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S1014 (s1014-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S1014 (s1014-il)
Reynolds number: 1,000,000
Max Cl/Cd: 54.89 at α=3.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1014-il-1000000.txt
Download as CSV file: xf-s1014-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1014                                           
  
 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  -1.2261   0.07322   0.06899  -0.0550   0.8872   0.0169
 -19.500  -1.2450   0.06739   0.06298  -0.0573   0.8759   0.0172
 -19.250  -1.2554   0.06289   0.05834  -0.0588   0.8680   0.0174
 -19.000  -1.2629   0.05899   0.05430  -0.0599   0.8612   0.0176
 -18.750  -1.2671   0.05554   0.05075  -0.0607   0.8566   0.0180
 -18.500  -1.2692   0.05248   0.04760  -0.0612   0.8524   0.0183
 -18.250  -1.2681   0.04992   0.04493  -0.0615   0.8484   0.0186
 -18.000  -1.2653   0.04764   0.04255  -0.0615   0.8448   0.0190
 -17.750  -1.2600   0.04563   0.04046  -0.0615   0.8424   0.0194
 -17.500  -1.2557   0.04358   0.03833  -0.0613   0.8399   0.0197
 -17.250  -1.2471   0.04202   0.03668  -0.0610   0.8374   0.0201
 -17.000  -1.2426   0.04015   0.03472  -0.0606   0.8351   0.0203
 -16.750  -1.2451   0.03777   0.03225  -0.0596   0.8328   0.0210
 -16.500  -1.2391   0.03618   0.03060  -0.0589   0.8306   0.0217
 -16.250  -1.2305   0.03484   0.02919  -0.0581   0.8284   0.0222
 -16.000  -1.2195   0.03368   0.02800  -0.0575   0.8271   0.0230
 -15.750  -1.2097   0.03247   0.02672  -0.0567   0.8258   0.0235
 -15.500  -1.1977   0.03144   0.02563  -0.0560   0.8243   0.0240
 -15.250  -1.1909   0.03008   0.02422  -0.0548   0.8229   0.0251
 -15.000  -1.1807   0.02898   0.02309  -0.0538   0.8215   0.0260
 -14.750  -1.1689   0.02802   0.02209  -0.0528   0.8201   0.0268
 -14.500  -1.1552   0.02721   0.02123  -0.0520   0.8188   0.0279
 -14.250  -1.1400   0.02650   0.02046  -0.0512   0.8175   0.0287
 -14.000  -1.1297   0.02549   0.01942  -0.0499   0.8162   0.0300
 -13.750  -1.1168   0.02468   0.01859  -0.0488   0.8149   0.0315
 -13.500  -1.1014   0.02403   0.01790  -0.0479   0.8134   0.0328
 -13.250  -1.0844   0.02348   0.01729  -0.0471   0.8119   0.0338
 -13.000  -1.0717   0.02265   0.01645  -0.0459   0.8111   0.0357
 -12.750  -1.0563   0.02199   0.01580  -0.0449   0.8103   0.0374
 -12.500  -1.0392   0.02144   0.01521  -0.0441   0.8095   0.0389
 -12.250  -1.0208   0.02097   0.01471  -0.0433   0.8087   0.0401
 -12.000  -1.0068   0.02026   0.01400  -0.0421   0.8078   0.0426
 -11.750  -0.9897   0.01972   0.01345  -0.0411   0.8070   0.0445
 -11.500  -0.9709   0.01929   0.01300  -0.0404   0.8061   0.0464
 -11.250  -0.9538   0.01876   0.01246  -0.0394   0.8052   0.0486
 -11.000  -0.9369   0.01823   0.01194  -0.0383   0.8044   0.0512
 -10.750  -0.9182   0.01780   0.01150  -0.0375   0.8035   0.0534
 -10.500  -0.8985   0.01744   0.01110  -0.0367   0.8027   0.0552
 -10.250  -0.8818   0.01692   0.01059  -0.0355   0.8019   0.0588
 -10.000  -0.8630   0.01651   0.01019  -0.0346   0.8012   0.0617
  -9.750  -0.8426   0.01619   0.00984  -0.0339   0.8004   0.0640
  -9.500  -0.8252   0.01572   0.00939  -0.0327   0.7996   0.0683
  -9.250  -0.8062   0.01535   0.00903  -0.0318   0.7989   0.0719
  -9.000  -0.7858   0.01505   0.00871  -0.0310   0.7982   0.0750
  -8.750  -0.7679   0.01464   0.00834  -0.0298   0.7973   0.0807
  -8.500  -0.7481   0.01434   0.00804  -0.0289   0.7965   0.0846
  -8.250  -0.7289   0.01403   0.00775  -0.0279   0.7955   0.0901
  -8.000  -0.7097   0.01369   0.00743  -0.0269   0.7950   0.0957
  -7.750  -0.6898   0.01337   0.00713  -0.0260   0.7944   0.1013
  -7.500  -0.6709   0.01302   0.00682  -0.0248   0.7940   0.1085
  -7.250  -0.6511   0.01273   0.00654  -0.0238   0.7934   0.1153
  -7.000  -0.6323   0.01240   0.00626  -0.0226   0.7929   0.1235
  -6.750  -0.6134   0.01209   0.00599  -0.0214   0.7923   0.1321
  -6.250  -0.5771   0.01147   0.00547  -0.0187   0.7910   0.1536
  -6.000  -0.5604   0.01117   0.00523  -0.0170   0.7903   0.1668
  -5.750  -0.5447   0.01091   0.00504  -0.0150   0.7896   0.1811
  -5.500  -0.5301   0.01069   0.00489  -0.0128   0.7888   0.1974
  -5.250  -0.5139   0.01044   0.00473  -0.0109   0.7881   0.2183
  -5.000  -0.4965   0.01014   0.00455  -0.0092   0.7872   0.2441
  -4.750  -0.4784   0.00983   0.00437  -0.0077   0.7864   0.2736
  -4.500  -0.4615   0.00946   0.00418  -0.0060   0.7857   0.3139
  -4.250  -0.4448   0.00905   0.00398  -0.0042   0.7850   0.3615
  -4.000  -0.4285   0.00859   0.00376  -0.0024   0.7843   0.4194
  -3.750  -0.4134   0.00803   0.00350  -0.0004   0.7836   0.4911
  -3.500  -0.3985   0.00741   0.00323   0.0018   0.7829   0.5740
  -3.250  -0.3816   0.00696   0.00320   0.0037   0.7820   0.6699
  -3.000  -0.3536   0.00703   0.00331   0.0037   0.7813   0.6991
  -2.750  -0.3247   0.00714   0.00341   0.0034   0.7808   0.7116
  -2.500  -0.2956   0.00729   0.00355   0.0031   0.7801   0.7196
  -2.250  -0.2668   0.00748   0.00372   0.0029   0.7790   0.7265
  -2.000  -0.2376   0.00759   0.00382   0.0025   0.7784   0.7315
  -1.750  -0.2078   0.00768   0.00393   0.0021   0.7778   0.7354
  -1.500  -0.1782   0.00778   0.00403   0.0017   0.7770   0.7397
  -1.250  -0.1487   0.00786   0.00410   0.0013   0.7760   0.7434
  -1.000  -0.1194   0.00790   0.00413   0.0009   0.7746   0.7464
  -0.750  -0.0896   0.00792   0.00418   0.0006   0.7729   0.7494
  -0.500  -0.0597   0.00794   0.00421   0.0003   0.7701   0.7527
  -0.250  -0.0295   0.00788   0.00412   0.0001   0.7663   0.7566
   0.000   0.0000   0.00796   0.00414   0.0000   0.7612   0.7612
   0.250   0.0295   0.00788   0.00412  -0.0001   0.7565   0.7663
   0.500   0.0596   0.00794   0.00421  -0.0003   0.7527   0.7701
   0.750   0.0896   0.00792   0.00418  -0.0006   0.7494   0.7730
   1.000   0.1194   0.00790   0.00413  -0.0009   0.7464   0.7746
   1.250   0.1487   0.00786   0.00410  -0.0013   0.7434   0.7760
   1.500   0.1781   0.00778   0.00403  -0.0017   0.7397   0.7770
   1.750   0.2078   0.00768   0.00393  -0.0021   0.7354   0.7778
   2.000   0.2375   0.00759   0.00382  -0.0025   0.7315   0.7784
   2.250   0.2668   0.00748   0.00372  -0.0029   0.7266   0.7790
   2.500   0.2955   0.00729   0.00355  -0.0031   0.7196   0.7801
   2.750   0.3246   0.00714   0.00341  -0.0034   0.7116   0.7808
   3.000   0.3536   0.00703   0.00331  -0.0037   0.6991   0.7813
   3.250   0.3815   0.00695   0.00319  -0.0037   0.6693   0.7820
   3.500   0.3985   0.00741   0.00323  -0.0017   0.5737   0.7829
   3.750   0.4133   0.00804   0.00351   0.0004   0.4905   0.7836
   4.000   0.4283   0.00860   0.00376   0.0024   0.4184   0.7843
   4.250   0.4448   0.00905   0.00398   0.0042   0.3619   0.7850
   4.500   0.4614   0.00946   0.00418   0.0060   0.3134   0.7857
   4.750   0.4784   0.00983   0.00437   0.0077   0.2737   0.7864
   5.000   0.4965   0.01014   0.00455   0.0092   0.2441   0.7872
   5.250   0.5139   0.01044   0.00473   0.0109   0.2184   0.7881
   5.500   0.5302   0.01068   0.00489   0.0128   0.1977   0.7888
   5.750   0.5448   0.01091   0.00504   0.0150   0.1810   0.7896
   6.000   0.5603   0.01117   0.00523   0.0170   0.1665   0.7903
   6.250   0.5772   0.01147   0.00547   0.0187   0.1537   0.7910
   6.750   0.6137   0.01208   0.00599   0.0214   0.1328   0.7923
   7.000   0.6324   0.01240   0.00626   0.0226   0.1237   0.7929
   7.250   0.6512   0.01272   0.00654   0.0238   0.1154   0.7934
   7.500   0.6710   0.01302   0.00682   0.0248   0.1085   0.7940
   7.750   0.6898   0.01337   0.00712   0.0259   0.1013   0.7945
   8.000   0.7098   0.01368   0.00743   0.0269   0.0959   0.7950
   8.250   0.7291   0.01403   0.00774   0.0279   0.0903   0.7955
   8.500   0.7482   0.01434   0.00804   0.0289   0.0847   0.7965
   8.750   0.7681   0.01464   0.00833   0.0298   0.0806   0.7973
   9.000   0.7860   0.01504   0.00870   0.0310   0.0750   0.7982
   9.250   0.8064   0.01534   0.00902   0.0317   0.0719   0.7989
   9.500   0.8254   0.01572   0.00939   0.0327   0.0683   0.7996
   9.750   0.8430   0.01618   0.00983   0.0338   0.0639   0.8004
  10.000   0.8634   0.01649   0.01017   0.0346   0.0618   0.8012
  10.250   0.8821   0.01691   0.01059   0.0355   0.0588   0.8019
  10.500   0.8988   0.01743   0.01109   0.0367   0.0551   0.8028
  10.750   0.9185   0.01780   0.01149   0.0374   0.0534   0.8036
  11.000   0.9372   0.01822   0.01193   0.0383   0.0511   0.8044
  11.250   0.9542   0.01875   0.01244   0.0393   0.0487   0.8052
  11.500   0.9712   0.01928   0.01299   0.0403   0.0464   0.8061
  11.750   0.9900   0.01971   0.01345   0.0411   0.0447   0.8070
  12.000   1.0071   0.02025   0.01399   0.0420   0.0425   0.8078
  12.250   1.0214   0.02095   0.01468   0.0433   0.0400   0.8087
  12.500   1.0396   0.02143   0.01521   0.0440   0.0389   0.8095
  12.750   1.0567   0.02198   0.01578   0.0449   0.0372   0.8103
  13.000   1.0721   0.02265   0.01644   0.0459   0.0355   0.8112
  13.250   1.0850   0.02347   0.01727   0.0471   0.0339   0.8119
  13.500   1.1020   0.02401   0.01787   0.0478   0.0326   0.8134
  13.750   1.1177   0.02464   0.01854   0.0487   0.0314   0.8149
  14.000   1.1304   0.02546   0.01938   0.0498   0.0300   0.8162
  14.250   1.1408   0.02646   0.02042   0.0511   0.0286   0.8176
  14.500   1.1558   0.02719   0.02120   0.0519   0.0279   0.8189
  14.750   1.1693   0.02801   0.02208   0.0528   0.0270   0.8202
  15.000   1.1814   0.02895   0.02306   0.0537   0.0261   0.8215
  15.250   1.1915   0.03006   0.02419   0.0547   0.0250   0.8230
  15.500   1.1974   0.03148   0.02567   0.0560   0.0241   0.8244
  15.750   1.2106   0.03243   0.02668   0.0566   0.0236   0.8258
  16.000   1.2216   0.03354   0.02785   0.0574   0.0230   0.8272
  16.250   1.2314   0.03479   0.02915   0.0581   0.0222   0.8284
  16.500   1.2394   0.03617   0.03060   0.0588   0.0217   0.8308
  16.750   1.2463   0.03769   0.03218   0.0595   0.0212   0.8330
  17.000   1.2471   0.03978   0.03434   0.0604   0.0205   0.8352
  17.250   1.2514   0.04165   0.03630   0.0609   0.0199   0.8376
  17.500   1.2587   0.04333   0.03806   0.0612   0.0197   0.8400
  17.750   1.2629   0.04537   0.04019   0.0614   0.0193   0.8426
  18.000   1.2676   0.04744   0.04234   0.0614   0.0189   0.8450
  18.250   1.2691   0.04985   0.04485   0.0614   0.0186   0.8487
  18.500   1.2705   0.05236   0.04747   0.0612   0.0183   0.8527
  18.750   1.2683   0.05542   0.05063   0.0607   0.0179   0.8571
  19.000   1.2653   0.05870   0.05401   0.0599   0.0177   0.8619
  19.250   1.2577   0.06262   0.05807   0.0589   0.0174   0.8689
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