1.3571   0.06908   0.06359  -0.0182   0.0099   1.0000
  16.500   1.3506   0.07311   0.06770  -0.0187   0.0097   1.0000
  16.750   1.3388   0.07790   0.07260  -0.0194   0.0096   1.0000
  17.000   1.3248   0.08308   0.07790  -0.0203   0.0095   1.0000
  17.250   1.3103   0.08842   0.08334  -0.0213   0.0094   1.0000
  17.500   1.2932   0.09418   0.08923  -0.0226   0.0093   1.0000
  17.750   1.2785   0.09963   0.09478  -0.0238   0.0092   1.0000
  18.000   1.2630   0.10534   0.10060  -0.0253   0.0092   1.0000
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