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GOE 770 AIRFOIL (goe770-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 770 AIRFOIL (goe770-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.65 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe770-il-1000000.txt
Download as CSV file: xf-goe770-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 770 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1454   0.08038   0.07652  -0.0479   1.0000   0.0274
 -19.500  -1.1502   0.07623   0.07229  -0.0499   1.0000   0.0276
 -19.250  -1.1542   0.07226   0.06825  -0.0518   1.0000   0.0278
 -19.000  -1.1574   0.06845   0.06437  -0.0535   1.0000   0.0280
 -18.750  -1.1597   0.06482   0.06067  -0.0550   1.0000   0.0282
 -18.500  -1.1611   0.06142   0.05720  -0.0564   1.0000   0.0284
 -18.250  -1.1613   0.05824   0.05395  -0.0576   1.0000   0.0286
 -18.000  -1.1608   0.05521   0.05084  -0.0587   1.0000   0.0288
 -17.750  -1.1596   0.05231   0.04787  -0.0597   1.0000   0.0291
 -17.500  -1.1571   0.04963   0.04511  -0.0605   1.0000   0.0293
 -17.250  -1.1530   0.04719   0.04259  -0.0612   1.0000   0.0294
 -17.000  -1.1469   0.04497   0.04030  -0.0618   1.0000   0.0296
 -16.750  -1.1503   0.04198   0.03725  -0.0623   1.0000   0.0300
 -16.500  -1.1501   0.03931   0.03454  -0.0628   1.0000   0.0303
 -16.250  -1.1458   0.03704   0.03224  -0.0632   1.0000   0.0306
 -16.000  -1.1390   0.03504   0.03019  -0.0635   1.0000   0.0309
 -15.750  -1.1305   0.03320   0.02831  -0.0637   1.0000   0.0312
 -15.500  -1.1209   0.03149   0.02657  -0.0639   1.0000   0.0315
 -15.250  -1.1105   0.02991   0.02494  -0.0639   1.0000   0.0318
 -15.000  -1.0991   0.02843   0.02342  -0.0639   1.0000   0.0322
 -14.750  -1.0870   0.02707   0.02201  -0.0638   1.0000   0.0325
 -14.500  -1.0699   0.02585   0.02072  -0.0644   0.9567   0.0329
 -14.250  -1.0623   0.02511   0.01959  -0.0623   0.8401   0.0332
 -14.000  -1.0476   0.02436   0.01860  -0.0615   0.7895   0.0335
 -13.750  -1.0410   0.02294   0.01701  -0.0605   0.7530   0.0340
 -13.500  -1.0297   0.02193   0.01586  -0.0596   0.7221   0.0345
 -13.250  -1.0153   0.02113   0.01495  -0.0586   0.6974   0.0349
 -13.000  -0.9994   0.02046   0.01418  -0.0576   0.6784   0.0354
 -12.750  -0.9826   0.01985   0.01348  -0.0566   0.6642   0.0359
 -12.500  -0.9651   0.01929   0.01284  -0.0555   0.6533   0.0364
 -12.250  -0.9469   0.01879   0.01226  -0.0544   0.6436   0.0369
 -12.000  -0.9279   0.01837   0.01177  -0.0532   0.6353   0.0373
 -11.750  -0.9123   0.01792   0.01126  -0.0514   0.6289   0.0379
 -11.500  -0.8967   0.01734   0.01064  -0.0497   0.6223   0.0387
 -11.250  -0.8763   0.01693   0.01018  -0.0487   0.6153   0.0394
 -11.000  -0.8542   0.01655   0.00978  -0.0478   0.6107   0.0401
 -10.750  -0.8314   0.01621   0.00940  -0.0471   0.6055   0.0409
 -10.500  -0.8079   0.01591   0.00904  -0.0464   0.6003   0.0416
 -10.250  -0.7847   0.01560   0.00866  -0.0456   0.5945   0.0424
 -10.000  -0.7626   0.01514   0.00821  -0.0448   0.5916   0.0435
  -9.750  -0.7382   0.01482   0.00788  -0.0442   0.5879   0.0447
  -9.500  -0.7130   0.01457   0.00759  -0.0437   0.5837   0.0459
  -9.250  -0.6873   0.01436   0.00733  -0.0433   0.5793   0.0469
  -9.000  -0.6639   0.01400   0.00694  -0.0426   0.5740   0.0486
  -8.750  -0.6382   0.01372   0.00667  -0.0421   0.5715   0.0502
  -8.500  -0.6118   0.01350   0.00642  -0.0418   0.5686   0.0518
  -8.250  -0.5864   0.01319   0.00612  -0.0413   0.5652   0.0539
  -8.000  -0.5601   0.01296   0.00588  -0.0410   0.5616   0.0562
  -7.750  -0.5337   0.01276   0.00565  -0.0407   0.5576   0.0588
  -7.500  -0.5075   0.01257   0.00544  -0.0403   0.5531   0.0618
  -7.250  -0.4803   0.01236   0.00523  -0.0401   0.5510   0.0647
  -7.000  -0.4534   0.01212   0.00503  -0.0399   0.5483   0.0683
  -6.750  -0.4260   0.01194   0.00484  -0.0397   0.5451   0.0719
  -6.500  -0.3987   0.01175   0.00466  -0.0395   0.5414   0.0761
  -6.250  -0.3714   0.01160   0.00448  -0.0393   0.5371   0.0803
  -6.000  -0.3440   0.01147   0.00435  -0.0392   0.5326   0.0850
  -5.750  -0.3163   0.01127   0.00417  -0.0390   0.5303   0.0900
  -5.500  -0.2881   0.01112   0.00403  -0.0390   0.5275   0.0948
  -5.250  -0.2606   0.01093   0.00386  -0.0388   0.5246   0.1009
  -5.000  -0.2327   0.01078   0.00371  -0.0388   0.5216   0.1073
  -4.750  -0.2052   0.01061   0.00355  -0.0386   0.5181   0.1158
  -4.500  -0.1787   0.01040   0.00339  -0.0384   0.5139   0.1316
  -4.250  -0.1550   0.00980   0.00310  -0.0378   0.5119   0.1969
  -4.000  -0.1288   0.00945   0.00297  -0.0375   0.5097   0.2507
  -3.750  -0.1006   0.00928   0.00288  -0.0375   0.5070   0.2734
  -3.500  -0.0720   0.00916   0.00280  -0.0376   0.5041   0.2900
  -3.250  -0.0438   0.00904   0.00271  -0.0376   0.5008   0.3072
  -3.000  -0.0160   0.00891   0.00262  -0.0375   0.4971   0.3264
  -2.750   0.0111   0.00870   0.00252  -0.0374   0.4937   0.3581
  -2.500   0.0368   0.00830   0.00244  -0.0371   0.4916   0.4388
  -2.250   0.0655   0.00820   0.00243  -0.0371   0.4889   0.4703
  -2.000   0.0948   0.00816   0.00242  -0.0373   0.4859   0.4882
  -1.750   0.1243   0.00817   0.00241  -0.0375   0.4826   0.5024
  -1.500   0.1531   0.00816   0.00242  -0.0376   0.4790   0.5139
  -1.250   0.1826   0.00821   0.00243  -0.0378   0.4752   0.5219
  -1.000   0.2122   0.00817   0.00243  -0.0380   0.4725   0.5303
  -0.750   0.2418   0.00816   0.00243  -0.0383   0.4691   0.5385
  -0.500   0.2716   0.00820   0.00243  -0.0385   0.4655   0.5446
  -0.250   0.3006   0.00820   0.00244  -0.0387   0.4617   0.5514
   0.000   0.3295   0.00826   0.00247  -0.0388   0.4574   0.5583
   0.250   0.3595   0.00827   0.00249  -0.0392   0.4546   0.5646
   0.500   0.3888   0.00825   0.00250  -0.0394   0.4510   0.5726
   0.750   0.4181   0.00827   0.00252  -0.0396   0.4468   0.5788
   1.000   0.4471   0.00833   0.00255  -0.0398   0.4422   0.5833
   1.250   0.4766   0.00839   0.00258  -0.0401   0.4381   0.5870
   1.500   0.5059   0.00838   0.00261  -0.0404   0.4338   0.5931
   1.750   0.5348   0.00842   0.00264  -0.0406   0.4287   0.5988
   2.000   0.5633   0.00850   0.00270  -0.0407   0.4232   0.6047
   2.250   0.5926   0.00853   0.00274  -0.0410   0.4191   0.6114
   2.500   0.6214   0.00856   0.00280  -0.0412   0.4140   0.6198
   2.750   0.6498   0.00864   0.00286  -0.0414   0.4084   0.6278
   3.000   0.6781   0.00871   0.00294  -0.0415   0.4032   0.6366
   3.250   0.7067   0.00874   0.00301  -0.0417   0.3982   0.6470
   3.500   0.7346   0.00883   0.00310  -0.0418   0.3925   0.6579
   3.750   0.7622   0.00892   0.00321  -0.0419   0.3870   0.6712
   4.000   0.7903   0.00895   0.00330  -0.0420   0.3824   0.6877
   4.250   0.8175   0.00902   0.00342  -0.0420   0.3772   0.7078
   4.500   0.8438   0.00914   0.00357  -0.0418   0.3713   0.7303
   4.750   0.8713   0.00916   0.00368  -0.0419   0.3676   0.7557
   5.250   0.9232   0.00928   0.00399  -0.0413   0.3588   0.8229
   5.500   0.9476   0.00939   0.00419  -0.0407   0.3543   0.8586
   5.750   0.9736   0.00943   0.00434  -0.0404   0.3518   0.8915
   6.000   0.9991   0.00951   0.00451  -0.0399   0.3487   0.9227
   6.250   1.0276   0.00966   0.00471  -0.0402   0.3454   0.9508
   6.500   1.0607   0.00990   0.00493  -0.0415   0.3417   0.9693
   6.750   1.0944   0.01017   0.00518  -0.0431   0.3376   0.9816
   7.000   1.1310   0.01032   0.00535  -0.0452   0.3351   0.9896
   7.250   1.1686   0.01050   0.00554  -0.0475   0.3317   0.9941
   7.500   1.2062   0.01074   0.00576  -0.0500   0.3282   0.9977
   7.750   1.2376   0.01101   0.00601  -0.0512   0.3246   1.0000
   8.000   1.2544   0.01126   0.00623  -0.0494   0.3214   1.0000
   8.250   1.2756   0.01137   0.00638  -0.0483   0.3196   1.0000
   8.500   1.2965   0.01151   0.00654  -0.0472   0.3173   1.0000
   8.750   1.3169   0.01169   0.00673  -0.0461   0.3144   1.0000
   9.000   1.3364   0.01193   0.00696  -0.0449   0.3110   1.0000
   9.250   1.3542   0.01226   0.00726  -0.0435   0.3071   1.0000
   9.500   1.3748   0.01250   0.00752  -0.0425   0.3047   1.0000
   9.750   1.3964   0.01267   0.00773  -0.0417   0.3027   1.0000
  10.000   1.4166   0.01288   0.00797  -0.0407   0.3004   1.0000
  10.250   1.4356   0.01315   0.00826  -0.0396   0.2979   1.0000
  10.500   1.4537   0.01349   0.00861  -0.0384   0.2952   1.0000
  10.750   1.4698   0.01394   0.00906  -0.0370   0.2919   1.0000
  11.000   1.4877   0.01436   0.00950  -0.0360   0.2888   1.0000
  11.250   1.5093   0.01465   0.00984  -0.0356   0.2865   1.0000
  11.500   1.5292   0.01503   0.01025  -0.0350   0.2839   1.0000
  11.750   1.5471   0.01553   0.01077  -0.0342   0.2809   1.0000
  12.000   1.5620   0.01621   0.01146  -0.0333   0.2772   1.0000
  12.250   1.5766   0.01696   0.01222  -0.0324   0.2736   1.0000
  12.500   1.5966   0.01745   0.01277  -0.0321   0.2709   1.0000
  12.750   1.6135   0.01815   0.01351  -0.0317   0.2668   1.0000
  13.000   1.6254   0.01922   0.01458  -0.0310   0.2620   1.0000
  13.250   1.6383   0.02028   0.01567  -0.0304   0.2575   1.0000
  13.500   1.6531   0.02125   0.01668  -0.0301   0.2525   1.0000
  13.750   1.6595   0.02291   0.01834  -0.0295   0.2460   1.0000
  14.000   1.6697   0.02432   0.01979  -0.0291   0.2397   1.0000
  14.250   1.6716   0.02646   0.02192  -0.0286   0.2315   1.0000
  14.500   1.6753   0.02849   0.02397  -0.0281   0.2234   1.0000
  14.750   1.6691   0.03142   0.02689  -0.0274   0.2139   1.0000
  15.000   1.6572   0.03484   0.03030  -0.0265   0.2027   1.0000
  15.250   1.6426   0.03850   0.03396  -0.0256   0.1917   1.0000
  15.500   1.6267   0.04238   0.03784  -0.0248   0.1821   1.0000
  15.750   1.6104   0.04640   0.04186  -0.0241   0.1741   1.0000
  16.000   1.5965   0.05031   0.04578  -0.0237   0.1666   1.0000
  16.250   1.5859   0.05394   0.04943  -0.0234   0.1607   1.0000
  16.500   1.5739   0.05785   0.05336  -0.0232   0.1550   1.0000
  16.750   1.5639   0.06160   0.05714  -0.0232   0.1500   1.0000
  17.000   1.5574   0.06498   0.06056  -0.0232   0.1448   1.0000
  17.250   1.5431   0.06934   0.06494  -0.0233   0.1400   1.0000
  17.500   1.5388   0.07262   0.06826  -0.0235   0.1353   1.0000
  17.750   1.5263   0.07684   0.07250  -0.0237   0.1301   1.0000
  18.000   1.5172   0.08078   0.07648  -0.0241   0.1251   1.0000
  18.250   1.5044   0.08519   0.08091  -0.0246   0.1193   1.0000
  18.500   1.4938   0.08939   0.08513  -0.0251   0.1134   1.0000
  18.750   1.4768   0.09443   0.09019  -0.0259   0.1072   1.0000
  19.000   1.4621   0.09928   0.09504  -0.0267   0.0999   1.0000
  19.250   1.4460   0.10436   0.10012  -0.0277   0.0918   1.0000
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