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GOE 692 AIRFOIL (goe692-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 692 AIRFOIL (goe692-il)
Reynolds number: 100,000
Max Cl/Cd: 49.64 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe692-il-100000-n5.txt
Download as CSV file: xf-goe692-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 692 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
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.2423   0.09443   0.08886  -0.0853   0.9608   0.0597
 -10.000  -0.2446   0.08723   0.08164  -0.0915   0.9569   0.0599
  -9.500  -0.4207   0.04858   0.04225  -0.1179   0.9210   0.0598
  -9.250  -0.4369   0.04195   0.03481  -0.1190   0.9124   0.0609
  -9.000  -0.4253   0.04001   0.03266  -0.1183   0.9054   0.0620
  -8.750  -0.4044   0.03893   0.03152  -0.1183   0.8996   0.0632
  -8.500  -0.3808   0.03712   0.02948  -0.1193   0.8956   0.0649
  -8.250  -0.3665   0.03520   0.02722  -0.1185   0.8887   0.0667
  -8.000  -0.3499   0.03302   0.02455  -0.1179   0.8824   0.0686
  -7.750  -0.3220   0.03174   0.02317  -0.1187   0.8787   0.0703
  -7.500  -0.2959   0.03085   0.02220  -0.1189   0.8743   0.0723
  -7.250  -0.2776   0.02997   0.02113  -0.1177   0.8667   0.0749
  -7.000  -0.2501   0.02869   0.01954  -0.1182   0.8624   0.0783
  -6.750  -0.2184   0.02790   0.01876  -0.1193   0.8592   0.0812
  -6.500  -0.2006   0.02733   0.01806  -0.1177   0.8512   0.0842
  -6.250  -0.1738   0.02645   0.01697  -0.1178   0.8462   0.0882
  -6.000  -0.1428   0.02586   0.01640  -0.1186   0.8426   0.0923
  -5.750  -0.1187   0.02533   0.01570  -0.1180   0.8365   0.0971
  -5.500  -0.0946   0.02491   0.01528  -0.1175   0.8299   0.1014
  -5.250  -0.0643   0.02442   0.01470  -0.1180   0.8258   0.1072
  -5.000  -0.0316   0.02387   0.01408  -0.1190   0.8227   0.1132
  -4.750  -0.0138   0.02378   0.01397  -0.1173   0.8140   0.1183
  -4.500   0.0152   0.02334   0.01343  -0.1175   0.8091   0.1249
  -4.250   0.0473   0.02293   0.01300  -0.1183   0.8055   0.1318
  -4.000   0.0683   0.02275   0.01274  -0.1171   0.7980   0.1382
  -3.750   0.0949   0.02247   0.01248  -0.1169   0.7923   0.1450
  -3.500   0.1264   0.02205   0.01197  -0.1174   0.7884   0.1538
  -3.250   0.1501   0.02187   0.01182  -0.1168   0.7820   0.1613
  -3.000   0.1748   0.02167   0.01158  -0.1162   0.7756   0.1707
  -2.750   0.2049   0.02134   0.01125  -0.1165   0.7713   0.1813
  -2.500   0.2317   0.02111   0.01102  -0.1163   0.7659   0.1918
  -2.250   0.2541   0.02106   0.01095  -0.1154   0.7588   0.2033
  -2.000   0.2835   0.02076   0.01068  -0.1156   0.7542   0.2159
  -1.750   0.3124   0.02052   0.01045  -0.1157   0.7495   0.2293
  -1.500   0.3331   0.02055   0.01050  -0.1144   0.7419   0.2428
  -1.250   0.3620   0.02030   0.01028  -0.1146   0.7371   0.2597
  -0.750   0.4113   0.02005   0.01023  -0.1135   0.7250   0.3050
  -0.500   0.4396   0.01975   0.01008  -0.1136   0.7202   0.3444
  -0.250   0.4702   0.01929   0.00988  -0.1140   0.7163   0.4153
   0.000   0.4863   0.01912   0.01019  -0.1120   0.7086   0.5281
   0.250   0.5074   0.01854   0.01030  -0.1097   0.7037   0.7296
   0.500   0.5578   0.01822   0.01021  -0.1128   0.7002   0.9183
   0.750   0.6044   0.01845   0.01039  -0.1169   0.6933   0.9897
   1.000   0.6353   0.01852   0.01034  -0.1176   0.6876   1.0000
   1.250   0.6648   0.01847   0.01013  -0.1178   0.6834   1.0000
   1.500   0.6800   0.01879   0.01041  -0.1156   0.6760   1.0000
   1.750   0.7044   0.01889   0.01041  -0.1149   0.6703   1.0000
   2.000   0.7356   0.01885   0.01023  -0.1154   0.6660   1.0000
   2.250   0.7506   0.01923   0.01060  -0.1132   0.6583   1.0000
   2.500   0.7765   0.01933   0.01062  -0.1128   0.6526   1.0000
   2.750   0.8084   0.01931   0.01048  -0.1134   0.6481   1.0000
   3.000   0.8226   0.01974   0.01093  -0.1111   0.6400   1.0000
   3.250   0.8502   0.01983   0.01094  -0.1110   0.6342   1.0000
   3.500   0.8766   0.01997   0.01102  -0.1107   0.6284   1.0000
   3.750   0.8949   0.02031   0.01136  -0.1091   0.6206   1.0000
   4.000   0.9254   0.02032   0.01130  -0.1094   0.6147   1.0000
   4.250   0.9425   0.02067   0.01166  -0.1076   0.6062   1.0000
   4.500   0.9689   0.02074   0.01167  -0.1072   0.5983   1.0000
   4.750   0.9880   0.02101   0.01194  -0.1057   0.5894   1.0000
   5.000   1.0117   0.02115   0.01204  -0.1049   0.5810   1.0000
   5.250   1.0314   0.02143   0.01232  -0.1035   0.5727   1.0000
   5.500   1.0522   0.02168   0.01258  -0.1023   0.5645   1.0000
   5.750   1.0740   0.02192   0.01281  -0.1012   0.5568   1.0000
   6.000   1.0910   0.02227   0.01319  -0.0994   0.5480   1.0000
   6.250   1.1130   0.02250   0.01340  -0.0984   0.5401   1.0000
   6.500   1.1273   0.02287   0.01380  -0.0962   0.5302   1.0000
   6.750   1.1422   0.02319   0.01413  -0.0939   0.5204   1.0000
   7.000   1.1605   0.02338   0.01428  -0.0922   0.5098   1.0000
   7.250   1.1684   0.02392   0.01486  -0.0890   0.4973   1.0000
   7.500   1.1811   0.02435   0.01528  -0.0866   0.4848   1.0000
   7.750   1.1962   0.02473   0.01562  -0.0846   0.4727   1.0000
   8.000   1.2094   0.02524   0.01612  -0.0825   0.4605   1.0000
   8.250   1.2208   0.02592   0.01683  -0.0803   0.4490   1.0000
   8.500   1.2357   0.02649   0.01738  -0.0785   0.4383   1.0000
   8.750   1.2488   0.02716   0.01804  -0.0766   0.4271   1.0000
   9.000   1.2597   0.02798   0.01890  -0.0746   0.4157   1.0000
   9.250   1.2724   0.02873   0.01964  -0.0728   0.4045   1.0000
   9.500   1.2834   0.02959   0.02050  -0.0709   0.3926   1.0000
   9.750   1.2917   0.03066   0.02159  -0.0688   0.3802   1.0000
  10.000   1.3008   0.03170   0.02264  -0.0669   0.3679   1.0000
  10.250   1.3097   0.03279   0.02371  -0.0649   0.3556   1.0000
  10.500   1.3166   0.03405   0.02498  -0.0630   0.3429   1.0000
  10.750   1.3230   0.03541   0.02636  -0.0611   0.3304   1.0000
  11.000   1.3297   0.03677   0.02773  -0.0593   0.3186   1.0000
  11.250   1.3366   0.03815   0.02907  -0.0576   0.3074   1.0000
  11.500   1.3421   0.03971   0.03067  -0.0560   0.2961   1.0000
  11.750   1.3482   0.04125   0.03222  -0.0544   0.2859   1.0000
  12.000   1.3544   0.04279   0.03372  -0.0529   0.2764   1.0000
  12.250   1.3599   0.04449   0.03548  -0.0515   0.2669   1.0000
  12.500   1.3665   0.04606   0.03701  -0.0501   0.2587   1.0000
  12.750   1.3722   0.04784   0.03888  -0.0489   0.2503   1.0000
  13.000   1.3793   0.04944   0.04042  -0.0477   0.2432   1.0000
  13.250   1.3850   0.05131   0.04239  -0.0466   0.2357   1.0000
  13.500   1.3915   0.05304   0.04412  -0.0455   0.2291   1.0000
  13.750   1.3986   0.05478   0.04591  -0.0446   0.2229   1.0000
  14.000   1.4047   0.05668   0.04789  -0.0437   0.2168   1.0000
  14.250   1.4139   0.05819   0.04937  -0.0428   0.2119   1.0000
  14.500   1.4221   0.05993   0.05120  -0.0420   0.2072   1.0000
  14.750   1.4291   0.06182   0.05321  -0.0413   0.2025   1.0000
  15.000   1.4381   0.06345   0.05488  -0.0405   0.1985   1.0000
  15.250   1.4511   0.06461   0.05600  -0.0398   0.1948   1.0000
  15.500   1.4541   0.06703   0.05862  -0.0392   0.1907   1.0000
  15.750   1.4583   0.06928   0.06098  -0.0387   0.1865   1.0000
  16.000   1.4646   0.07122   0.06297  -0.0382   0.1825   1.0000
  16.250   1.4692   0.07339   0.06519  -0.0377   0.1784   1.0000
  16.500   1.4660   0.07662   0.06861  -0.0375   0.1739   1.0000
  16.750   1.4665   0.07934   0.07142  -0.0374   0.1696   1.0000
  17.000   1.4729   0.08123   0.07327  -0.0371   0.1656   1.0000
  17.250   1.4647   0.08530   0.07760  -0.0373   0.1616   1.0000
  17.500   1.4602   0.08885   0.08129  -0.0376   0.1572   1.0000
  17.750   1.4619   0.09146   0.08389  -0.0378   0.1529   1.0000
  18.000   1.4533   0.09574   0.08835  -0.0385   0.1488   1.0000
  18.250   1.4440   0.10021   0.09299  -0.0395   0.1445   1.0000
  18.500   1.4421   0.10349   0.09629  -0.0402   0.1400   1.0000
  18.750   1.4343   0.10787   0.10080  -0.0413   0.1360   1.0000
  19.000   1.4221   0.11308   0.10622  -0.0430   0.1320   1.0000
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