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GOE 600 AIRFOIL (goe600-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 600 AIRFOIL (goe600-il)
Reynolds number: 100,000
Max Cl/Cd: 49.42 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe600-il-100000-n5.txt
Download as CSV file: xf-goe600-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 600 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.7348   0.07340   0.06791  -0.0482   1.0000   0.0279
 -12.250  -0.7577   0.06599   0.06031  -0.0538   1.0000   0.0278
 -12.000  -0.7791   0.05974   0.05384  -0.0581   1.0000   0.0278
 -11.750  -0.7992   0.05465   0.04847  -0.0605   1.0000   0.0279
 -11.500  -0.8115   0.05112   0.04478  -0.0608   1.0000   0.0282
 -11.250  -0.8152   0.04887   0.04246  -0.0597   1.0000   0.0288
 -11.000  -0.8174   0.04688   0.04037  -0.0582   1.0000   0.0294
 -10.750  -0.8168   0.04473   0.03805  -0.0568   1.0000   0.0302
 -10.500  -0.8148   0.04241   0.03549  -0.0552   1.0000   0.0312
 -10.250  -0.8110   0.03999   0.03278  -0.0535   1.0000   0.0322
 -10.000  -0.8047   0.03765   0.03012  -0.0516   1.0000   0.0334
  -9.750  -0.7964   0.03560   0.02771  -0.0497   1.0000   0.0350
  -9.500  -0.7852   0.03425   0.02639  -0.0481   1.0000   0.0366
  -9.250  -0.7739   0.03303   0.02508  -0.0462   1.0000   0.0386
  -9.000  -0.7626   0.03162   0.02344  -0.0441   1.0000   0.0408
  -8.750  -0.7504   0.03030   0.02182  -0.0419   1.0000   0.0431
  -8.500  -0.7401   0.02898   0.02056  -0.0398   1.0000   0.0457
  -8.250  -0.7284   0.02802   0.01953  -0.0377   1.0000   0.0489
  -8.000  -0.7156   0.02702   0.01834  -0.0355   1.0000   0.0525
  -7.750  -0.6971   0.02578   0.01707  -0.0347   0.9979   0.0567
  -7.500  -0.6649   0.02468   0.01584  -0.0365   0.9923   0.0631
  -7.250  -0.6328   0.02364   0.01478  -0.0383   0.9863   0.0700
  -7.000  -0.6000   0.02284   0.01392  -0.0399   0.9801   0.0785
  -6.750  -0.5653   0.02218   0.01320  -0.0419   0.9745   0.0883
  -6.500  -0.5327   0.02154   0.01252  -0.0434   0.9679   0.0997
  -6.250  -0.4982   0.02086   0.01179  -0.0453   0.9624   0.1137
  -6.000  -0.4663   0.02023   0.01110  -0.0466   0.9557   0.1296
  -5.750  -0.4336   0.01964   0.01045  -0.0480   0.9491   0.1474
  -5.500  -0.4021   0.01907   0.00983  -0.0492   0.9425   0.1635
  -5.250  -0.3720   0.01852   0.00930  -0.0500   0.9350   0.1802
  -5.000  -0.3404   0.01794   0.00881  -0.0512   0.9293   0.2015
  -4.750  -0.3132   0.01743   0.00843  -0.0515   0.9207   0.2321
  -4.500  -0.2823   0.01688   0.00808  -0.0525   0.9150   0.2847
  -4.250  -0.2571   0.01647   0.00787  -0.0522   0.9059   0.3419
  -4.000  -0.2279   0.01609   0.00767  -0.0526   0.9001   0.4020
  -3.750  -0.2021   0.01589   0.00759  -0.0523   0.8917   0.4472
  -3.500  -0.1730   0.01572   0.00744  -0.0524   0.8856   0.4820
  -3.250  -0.1462   0.01563   0.00734  -0.0521   0.8777   0.5099
  -3.000  -0.1177   0.01553   0.00721  -0.0521   0.8713   0.5359
  -2.750  -0.0906   0.01547   0.00715  -0.0519   0.8646   0.5606
  -2.500  -0.0635   0.01539   0.00708  -0.0516   0.8579   0.5879
  -2.250  -0.0359   0.01531   0.00701  -0.0514   0.8521   0.6142
  -2.000  -0.0099   0.01526   0.00700  -0.0509   0.8448   0.6381
  -1.750   0.0182   0.01518   0.00692  -0.0507   0.8399   0.6620
  -1.500   0.0439   0.01516   0.00696  -0.0502   0.8328   0.6859
  -1.250   0.0707   0.01510   0.00695  -0.0496   0.8270   0.7129
  -1.000   0.0970   0.01506   0.00698  -0.0490   0.8215   0.7421
  -0.750   0.1223   0.01505   0.00704  -0.0481   0.8144   0.7718
  -0.500   0.1494   0.01495   0.00698  -0.0473   0.8079   0.7998
  -0.250   0.1755   0.01490   0.00697  -0.0465   0.7979   0.8261
   0.000   0.2037   0.01483   0.00690  -0.0460   0.7889   0.8529
   0.250   0.2346   0.01479   0.00686  -0.0461   0.7809   0.8805
   0.500   0.2690   0.01481   0.00689  -0.0471   0.7737   0.9071
   0.750   0.3060   0.01481   0.00688  -0.0487   0.7664   0.9326
   1.000   0.3456   0.01483   0.00688  -0.0510   0.7592   0.9557
   1.250   0.3867   0.01484   0.00688  -0.0538   0.7512   0.9762
   1.500   0.4299   0.01484   0.00686  -0.0571   0.7431   0.9935
   1.750   0.4620   0.01484   0.00683  -0.0581   0.7344   1.0000
   2.000   0.4842   0.01491   0.00686  -0.0572   0.7251   1.0000
   2.250   0.5082   0.01492   0.00682  -0.0564   0.7166   1.0000
   2.500   0.5306   0.01503   0.00694  -0.0555   0.7056   1.0000
   2.750   0.5543   0.01510   0.00699  -0.0546   0.6951   1.0000
   3.000   0.5790   0.01514   0.00699  -0.0538   0.6846   1.0000
   3.250   0.6024   0.01524   0.00711  -0.0529   0.6712   1.0000
   3.500   0.6261   0.01532   0.00721  -0.0521   0.6571   1.0000
   3.750   0.6502   0.01541   0.00730  -0.0512   0.6420   1.0000
   4.000   0.6743   0.01549   0.00742  -0.0504   0.6260   1.0000
   4.250   0.6986   0.01559   0.00752  -0.0496   0.6088   1.0000
   4.500   0.7223   0.01570   0.00765  -0.0487   0.5885   1.0000
   4.750   0.7458   0.01583   0.00780  -0.0477   0.5650   1.0000
   5.000   0.7689   0.01598   0.00793  -0.0467   0.5375   1.0000
   5.250   0.7917   0.01618   0.00805  -0.0456   0.5057   1.0000
   5.500   0.8136   0.01648   0.00820  -0.0444   0.4718   1.0000
   5.750   0.8347   0.01689   0.00845  -0.0432   0.4405   1.0000
   6.000   0.8556   0.01739   0.00881  -0.0420   0.4121   1.0000
   6.250   0.8765   0.01791   0.00926  -0.0409   0.3873   1.0000
   6.500   0.8973   0.01845   0.00976  -0.0398   0.3644   1.0000
   6.750   0.9181   0.01899   0.01028  -0.0388   0.3420   1.0000
   7.000   0.9383   0.01955   0.01083  -0.0377   0.3200   1.0000
   7.250   0.9580   0.02014   0.01140  -0.0365   0.2985   1.0000
   7.500   0.9768   0.02077   0.01202  -0.0352   0.2751   1.0000
   7.750   0.9944   0.02146   0.01267  -0.0339   0.2505   1.0000
   8.000   1.0104   0.02224   0.01336  -0.0323   0.2253   1.0000
   8.250   1.0260   0.02306   0.01410  -0.0308   0.2004   1.0000
   8.500   1.0410   0.02393   0.01491  -0.0292   0.1786   1.0000
   8.750   1.0558   0.02480   0.01579  -0.0276   0.1600   1.0000
   9.000   1.0694   0.02573   0.01670  -0.0259   0.1429   1.0000
   9.250   1.0814   0.02672   0.01767  -0.0240   0.1268   1.0000
   9.500   1.0908   0.02777   0.01870  -0.0217   0.1122   1.0000
   9.750   1.0996   0.02895   0.01985  -0.0196   0.0988   1.0000
  10.000   1.1066   0.03032   0.02120  -0.0175   0.0868   1.0000
  10.250   1.1138   0.03176   0.02268  -0.0155   0.0762   1.0000
  10.500   1.1203   0.03330   0.02432  -0.0136   0.0672   1.0000
  10.750   1.1253   0.03500   0.02603  -0.0119   0.0602   1.0000
  11.000   1.1325   0.03660   0.02776  -0.0103   0.0541   1.0000
  11.250   1.1366   0.03847   0.02965  -0.0089   0.0500   1.0000
  11.500   1.1421   0.04031   0.03161  -0.0076   0.0461   1.0000
  11.750   1.1450   0.04241   0.03376  -0.0065   0.0433   1.0000
  12.000   1.1461   0.04476   0.03618  -0.0054   0.0412   1.0000
  12.250   1.1490   0.04704   0.03862  -0.0044   0.0390   1.0000
  12.500   1.1508   0.04948   0.04117  -0.0036   0.0370   1.0000
  12.750   1.1506   0.05216   0.04395  -0.0031   0.0354   1.0000
  13.000   1.1481   0.05514   0.04696  -0.0025   0.0340   1.0000
  13.250   1.1500   0.05784   0.04985  -0.0020   0.0329   1.0000
  13.500   1.1507   0.06072   0.05292  -0.0016   0.0317   1.0000
  13.750   1.1502   0.06379   0.05615  -0.0014   0.0306   1.0000
  14.000   1.1485   0.06704   0.05954  -0.0015   0.0296   1.0000
  14.250   1.1457   0.07046   0.06308  -0.0018   0.0287   1.0000
  14.500   1.1426   0.07397   0.06667  -0.0022   0.0279   1.0000
  14.750   1.1401   0.07752   0.07026  -0.0025   0.0271   1.0000
  15.000   1.1336   0.08192   0.07488  -0.0036   0.0265   1.0000
  15.250   1.1256   0.08672   0.07994  -0.0051   0.0261   1.0000
  15.500   1.1161   0.09197   0.08542  -0.0070   0.0257   1.0000
  15.750   1.1048   0.09773   0.09141  -0.0094   0.0254   1.0000
  16.000   1.0914   0.10412   0.09803  -0.0124   0.0252   1.0000
  16.250   1.0758   0.11129   0.10542  -0.0162   0.0251   1.0000
  16.500   1.0574   0.11942   0.11377  -0.0208   0.0250   1.0000
  16.750   1.0353   0.12888   0.12345  -0.0265   0.0251   1.0000
  17.000   1.0078   0.14037   0.13515  -0.0337   0.0254   1.0000
  17.250   0.9694   0.15611   0.15106  -0.0434   0.0259   1.0000
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