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GOE 430 AIRFOIL (goe430-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 430 AIRFOIL (goe430-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.77 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe430-il-1000000-n5.txt
Download as CSV file: xf-goe430-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 430 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.7306   0.12681   0.12469  -0.0429   1.0000   0.0223
 -17.500  -0.7890   0.11219   0.10992  -0.0514   1.0000   0.0232
 -17.250  -0.8213   0.10281   0.10045  -0.0570   1.0000   0.0240
 -17.000  -0.8504   0.09424   0.09179  -0.0624   1.0000   0.0245
 -16.750  -0.8806   0.08573   0.08318  -0.0679   1.0000   0.0249
 -16.500  -0.9140   0.07695   0.07429  -0.0738   1.0000   0.0252
 -16.250  -0.9568   0.06712   0.06433  -0.0806   1.0000   0.0251
 -16.000  -1.0064   0.05675   0.05381  -0.0882   1.0000   0.0249
 -15.750  -1.0561   0.04676   0.04367  -0.0957   1.0000   0.0245
 -15.250  -1.0890   0.03067   0.02723  -0.1153   0.9872   0.0253
 -15.000  -1.0625   0.02597   0.02240  -0.1258   0.9794   0.0266
 -14.750  -1.0319   0.02355   0.01986  -0.1321   0.9727   0.0281
 -14.500  -1.0045   0.02226   0.01848  -0.1349   0.9661   0.0292
 -14.250  -0.9771   0.02124   0.01735  -0.1369   0.9593   0.0299
 -14.000  -0.9509   0.02032   0.01635  -0.1384   0.9520   0.0307
 -13.750  -0.9245   0.01961   0.01559  -0.1394   0.9449   0.0316
 -13.500  -0.8979   0.01903   0.01496  -0.1402   0.9388   0.0325
 -13.250  -0.8713   0.01847   0.01434  -0.1409   0.9329   0.0332
 -12.750  -0.8176   0.01744   0.01314  -0.1421   0.9224   0.0344
 -12.500  -0.7905   0.01699   0.01261  -0.1426   0.9167   0.0349
 -12.000  -0.7361   0.01601   0.01147  -0.1436   0.9062   0.0359
 -11.750  -0.7087   0.01551   0.01092  -0.1442   0.9008   0.0366
 -11.500  -0.6810   0.01515   0.01051  -0.1445   0.8956   0.0374
 -11.250  -0.6529   0.01483   0.01016  -0.1449   0.8910   0.0381
 -11.000  -0.6247   0.01454   0.00982  -0.1453   0.8863   0.0387
 -10.750  -0.5964   0.01429   0.00953  -0.1456   0.8822   0.0395
 -10.500  -0.5680   0.01402   0.00920  -0.1459   0.8786   0.0402
 -10.250  -0.5394   0.01369   0.00881  -0.1464   0.8753   0.0406
 -10.000  -0.5107   0.01336   0.00843  -0.1468   0.8717   0.0409
  -9.750  -0.4821   0.01303   0.00803  -0.1472   0.8674   0.0412
  -9.500  -0.4536   0.01272   0.00765  -0.1475   0.8627   0.0414
  -9.250  -0.4248   0.01242   0.00729  -0.1478   0.8580   0.0416
  -9.000  -0.3961   0.01193   0.00673  -0.1484   0.8528   0.0422
  -8.750  -0.3672   0.01154   0.00627  -0.1488   0.8481   0.0428
  -8.500  -0.3382   0.01122   0.00590  -0.1492   0.8441   0.0434
  -8.250  -0.3089   0.01093   0.00558  -0.1496   0.8398   0.0439
  -8.000  -0.2798   0.01067   0.00528  -0.1500   0.8344   0.0444
  -7.750  -0.2507   0.01045   0.00500  -0.1502   0.8288   0.0450
  -7.500  -0.2213   0.01022   0.00474  -0.1506   0.8237   0.0455
  -7.250  -0.1920   0.01002   0.00450  -0.1509   0.8174   0.0462
  -7.000  -0.1629   0.00984   0.00426  -0.1511   0.8110   0.0468
  -6.750  -0.1335   0.00966   0.00404  -0.1514   0.8039   0.0474
  -6.500  -0.1043   0.00950   0.00382  -0.1516   0.7963   0.0479
  -6.250  -0.0750   0.00934   0.00362  -0.1519   0.7878   0.0484
  -6.000  -0.0459   0.00922   0.00343  -0.1521   0.7782   0.0488
  -5.750  -0.0166   0.00910   0.00325  -0.1523   0.7677   0.0491
  -5.500   0.0127   0.00893   0.00302  -0.1525   0.7581   0.0502
  -5.250   0.0418   0.00879   0.00282  -0.1527   0.7470   0.0515
  -5.000   0.0710   0.00868   0.00266  -0.1529   0.7341   0.0527
  -4.750   0.1000   0.00859   0.00251  -0.1531   0.7204   0.0540
  -4.500   0.1290   0.00852   0.00238  -0.1532   0.7061   0.0553
  -4.250   0.1579   0.00847   0.00226  -0.1534   0.6922   0.0566
  -4.000   0.1868   0.00844   0.00216  -0.1535   0.6788   0.0580
  -3.750   0.2157   0.00840   0.00207  -0.1536   0.6658   0.0608
  -3.500   0.2447   0.00834   0.00197  -0.1538   0.6532   0.0649
  -3.250   0.2736   0.00828   0.00188  -0.1540   0.6395   0.0727
  -3.000   0.3026   0.00815   0.00181  -0.1542   0.6255   0.0989
  -2.750   0.3314   0.00813   0.00178  -0.1544   0.6124   0.1139
  -2.250   0.3891   0.00815   0.00175  -0.1546   0.5883   0.1276
  -2.000   0.4178   0.00819   0.00174  -0.1547   0.5769   0.1319
  -1.750   0.4465   0.00821   0.00174  -0.1548   0.5642   0.1376
  -1.500   0.4752   0.00825   0.00173  -0.1548   0.5516   0.1422
  -1.250   0.5039   0.00829   0.00174  -0.1549   0.5386   0.1458
  -1.000   0.5323   0.00836   0.00175  -0.1549   0.5240   0.1488
  -0.750   0.5606   0.00843   0.00176  -0.1549   0.5080   0.1537
  -0.500   0.5889   0.00851   0.00179  -0.1549   0.4923   0.1587
  -0.250   0.6169   0.00860   0.00182  -0.1549   0.4768   0.1657
   0.000   0.6447   0.00870   0.00187  -0.1549   0.4589   0.1753
   0.250   0.6722   0.00883   0.00195  -0.1548   0.4394   0.1900
   0.500   0.7004   0.00885   0.00202  -0.1549   0.4269   0.2254
   0.750   0.7286   0.00890   0.00210  -0.1550   0.4183   0.2564
   1.000   0.7573   0.00892   0.00217  -0.1551   0.4129   0.2772
   1.250   0.7856   0.00899   0.00224  -0.1551   0.4072   0.2913
   1.500   0.8138   0.00906   0.00232  -0.1551   0.4018   0.3032
   1.750   0.8423   0.00910   0.00239  -0.1551   0.3969   0.3141
   2.000   0.8703   0.00918   0.00248  -0.1551   0.3901   0.3253
   2.250   0.8983   0.00927   0.00257  -0.1551   0.3830   0.3398
   2.500   0.9262   0.00934   0.00268  -0.1551   0.3741   0.3598
   2.750   0.9541   0.00941   0.00279  -0.1550   0.3665   0.3852
   3.000   0.9817   0.00950   0.00292  -0.1550   0.3560   0.4177
   3.250   1.0089   0.00963   0.00307  -0.1549   0.3419   0.4480
   3.500   1.0287   0.01042   0.00349  -0.1536   0.2619   0.4695
   3.750   1.0516   0.01095   0.00386  -0.1528   0.2266   0.4860
   4.000   1.0772   0.01121   0.00410  -0.1523   0.2144   0.5021
   4.250   1.1037   0.01139   0.00429  -0.1521   0.2078   0.5177
   4.500   1.1292   0.01164   0.00453  -0.1517   0.1989   0.5311
   4.750   1.1558   0.01179   0.00472  -0.1514   0.1942   0.5492
   5.000   1.1820   0.01195   0.00493  -0.1511   0.1895   0.5717
   5.250   1.2078   0.01215   0.00516  -0.1507   0.1846   0.5938
   5.500   1.2337   0.01233   0.00540  -0.1503   0.1803   0.6208
   5.750   1.2595   0.01251   0.00562  -0.1499   0.1753   0.6451
   6.000   1.2837   0.01281   0.00589  -0.1493   0.1656   0.6628
   6.250   1.3080   0.01309   0.00616  -0.1487   0.1543   0.6778
   6.500   1.3310   0.01345   0.00646  -0.1479   0.1399   0.6904
   6.750   1.3512   0.01400   0.00690  -0.1467   0.1147   0.7034
   7.000   1.3696   0.01465   0.00743  -0.1451   0.0924   0.7196
   7.250   1.3910   0.01503   0.00784  -0.1441   0.0850   0.7441
   7.500   1.4082   0.01495   0.00817  -0.1420   0.0821   1.0000
   7.750   1.4298   0.01532   0.00854  -0.1409   0.0797   1.0000
   8.000   1.4504   0.01572   0.00892  -0.1397   0.0767   1.0000
   8.250   1.4700   0.01608   0.00929  -0.1382   0.0741   1.0000
   8.500   1.4896   0.01641   0.00965  -0.1368   0.0727   1.0000
   8.750   1.5086   0.01680   0.01005  -0.1353   0.0707   1.0000
   9.000   1.5261   0.01727   0.01052  -0.1337   0.0676   1.0000
   9.250   1.5421   0.01784   0.01107  -0.1318   0.0631   1.0000
   9.500   1.5594   0.01833   0.01157  -0.1302   0.0582   1.0000
   9.750   1.5567   0.02004   0.01304  -0.1259   0.0262   1.0000
  10.000   1.5660   0.02110   0.01408  -0.1234   0.0189   1.0000
  10.250   1.5789   0.02195   0.01494  -0.1214   0.0165   1.0000
  10.500   1.5921   0.02281   0.01582  -0.1196   0.0150   1.0000
  10.750   1.6052   0.02368   0.01673  -0.1179   0.0140   1.0000
  11.000   1.6175   0.02464   0.01771  -0.1161   0.0131   1.0000
  11.250   1.6289   0.02569   0.01879  -0.1143   0.0123   1.0000
  11.500   1.6413   0.02668   0.01982  -0.1126   0.0118   1.0000
  11.750   1.6529   0.02775   0.02094  -0.1110   0.0114   1.0000
  12.000   1.6637   0.02891   0.02214  -0.1093   0.0109   1.0000
  12.250   1.6736   0.03017   0.02344  -0.1077   0.0104   1.0000
  12.500   1.6822   0.03156   0.02487  -0.1060   0.0100   1.0000
  12.750   1.6897   0.03307   0.02643  -0.1043   0.0096   1.0000
  13.000   1.6981   0.03455   0.02797  -0.1028   0.0094   1.0000
  13.250   1.7062   0.03608   0.02955  -0.1014   0.0092   1.0000
  13.500   1.7134   0.03772   0.03126  -0.1000   0.0090   1.0000
  13.750   1.7199   0.03948   0.03307  -0.0987   0.0087   1.0000
  14.000   1.7257   0.04135   0.03501  -0.0974   0.0085   1.0000
  14.250   1.7309   0.04335   0.03707  -0.0962   0.0083   1.0000
  14.500   1.7351   0.04549   0.03927  -0.0951   0.0081   1.0000
  14.750   1.7386   0.04778   0.04162  -0.0941   0.0079   1.0000
  15.000   1.7411   0.05025   0.04415  -0.0932   0.0077   1.0000
  15.250   1.7425   0.05291   0.04689  -0.0924   0.0075   1.0000
  15.500   1.7417   0.05587   0.04993  -0.0917   0.0073   1.0000
  15.750   1.7437   0.05856   0.05269  -0.0912   0.0072   1.0000
  16.000   1.7448   0.06141   0.05562  -0.0907   0.0071   1.0000
  16.250   1.7452   0.06441   0.05870  -0.0903   0.0069   1.0000
  16.500   1.7444   0.06760   0.06197  -0.0901   0.0068   1.0000
  16.750   1.7425   0.07094   0.06540  -0.0899   0.0067   1.0000
  17.000   1.7397   0.07446   0.06900  -0.0899   0.0066   1.0000
  17.250   1.7361   0.07815   0.07278  -0.0899   0.0065   1.0000
  17.500   1.7319   0.08198   0.07669  -0.0901   0.0064   1.0000
  17.750   1.7270   0.08594   0.08075  -0.0905   0.0064   1.0000
  18.000   1.7211   0.09006   0.08497  -0.0909   0.0063   1.0000
  18.250   1.7149   0.09432   0.08931  -0.0915   0.0062   1.0000
  18.500   1.7080   0.09873   0.09381  -0.0922   0.0061   1.0000
  18.750   1.7003   0.10330   0.09847  -0.0932   0.0060   1.0000
  19.000   1.6921   0.10798   0.10325  -0.0942   0.0060   1.0000
  19.250   1.6833   0.11278   0.10815  -0.0954   0.0059   1.0000
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