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GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 776 AIRFOIL (goe776-il)
Reynolds number: 100,000
Max Cl/Cd: 28.8 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe776-il-100000-n5.txt
Download as CSV file: xf-goe776-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 776 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8674   0.09284   0.08468  -0.0523   1.0000   0.1569
 -16.500  -0.9122   0.08366   0.07526  -0.0554   1.0000   0.1611
 -16.250  -0.8962   0.08289   0.07455  -0.0553   1.0000   0.1637
 -16.000  -0.9084   0.07843   0.07001  -0.0564   1.0000   0.1672
 -15.750  -0.9457   0.07101   0.06230  -0.0583   1.0000   0.1713
 -15.500  -0.9385   0.06922   0.06054  -0.0583   1.0000   0.1742
 -15.250  -0.9322   0.06736   0.05871  -0.0583   1.0000   0.1773
 -15.000  -0.9402   0.06392   0.05517  -0.0586   1.0000   0.1810
 -14.750  -0.9599   0.05936   0.05040  -0.0589   1.0000   0.1849
 -14.500  -0.9475   0.05832   0.04944  -0.0585   1.0000   0.1879
 -14.250  -0.9437   0.05645   0.04758  -0.0581   1.0000   0.1914
 -14.000  -0.9489   0.05378   0.04482  -0.0576   1.0000   0.1954
 -13.750  -0.9578   0.05091   0.04180  -0.0568   1.0000   0.1994
 -13.500  -0.9473   0.04990   0.04089  -0.0560   1.0000   0.2027
 -13.250  -0.9451   0.04827   0.03924  -0.0550   1.0000   0.2065
 -13.000  -0.9494   0.04622   0.03711  -0.0536   1.0000   0.2108
 -12.750  -0.9514   0.04449   0.03532  -0.0519   1.0000   0.2147
 -12.500  -0.9455   0.04348   0.03438  -0.0503   1.0000   0.2183
 -12.250  -0.9460   0.04216   0.03305  -0.0483   1.0000   0.2223
 -12.000  -0.9514   0.04067   0.03148  -0.0457   1.0000   0.2268
 -11.750  -0.9525   0.03955   0.03036  -0.0431   1.0000   0.2307
 -11.500  -0.9513   0.03872   0.02959  -0.0404   1.0000   0.2344
 -11.250  -0.9554   0.03777   0.02863  -0.0372   1.0000   0.2385
 -11.000  -0.9635   0.03677   0.02757  -0.0333   1.0000   0.2429
 -10.750  -0.9689   0.03602   0.02682  -0.0294   1.0000   0.2467
 -10.500  -0.9735   0.03544   0.02631  -0.0253   1.0000   0.2503
 -10.250  -0.9826   0.03483   0.02569  -0.0207   1.0000   0.2543
 -10.000  -0.9703   0.03389   0.02465  -0.0200   0.9958   0.2603
  -9.750  -0.9424   0.03315   0.02396  -0.0217   0.9906   0.2661
  -9.500  -0.9187   0.03233   0.02313  -0.0225   0.9831   0.2727
  -9.250  -0.8928   0.03150   0.02220  -0.0238   0.9768   0.2798
  -9.000  -0.8676   0.03090   0.02168  -0.0245   0.9690   0.2857
  -8.750  -0.8413   0.03019   0.02091  -0.0255   0.9619   0.2932
  -8.500  -0.8160   0.02956   0.02028  -0.0261   0.9541   0.2999
  -8.250  -0.7896   0.02900   0.01975  -0.0267   0.9460   0.3067
  -8.000  -0.7610   0.02829   0.01893  -0.0279   0.9399   0.3151
  -7.750  -0.7404   0.02788   0.01862  -0.0270   0.9286   0.3210
  -7.500  -0.7115   0.02729   0.01800  -0.0278   0.9218   0.3290
  -7.250  -0.6968   0.02684   0.01752  -0.0259   0.9092   0.3359
  -7.000  -0.6668   0.02635   0.01709  -0.0266   0.9019   0.3432
  -6.750  -0.6511   0.02595   0.01663  -0.0247   0.8895   0.3508
  -6.500  -0.6230   0.02547   0.01618  -0.0249   0.8811   0.3581
  -6.250  -0.6028   0.02513   0.01585  -0.0236   0.8699   0.3654
  -6.000  -0.5817   0.02467   0.01528  -0.0225   0.8595   0.3738
  -5.750  -0.5554   0.02434   0.01505  -0.0222   0.8497   0.3806
  -5.500  -0.5345   0.02400   0.01468  -0.0210   0.8382   0.3885
  -5.250  -0.5097   0.02361   0.01424  -0.0204   0.8289   0.3965
  -5.000  -0.4882   0.02337   0.01406  -0.0191   0.8165   0.4037
  -4.750  -0.4621   0.02298   0.01358  -0.0187   0.8080   0.4126
  -4.500  -0.4425   0.02278   0.01343  -0.0172   0.7947   0.4197
  -4.250  -0.4146   0.02245   0.01309  -0.0170   0.7857   0.4281
  -4.000  -0.3979   0.02227   0.01282  -0.0150   0.7726   0.4368
  -3.750  -0.3684   0.02199   0.01261  -0.0150   0.7630   0.4443
  -3.500  -0.3484   0.02184   0.01244  -0.0135   0.7506   0.4530
  -3.250  -0.3230   0.02159   0.01216  -0.0129   0.7403   0.4616
  -3.000  -0.2999   0.02146   0.01207  -0.0119   0.7285   0.4698
  -2.750  -0.2773   0.02126   0.01177  -0.0107   0.7176   0.4796
  -2.500  -0.2520   0.02114   0.01172  -0.0101   0.7065   0.4876
  -2.250  -0.2289   0.02101   0.01155  -0.0090   0.6952   0.4971
  -2.000  -0.2047   0.02088   0.01140  -0.0082   0.6845   0.5063
  -1.750  -0.1811   0.02080   0.01135  -0.0072   0.6730   0.5154
  -1.500  -0.1574   0.02067   0.01113  -0.0063   0.6631   0.5258
  -1.250  -0.1335   0.02064   0.01119  -0.0054   0.6510   0.5345
  -1.000  -0.1084   0.02053   0.01097  -0.0047   0.6418   0.5454
  -0.750  -0.0860   0.02053   0.01106  -0.0035   0.6297   0.5543
  -0.500  -0.0608   0.02047   0.01094  -0.0028   0.6198   0.5650
  -0.250  -0.0386   0.02046   0.01096  -0.0016   0.6087   0.5748
   0.000  -0.0134   0.02045   0.01094  -0.0009   0.5985   0.5850
   0.250   0.0088   0.02043   0.01090   0.0002   0.5882   0.5960
   0.500   0.0340   0.02046   0.01098   0.0010   0.5775   0.6057
   0.750   0.0567   0.02045   0.01087   0.0021   0.5683   0.6175
   1.000   0.0815   0.02052   0.01106   0.0028   0.5572   0.6268
   1.250   0.1060   0.02053   0.01097   0.0037   0.5484   0.6386
   1.500   0.1291   0.02062   0.01116   0.0047   0.5376   0.6484
   1.750   0.1532   0.02067   0.01118   0.0056   0.5283   0.6599
   2.000   0.1768   0.02077   0.01130   0.0065   0.5186   0.6705
   2.250   0.2006   0.02087   0.01142   0.0074   0.5090   0.6815
   2.500   0.2248   0.02095   0.01146   0.0083   0.5004   0.6929
   2.750   0.2482   0.02112   0.01171   0.0093   0.4904   0.7037
   3.000   0.2717   0.02120   0.01172   0.0102   0.4823   0.7155
   3.250   0.2964   0.02142   0.01202   0.0110   0.4729   0.7258
   3.500   0.3171   0.02153   0.01211   0.0124   0.4643   0.7385
   3.750   0.3453   0.02178   0.01236   0.0126   0.4562   0.7481
   4.000   0.3630   0.02192   0.01254   0.0145   0.4473   0.7613
   4.250   0.3924   0.02220   0.01280   0.0144   0.4392   0.7705
   4.500   0.4115   0.02240   0.01302   0.0161   0.4312   0.7834
   4.750   0.4377   0.02271   0.01338   0.0165   0.4224   0.7927
   5.000   0.4616   0.02294   0.01351   0.0174   0.4155   0.8049
   5.250   0.4839   0.02328   0.01397   0.0184   0.4067   0.8147
   5.500   0.5065   0.02357   0.01423   0.0195   0.3990   0.8263
   5.750   0.5308   0.02389   0.01454   0.0202   0.3917   0.8366
   6.000   0.5529   0.02428   0.01499   0.0212   0.3833   0.8472
   6.250   0.5752   0.02457   0.01523   0.0222   0.3763   0.8584
   6.500   0.6005   0.02503   0.01573   0.0225   0.3684   0.8677
   6.750   0.6179   0.02537   0.01609   0.0243   0.3609   0.8800
   7.000   0.6494   0.02582   0.01644   0.0236   0.3538   0.8876
   7.250   0.6626   0.02622   0.01695   0.0259   0.3463   0.9008
   7.500   0.6921   0.02674   0.01746   0.0253   0.3385   0.9079
   7.750   0.7083   0.02712   0.01780   0.0271   0.3323   0.9208
   8.000   0.7371   0.02775   0.01850   0.0262   0.3239   0.9273
   8.250   0.7597   0.02820   0.01889   0.0267   0.3174   0.9376
   8.500   0.7864   0.02883   0.01956   0.0260   0.3098   0.9450
   8.750   0.8132   0.02943   0.02018   0.0252   0.3024   0.9527
   9.000   0.8391   0.02997   0.02063   0.0247   0.2963   0.9610
   9.250   0.8654   0.03072   0.02150   0.0236   0.2885   0.9678
   9.500   0.8886   0.03136   0.02210   0.0232   0.2822   0.9763
   9.750   0.9172   0.03209   0.02285   0.0216   0.2756   0.9820
  10.000   0.9404   0.03294   0.02376   0.0208   0.2687   0.9897
  10.250   0.9684   0.03363   0.02438   0.0192   0.2628   0.9950
  10.500   0.9858   0.03459   0.02543   0.0190   0.2567   1.0000
  10.750   0.9757   0.03521   0.02608   0.0238   0.2526   1.0000
  11.000   0.9692   0.03583   0.02666   0.0281   0.2487   1.0000
  11.250   0.9681   0.03639   0.02712   0.0316   0.2452   1.0000
  11.500   0.9584   0.03741   0.02824   0.0357   0.2409   1.0000
  11.750   0.9530   0.03841   0.02927   0.0392   0.2366   1.0000
  12.000   0.9520   0.03933   0.03017   0.0420   0.2326   1.0000
  12.250   0.9566   0.04011   0.03085   0.0443   0.2290   1.0000
  12.500   0.9493   0.04168   0.03254   0.0471   0.2246   1.0000
  12.750   0.9470   0.04309   0.03399   0.0493   0.2203   1.0000
  13.000   0.9501   0.04428   0.03515   0.0510   0.2165   1.0000
  13.250   0.9553   0.04547   0.03629   0.0524   0.2128   1.0000
  13.500   0.9488   0.04766   0.03861   0.0539   0.2085   1.0000
  13.750   0.9485   0.04950   0.04049   0.0550   0.2045   1.0000
  14.000   0.9552   0.05082   0.04176   0.0559   0.2009   1.0000
  14.250   0.9561   0.05280   0.04377   0.0566   0.1973   1.0000
  14.500   0.9479   0.05573   0.04684   0.0571   0.1932   1.0000
  14.750   0.9484   0.05793   0.04906   0.0575   0.1895   1.0000
  15.000   0.9589   0.05916   0.05022   0.0579   0.1863   1.0000
  15.250   0.9494   0.06259   0.05378   0.0578   0.1827   1.0000
  15.500   0.9369   0.06652   0.05785   0.0575   0.1789   1.0000
  15.750   0.9385   0.06894   0.06028   0.0573   0.1755   1.0000
  16.000   0.9543   0.06971   0.06095   0.0576   0.1728   1.0000
  16.250   0.9229   0.07630   0.06780   0.0560   0.1689   1.0000
  16.500   0.9009   0.08202   0.07367   0.0545   0.1650   1.0000
  16.750   0.9100   0.08371   0.07533   0.0543   0.1621   1.0000
  17.000   0.9313   0.08379   0.07530   0.0546   0.1599   1.0000
  17.250   0.7957   0.10640   0.09852   0.0462   0.1514   1.0000
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