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GOE 430 AIRFOIL (goe430-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 430 AIRFOIL (goe430-il)
Reynolds number: 1,000,000
Max Cl/Cd: 125.09 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe430-il-1000000.txt
Download as CSV file: xf-goe430-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.7922   0.11100   0.10882  -0.0523   1.0000   0.0280
 -17.250  -0.8308   0.10045   0.09813  -0.0588   1.0000   0.0285
 -17.000  -0.8494   0.09367   0.09133  -0.0630   1.0000   0.0292
 -16.750  -0.8678   0.08692   0.08453  -0.0674   1.0000   0.0297
 -16.500  -0.8885   0.07989   0.07744  -0.0720   1.0000   0.0301
 -16.250  -0.9096   0.07292   0.07039  -0.0767   1.0000   0.0305
 -16.000  -0.9325   0.06591   0.06329  -0.0816   1.0000   0.0309
 -15.750  -0.9556   0.05924   0.05653  -0.0865   1.0000   0.0312
 -15.500  -0.9785   0.05273   0.04993  -0.0914   1.0000   0.0314
 -15.250  -0.9986   0.04684   0.04395  -0.0957   1.0000   0.0317
 -15.000  -1.0254   0.04141   0.03843  -0.0983   1.0000   0.0318
 -14.750  -1.0495   0.03629   0.03323  -0.1013   0.9978   0.0320
 -14.500  -1.0226   0.03252   0.02933  -0.1095   0.9948   0.0327
 -14.250  -0.9913   0.02964   0.02631  -0.1167   0.9925   0.0331
 -14.000  -0.9583   0.02500   0.02152  -0.1286   0.9877   0.0343
 -13.750  -0.9236   0.02373   0.02020  -0.1329   0.9857   0.0350
 -13.500  -0.8898   0.02298   0.01941  -0.1358   0.9837   0.0358
 -13.250  -0.8561   0.02231   0.01869  -0.1385   0.9818   0.0366
 -13.000  -0.8278   0.02166   0.01796  -0.1399   0.9766   0.0373
 -12.750  -0.7977   0.02102   0.01723  -0.1417   0.9725   0.0379
 -12.500  -0.7667   0.02047   0.01660  -0.1433   0.9690   0.0384
 -12.250  -0.7417   0.01972   0.01575  -0.1440   0.9619   0.0388
 -12.000  -0.7168   0.01842   0.01436  -0.1454   0.9560   0.0399
 -11.750  -0.6905   0.01792   0.01383  -0.1458   0.9498   0.0406
 -11.500  -0.6638   0.01749   0.01336  -0.1462   0.9437   0.0412
 -11.250  -0.6367   0.01709   0.01289  -0.1465   0.9384   0.0419
 -11.000  -0.6095   0.01670   0.01245  -0.1469   0.9330   0.0426
 -10.750  -0.5820   0.01633   0.01200  -0.1473   0.9284   0.0433
 -10.500  -0.5539   0.01607   0.01167  -0.1476   0.9243   0.0440
 -10.250  -0.5255   0.01591   0.01145  -0.1479   0.9204   0.0446
 -10.000  -0.4971   0.01571   0.01119  -0.1482   0.9161   0.0449
  -9.750  -0.4715   0.01435   0.00971  -0.1490   0.9115   0.0461
  -9.500  -0.4438   0.01377   0.00907  -0.1494   0.9068   0.0468
  -9.250  -0.4157   0.01331   0.00858  -0.1498   0.9025   0.0474
  -9.000  -0.3874   0.01291   0.00814  -0.1502   0.8980   0.0480
  -8.750  -0.3590   0.01257   0.00773  -0.1504   0.8936   0.0487
  -8.500  -0.3304   0.01226   0.00737  -0.1507   0.8891   0.0495
  -8.250  -0.3016   0.01191   0.00698  -0.1511   0.8849   0.0501
  -8.000  -0.2727   0.01159   0.00660  -0.1514   0.8806   0.0507
  -7.750  -0.2439   0.01130   0.00625  -0.1516   0.8763   0.0513
  -7.500  -0.2149   0.01105   0.00594  -0.1519   0.8720   0.0517
  -7.250  -0.1857   0.01080   0.00566  -0.1522   0.8675   0.0521
  -7.000  -0.1565   0.01034   0.00514  -0.1526   0.8630   0.0529
  -6.750  -0.1273   0.00991   0.00464  -0.1531   0.8584   0.0543
  -6.500  -0.0979   0.00962   0.00433  -0.1534   0.8535   0.0556
  -6.250  -0.0685   0.00937   0.00405  -0.1537   0.8478   0.0566
  -6.000  -0.0393   0.00916   0.00378  -0.1539   0.8420   0.0577
  -5.750  -0.0098   0.00897   0.00355  -0.1542   0.8366   0.0587
  -5.500   0.0197   0.00879   0.00334  -0.1545   0.8310   0.0597
  -5.250   0.0491   0.00865   0.00314  -0.1547   0.8255   0.0605
  -5.000   0.0789   0.00841   0.00287  -0.1550   0.8198   0.0628
  -4.750   0.1085   0.00820   0.00265  -0.1553   0.8133   0.0655
  -4.500   0.1379   0.00805   0.00247  -0.1555   0.8068   0.0685
  -4.250   0.1676   0.00787   0.00230  -0.1558   0.7995   0.0740
  -4.000   0.1971   0.00764   0.00213  -0.1562   0.7917   0.0923
  -3.750   0.2267   0.00748   0.00205  -0.1565   0.7834   0.1172
  -3.500   0.2558   0.00742   0.00199  -0.1566   0.7741   0.1286
  -3.250   0.2850   0.00739   0.00193  -0.1567   0.7633   0.1342
  -3.000   0.3140   0.00735   0.00187  -0.1568   0.7505   0.1405
  -2.750   0.3426   0.00736   0.00182  -0.1568   0.7347   0.1451
  -2.500   0.3712   0.00740   0.00178  -0.1567   0.7184   0.1484
  -2.250   0.3999   0.00737   0.00172  -0.1568   0.7036   0.1549
  -2.000   0.4286   0.00739   0.00168  -0.1569   0.6896   0.1596
  -1.750   0.4571   0.00744   0.00166  -0.1568   0.6757   0.1629
  -1.500   0.4858   0.00745   0.00163  -0.1569   0.6616   0.1686
  -1.250   0.5143   0.00747   0.00161  -0.1570   0.6470   0.1755
  -1.000   0.5429   0.00748   0.00160  -0.1570   0.6332   0.1872
  -0.750   0.5717   0.00743   0.00162  -0.1572   0.6216   0.2158
  -0.500   0.6004   0.00741   0.00166  -0.1573   0.6103   0.2564
  -0.250   0.6292   0.00743   0.00169  -0.1574   0.5995   0.2789
   0.000   0.6577   0.00747   0.00173  -0.1575   0.5882   0.2960
   0.250   0.6859   0.00754   0.00178  -0.1575   0.5736   0.3135
   0.500   0.7140   0.00761   0.00183  -0.1574   0.5579   0.3298
   0.750   0.7420   0.00769   0.00189  -0.1574   0.5422   0.3447
   1.000   0.7699   0.00777   0.00195  -0.1574   0.5249   0.3630
   1.250   0.7976   0.00786   0.00204  -0.1573   0.5056   0.3901
   1.500   0.8252   0.00796   0.00215  -0.1572   0.4881   0.4259
   1.750   0.8527   0.00809   0.00227  -0.1571   0.4740   0.4540
   2.000   0.8804   0.00820   0.00239  -0.1570   0.4629   0.4779
   2.250   0.9083   0.00829   0.00249  -0.1570   0.4542   0.4992
   2.500   0.9359   0.00841   0.00261  -0.1568   0.4457   0.5171
   2.750   0.9638   0.00850   0.00273  -0.1568   0.4385   0.5340
   3.000   0.9911   0.00864   0.00286  -0.1566   0.4292   0.5523
   3.250   1.0188   0.00874   0.00299  -0.1565   0.4214   0.5735
   3.500   1.0462   0.00885   0.00314  -0.1564   0.4143   0.5957
   3.750   1.0737   0.00896   0.00329  -0.1562   0.4081   0.6188
   4.000   1.1013   0.00907   0.00343  -0.1561   0.4014   0.6409
   4.250   1.1280   0.00924   0.00359  -0.1558   0.3937   0.6581
   4.500   1.1556   0.00933   0.00372  -0.1557   0.3860   0.6742
   4.750   1.1820   0.00950   0.00389  -0.1554   0.3755   0.6908
   5.000   1.2084   0.00966   0.00405  -0.1551   0.3623   0.7082
   5.250   1.2340   0.00988   0.00424  -0.1547   0.3411   0.7279
   5.500   1.2491   0.01092   0.00485  -0.1526   0.2525   0.7518
   5.750   1.2693   0.01126   0.00530  -0.1513   0.2272   0.8479
   6.000   1.2887   0.01144   0.00557  -0.1495   0.2145   1.0000
   6.250   1.3126   0.01181   0.00587  -0.1488   0.2049   1.0000
   6.500   1.3377   0.01207   0.00612  -0.1483   0.1987   1.0000
   6.750   1.3612   0.01243   0.00643  -0.1476   0.1904   1.0000
   7.000   1.3862   0.01266   0.00666  -0.1471   0.1851   1.0000
   7.250   1.4097   0.01300   0.00695  -0.1463   0.1771   1.0000
   7.500   1.4334   0.01329   0.00723  -0.1456   0.1698   1.0000
   7.750   1.4555   0.01368   0.00756  -0.1447   0.1587   1.0000
   8.000   1.4766   0.01412   0.00791  -0.1436   0.1443   1.0000
   8.250   1.4945   0.01473   0.00839  -0.1419   0.1218   1.0000
   8.500   1.5089   0.01548   0.00899  -0.1397   0.1015   1.0000
   8.750   1.5234   0.01607   0.00952  -0.1375   0.0922   1.0000
   9.000   1.5398   0.01660   0.01004  -0.1356   0.0877   1.0000
   9.250   1.5550   0.01719   0.01061  -0.1335   0.0827   1.0000
   9.500   1.5727   0.01766   0.01111  -0.1319   0.0800   1.0000
   9.750   1.5894   0.01819   0.01166  -0.1302   0.0770   1.0000
  10.000   1.6035   0.01889   0.01234  -0.1282   0.0728   1.0000
  10.250   1.6197   0.01947   0.01294  -0.1266   0.0681   1.0000
  10.500   1.6313   0.02035   0.01376  -0.1244   0.0568   1.0000
  10.750   1.6224   0.02260   0.01576  -0.1197   0.0255   1.0000
  11.000   1.6291   0.02392   0.01708  -0.1172   0.0210   1.0000
  11.250   1.6389   0.02507   0.01826  -0.1151   0.0190   1.0000
  11.500   1.6489   0.02623   0.01946  -0.1132   0.0179   1.0000
  11.750   1.6566   0.02759   0.02087  -0.1111   0.0167   1.0000
  12.000   1.6662   0.02885   0.02218  -0.1093   0.0161   1.0000
  12.250   1.6757   0.03014   0.02352  -0.1076   0.0156   1.0000
  12.500   1.6841   0.03154   0.02498  -0.1059   0.0150   1.0000
  12.750   1.6910   0.03311   0.02660  -0.1041   0.0145   1.0000
  13.000   1.6957   0.03492   0.02847  -0.1023   0.0140   1.0000
  13.250   1.6961   0.03716   0.03080  -0.1003   0.0135   1.0000
  13.500   1.7030   0.03886   0.03256  -0.0990   0.0133   1.0000
  13.750   1.7089   0.04071   0.03448  -0.0977   0.0130   1.0000
  14.000   1.7137   0.04274   0.03657  -0.0964   0.0127   1.0000
  14.250   1.7175   0.04491   0.03882  -0.0953   0.0124   1.0000
  14.500   1.7207   0.04723   0.04120  -0.0942   0.0121   1.0000
  14.750   1.7227   0.04975   0.04379  -0.0933   0.0119   1.0000
  15.000   1.7227   0.05256   0.04669  -0.0924   0.0116   1.0000
  15.250   1.7201   0.05576   0.04997  -0.0917   0.0114   1.0000
  15.500   1.7134   0.05954   0.05385  -0.0910   0.0111   1.0000
  15.750   1.7028   0.06396   0.05839  -0.0906   0.0109   1.0000
  16.000   1.7025   0.06712   0.06163  -0.0904   0.0109   1.0000
  16.250   1.7013   0.07043   0.06503  -0.0902   0.0107   1.0000
  16.500   1.6980   0.07407   0.06876  -0.0902   0.0106   1.0000
  16.750   1.6938   0.07789   0.07267  -0.0903   0.0105   1.0000
  17.000   1.6890   0.08187   0.07675  -0.0906   0.0104   1.0000
  17.250   1.6828   0.08609   0.08107  -0.0910   0.0102   1.0000
  17.500   1.6756   0.09049   0.08557  -0.0915   0.0101   1.0000
  17.750   1.6681   0.09502   0.09019  -0.0922   0.0100   1.0000
  18.000   1.6602   0.09967   0.09494  -0.0930   0.0099   1.0000
  18.250   1.6519   0.10443   0.09980  -0.0940   0.0098   1.0000
  18.500   1.6426   0.10938   0.10484  -0.0952   0.0097   1.0000
  18.750   1.6334   0.11434   0.10990  -0.0965   0.0096   1.0000
  19.000   1.6244   0.11934   0.11499  -0.0980   0.0095   1.0000
  19.250   1.6148   0.12450   0.12025  -0.0997   0.0094   1.0000
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