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GOE 626 AIRFOIL (goe626-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 626 AIRFOIL (goe626-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.28 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe626-il-1000000.txt
Download as CSV file: xf-goe626-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 626 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.7819   0.12369   0.12084  -0.0577   1.0000   0.0245
 -19.500  -0.7921   0.11876   0.11583  -0.0602   1.0000   0.0247
 -19.250  -0.7960   0.11486   0.11188  -0.0621   1.0000   0.0249
 -19.000  -0.7955   0.11171   0.10871  -0.0635   1.0000   0.0250
 -18.750  -0.7985   0.10796   0.10492  -0.0653   1.0000   0.0252
 -18.500  -0.8006   0.10439   0.10131  -0.0670   1.0000   0.0253
 -18.250  -0.8012   0.10118   0.09806  -0.0684   1.0000   0.0254
 -18.000  -0.8022   0.09785   0.09469  -0.0699   1.0000   0.0256
 -17.750  -0.8051   0.09426   0.09106  -0.0715   1.0000   0.0258
 -17.500  -0.8060   0.09110   0.08786  -0.0728   1.0000   0.0259
 -17.250  -0.8065   0.08809   0.08481  -0.0740   1.0000   0.0260
 -17.000  -0.8092   0.08468   0.08136  -0.0755   1.0000   0.0263
 -16.750  -0.8082   0.08206   0.07870  -0.0763   1.0000   0.0264
 -16.500  -0.8077   0.07942   0.07602  -0.0770   1.0000   0.0266
 -16.250  -0.8086   0.07653   0.07310  -0.0780   1.0000   0.0268
 -16.000  -0.8095   0.07380   0.07033  -0.0788   1.0000   0.0269
 -15.750  -0.8091   0.07139   0.06789  -0.0792   1.0000   0.0271
 -15.500  -0.8084   0.06914   0.06561  -0.0794   1.0000   0.0272
 -15.250  -0.8096   0.06673   0.06317  -0.0797   1.0000   0.0273
 -15.000  -0.8119   0.06435   0.06075  -0.0798   1.0000   0.0275
 -14.750  -0.8138   0.06221   0.05859  -0.0795   1.0000   0.0276
 -14.500  -0.8167   0.06027   0.05663  -0.0789   1.0000   0.0276
 -14.250  -0.8108   0.05781   0.05413  -0.0806   0.9994   0.0278
 -14.000  -0.7972   0.05482   0.05108  -0.0846   0.9981   0.0279
 -13.750  -0.7817   0.05217   0.04839  -0.0883   0.9964   0.0280
 -13.500  -0.7666   0.04934   0.04550  -0.0927   0.9944   0.0281
 -13.250  -0.7452   0.04823   0.04442  -0.0946   0.9929   0.0287
 -13.000  -0.7328   0.04600   0.04218  -0.0973   0.9896   0.0289
 -12.750  -0.7196   0.04340   0.03957  -0.1011   0.9858   0.0292
 -12.500  -0.7043   0.04035   0.03650  -0.1063   0.9826   0.0294
 -12.250  -0.6962   0.03704   0.03315  -0.1112   0.9767   0.0295
 -12.000  -0.6811   0.03291   0.02895  -0.1188   0.9707   0.0297
 -11.750  -0.6557   0.02846   0.02441  -0.1286   0.9678   0.0300
 -11.500  -0.6331   0.02441   0.02025  -0.1360   0.9617   0.0303
 -11.250  -0.6028   0.02095   0.01666  -0.1426   0.9576   0.0305
 -11.000  -0.5701   0.01911   0.01472  -0.1466   0.9545   0.0309
 -10.750  -0.5373   0.01786   0.01338  -0.1495   0.9511   0.0312
 -10.500  -0.5146   0.01697   0.01242  -0.1498   0.9435   0.0315
 -10.250  -0.4837   0.01614   0.01152  -0.1514   0.9387   0.0318
 -10.000  -0.4560   0.01553   0.01084  -0.1521   0.9325   0.0321
  -9.750  -0.4312   0.01468   0.00991  -0.1524   0.9249   0.0325
  -9.500  -0.4038   0.01384   0.00896  -0.1533   0.9186   0.0331
  -9.250  -0.3803   0.01323   0.00830  -0.1529   0.9107   0.0336
  -9.000  -0.3526   0.01271   0.00769  -0.1532   0.9032   0.0341
  -8.750  -0.3275   0.01227   0.00720  -0.1528   0.8951   0.0346
  -8.500  -0.3007   0.01188   0.00673  -0.1528   0.8875   0.0352
  -8.250  -0.2738   0.01153   0.00632  -0.1526   0.8810   0.0357
  -8.000  -0.2474   0.01121   0.00595  -0.1524   0.8737   0.0363
  -7.750  -0.2200   0.01091   0.00556  -0.1522   0.8667   0.0370
  -7.500  -0.1937   0.01054   0.00516  -0.1520   0.8597   0.0383
  -7.250  -0.1669   0.01023   0.00480  -0.1517   0.8518   0.0398
  -7.000  -0.1397   0.00996   0.00449  -0.1515   0.8444   0.0420
  -6.750  -0.1142   0.00940   0.00400  -0.1512   0.8360   0.0608
  -6.500  -0.0878   0.00900   0.00365  -0.1509   0.8274   0.0837
  -6.250  -0.0613   0.00866   0.00334  -0.1506   0.8179   0.0986
  -6.000  -0.0351   0.00827   0.00301  -0.1503   0.8079   0.1220
  -5.750  -0.0093   0.00783   0.00267  -0.1500   0.7961   0.1559
  -5.500   0.0171   0.00758   0.00248  -0.1496   0.7829   0.1815
  -5.250   0.0436   0.00748   0.00238  -0.1491   0.7669   0.1996
  -5.000   0.0701   0.00746   0.00232  -0.1485   0.7469   0.2107
  -4.750   0.0954   0.00753   0.00228  -0.1477   0.7185   0.2187
  -4.500   0.1198   0.00764   0.00226  -0.1467   0.6856   0.2253
  -4.250   0.1447   0.00779   0.00228  -0.1457   0.6601   0.2307
  -3.750   0.1982   0.00796   0.00227  -0.1447   0.6303   0.2376
  -3.500   0.2252   0.00802   0.00229  -0.1442   0.6192   0.2414
  -3.250   0.2528   0.00810   0.00233  -0.1439   0.6096   0.2449
  -3.000   0.2803   0.00820   0.00238  -0.1435   0.6007   0.2485
  -2.750   0.3086   0.00830   0.00243  -0.1433   0.5933   0.2511
  -2.500   0.3358   0.00833   0.00241  -0.1429   0.5853   0.2540
  -2.250   0.3637   0.00833   0.00242  -0.1426   0.5784   0.2573
  -2.000   0.3915   0.00839   0.00246  -0.1423   0.5702   0.2598
  -1.750   0.4188   0.00849   0.00251  -0.1419   0.5611   0.2626
  -1.500   0.4467   0.00856   0.00256  -0.1416   0.5520   0.2652
  -1.250   0.4737   0.00865   0.00259  -0.1412   0.5432   0.2669
  -1.000   0.5018   0.00869   0.00260  -0.1409   0.5352   0.2680
  -0.500   0.5557   0.00871   0.00256  -0.1401   0.5155   0.2732
  -0.250   0.5821   0.00878   0.00258  -0.1396   0.5037   0.2752
   0.000   0.6089   0.00884   0.00260  -0.1391   0.4921   0.2767
   0.250   0.6357   0.00890   0.00263  -0.1387   0.4820   0.2781
   0.500   0.6620   0.00899   0.00267  -0.1381   0.4717   0.2797
   0.750   0.6888   0.00906   0.00271  -0.1377   0.4627   0.2814
   1.000   0.7150   0.00916   0.00276  -0.1371   0.4532   0.2829
   1.250   0.7416   0.00923   0.00281  -0.1367   0.4452   0.2841
   1.500   0.7679   0.00933   0.00286  -0.1361   0.4369   0.2851
   1.750   0.7941   0.00943   0.00293  -0.1356   0.4295   0.2860
   2.000   0.8206   0.00952   0.00300  -0.1351   0.4221   0.2866
   2.250   0.8456   0.00958   0.00301  -0.1344   0.4129   0.2896
   2.500   0.8717   0.00964   0.00307  -0.1339   0.4037   0.2921
   2.750   0.8966   0.00977   0.00316  -0.1331   0.3949   0.2939
   3.000   0.9231   0.00983   0.00324  -0.1327   0.3890   0.2957
   3.250   0.9487   0.00994   0.00333  -0.1320   0.3828   0.2973
   3.500   0.9737   0.01007   0.00343  -0.1313   0.3764   0.2991
   3.750   0.9998   0.01015   0.00352  -0.1308   0.3703   0.3009
   4.000   1.0245   0.01029   0.00362  -0.1300   0.3630   0.3024
   4.250   1.0494   0.01041   0.00374  -0.1293   0.3559   0.3037
   4.500   1.0743   0.01054   0.00385  -0.1286   0.3485   0.3048
   4.750   1.0979   0.01068   0.00396  -0.1276   0.3416   0.3078
   5.000   1.1231   0.01074   0.00406  -0.1270   0.3364   0.3112
   5.250   1.1467   0.01088   0.00420  -0.1260   0.3291   0.3139
   5.500   1.1691   0.01104   0.00434  -0.1248   0.3224   0.3163
   5.750   1.1920   0.01116   0.00447  -0.1237   0.3155   0.3187
   6.000   1.2124   0.01137   0.00463  -0.1222   0.3065   0.3209
   6.250   1.2348   0.01151   0.00478  -0.1210   0.2985   0.3228
   6.500   1.2549   0.01175   0.00498  -0.1195   0.2889   0.3256
   6.750   1.2758   0.01195   0.00517  -0.1181   0.2785   0.3299
   7.000   1.2953   0.01222   0.00542  -0.1165   0.2660   0.3336
   7.250   1.3132   0.01258   0.00571  -0.1147   0.2495   0.3374
   7.500   1.3276   0.01311   0.00610  -0.1123   0.2261   0.3407
   7.750   1.3377   0.01382   0.00664  -0.1092   0.1954   0.3442
   8.000   1.3507   0.01439   0.00713  -0.1067   0.1782   0.3508
   8.250   1.3656   0.01486   0.00756  -0.1046   0.1684   0.3574
   8.500   1.3827   0.01524   0.00796  -0.1028   0.1623   0.3667
   8.750   1.3996   0.01561   0.00836  -0.1010   0.1576   0.3796
   9.250   1.4326   0.01634   0.00926  -0.0974   0.1488   0.4457
   9.500   1.4495   0.01661   0.00972  -0.0957   0.1452   0.5339
   9.750   1.4699   0.01644   0.01036  -0.0950   0.1400   1.0000
  10.000   1.4855   0.01694   0.01085  -0.0932   0.1346   1.0000
  10.250   1.5001   0.01752   0.01139  -0.0913   0.1270   1.0000
  10.500   1.5129   0.01819   0.01203  -0.0893   0.1173   1.0000
  10.750   1.5101   0.01970   0.01331  -0.0854   0.0869   1.0000
  11.000   1.5075   0.02129   0.01478  -0.0818   0.0701   1.0000
  11.250   1.5148   0.02239   0.01587  -0.0795   0.0657   1.0000
  11.500   1.5247   0.02338   0.01687  -0.0776   0.0632   1.0000
  11.750   1.5336   0.02445   0.01797  -0.0757   0.0614   1.0000
  12.000   1.5412   0.02566   0.01920  -0.0738   0.0596   1.0000
  12.250   1.5491   0.02690   0.02047  -0.0720   0.0583   1.0000
  12.500   1.5569   0.02820   0.02180  -0.0703   0.0573   1.0000
  12.750   1.5669   0.02937   0.02302  -0.0690   0.0567   1.0000
  13.000   1.5759   0.03067   0.02437  -0.0676   0.0562   1.0000
  13.250   1.5834   0.03213   0.02588  -0.0663   0.0557   1.0000
  13.500   1.5902   0.03370   0.02751  -0.0650   0.0550   1.0000
  13.750   1.5964   0.03540   0.02926  -0.0639   0.0546   1.0000
  14.000   1.6011   0.03730   0.03121  -0.0628   0.0542   1.0000
  14.250   1.6052   0.03934   0.03331  -0.0619   0.0536   1.0000
  14.500   1.6080   0.04160   0.03562  -0.0611   0.0530   1.0000
  14.750   1.6095   0.04407   0.03816  -0.0605   0.0525   1.0000
  15.000   1.6093   0.04683   0.04098  -0.0599   0.0519   1.0000
  15.250   1.6063   0.04998   0.04421  -0.0596   0.0512   1.0000
  15.500   1.6049   0.05303   0.04734  -0.0594   0.0510   1.0000
  15.750   1.6053   0.05592   0.05030  -0.0593   0.0506   1.0000
  16.000   1.6077   0.05862   0.05307  -0.0592   0.0504   1.0000
  16.250   1.6092   0.06146   0.05599  -0.0593   0.0502   1.0000
  16.500   1.6090   0.06458   0.05919  -0.0594   0.0500   1.0000
  16.750   1.6090   0.06772   0.06240  -0.0597   0.0496   1.0000
  17.000   1.6081   0.07103   0.06578  -0.0601   0.0493   1.0000
  17.250   1.6070   0.07441   0.06925  -0.0605   0.0490   1.0000
  17.500   1.6045   0.07808   0.07299  -0.0612   0.0487   1.0000
  17.750   1.6021   0.08177   0.07675  -0.0619   0.0484   1.0000
  18.000   1.6008   0.08534   0.08039  -0.0627   0.0480   1.0000
  18.250   1.5978   0.08922   0.08434  -0.0636   0.0476   1.0000
  18.500   1.5944   0.09322   0.08842  -0.0647   0.0473   1.0000
  18.750   1.5913   0.09720   0.09246  -0.0658   0.0468   1.0000
  19.000   1.5871   0.10138   0.09671  -0.0671   0.0464   1.0000
  19.250   1.5811   0.10589   0.10129  -0.0686   0.0459   1.0000
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