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S1014 (s1014-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S1014 (s1014-il)
Reynolds number: 500,000
Max Cl/Cd: 42.04 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1014-il-500000-n5.txt
Download as CSV file: xf-s1014-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1180   0.09134   0.08685  -0.0455   0.8714   0.0177
 -19.500  -1.1328   0.08512   0.08047  -0.0488   0.8664   0.0180
 -19.000  -1.1549   0.07452   0.06956  -0.0540   0.8579   0.0183
 -18.750  -1.1619   0.07006   0.06497  -0.0560   0.8540   0.0187
 -18.500  -1.1689   0.06579   0.06055  -0.0577   0.8504   0.0189
 -18.250  -1.1716   0.06228   0.05690  -0.0588   0.8469   0.0192
 -18.000  -1.1742   0.05890   0.05339  -0.0598   0.8440   0.0196
 -17.750  -1.1743   0.05592   0.05028  -0.0605   0.8411   0.0199
 -17.500  -1.1739   0.05311   0.04737  -0.0610   0.8382   0.0204
 -17.250  -1.1747   0.05031   0.04447  -0.0612   0.8355   0.0208
 -17.000  -1.1732   0.04787   0.04194  -0.0612   0.8329   0.0213
 -16.750  -1.1702   0.04568   0.03965  -0.0611   0.8306   0.0219
 -16.250  -1.1597   0.04191   0.03569  -0.0604   0.8270   0.0229
 -16.000  -1.1526   0.04027   0.03396  -0.0600   0.8252   0.0235
 -15.750  -1.1442   0.03879   0.03238  -0.0594   0.8235   0.0242
 -15.500  -1.1384   0.03715   0.03070  -0.0587   0.8218   0.0251
 -15.250  -1.1298   0.03577   0.02926  -0.0580   0.8202   0.0259
 -15.000  -1.1207   0.03448   0.02790  -0.0572   0.8186   0.0266
 -14.750  -1.1099   0.03335   0.02669  -0.0564   0.8171   0.0276
 -14.500  -1.0982   0.03231   0.02556  -0.0556   0.8157   0.0286
 -14.250  -1.0880   0.03118   0.02438  -0.0546   0.8144   0.0296
 -14.000  -1.0762   0.03019   0.02334  -0.0537   0.8132   0.0306
 -13.750  -1.0639   0.02926   0.02234  -0.0528   0.8119   0.0318
 -13.500  -1.0501   0.02841   0.02144  -0.0519   0.8109   0.0330
 -13.250  -1.0355   0.02762   0.02059  -0.0511   0.8099   0.0341
 -13.000  -1.0225   0.02675   0.01971  -0.0501   0.8088   0.0359
 -12.750  -1.0077   0.02600   0.01893  -0.0492   0.8077   0.0375
 -12.500  -0.9921   0.02531   0.01819  -0.0483   0.8067   0.0390
 -12.250  -0.9763   0.02464   0.01747  -0.0474   0.8056   0.0406
 -12.000  -0.9613   0.02394   0.01675  -0.0465   0.8046   0.0424
 -11.750  -0.9448   0.02332   0.01611  -0.0456   0.8035   0.0443
 -11.500  -0.9277   0.02275   0.01549  -0.0447   0.8024   0.0463
 -11.250  -0.9111   0.02215   0.01487  -0.0438   0.8012   0.0485
 -11.000  -0.8944   0.02158   0.01429  -0.0428   0.8002   0.0509
 -10.750  -0.8765   0.02108   0.01375  -0.0419   0.7992   0.0532
 -10.500  -0.8583   0.02059   0.01322  -0.0411   0.7984   0.0555
 -10.250  -0.8411   0.02006   0.01269  -0.0401   0.7976   0.0586
 -10.000  -0.8227   0.01961   0.01221  -0.0392   0.7967   0.0617
  -9.750  -0.8038   0.01918   0.01176  -0.0384   0.7959   0.0648
  -9.500  -0.7858   0.01871   0.01129  -0.0374   0.7952   0.0683
  -9.250  -0.7667   0.01828   0.01087  -0.0366   0.7945   0.0721
  -9.000  -0.7473   0.01788   0.01045  -0.0358   0.7938   0.0755
  -8.750  -0.7287   0.01744   0.01004  -0.0348   0.7931   0.0804
  -8.500  -0.7089   0.01707   0.00967  -0.0340   0.7924   0.0846
  -8.250  -0.6898   0.01667   0.00928  -0.0331   0.7917   0.0893
  -8.000  -0.6702   0.01630   0.00892  -0.0322   0.7909   0.0946
  -7.750  -0.6504   0.01595   0.00858  -0.0314   0.7901   0.1002
  -7.500  -0.6312   0.01558   0.00824  -0.0304   0.7894   0.1065
  -7.250  -0.6111   0.01526   0.00792  -0.0295   0.7886   0.1129
  -7.000  -0.5921   0.01489   0.00760  -0.0285   0.7878   0.1208
  -6.750  -0.5721   0.01458   0.00729  -0.0275   0.7870   0.1280
  -6.500  -0.5530   0.01423   0.00698  -0.0265   0.7860   0.1370
  -6.250  -0.5341   0.01389   0.00669  -0.0253   0.7851   0.1471
  -6.000  -0.5149   0.01358   0.00640  -0.0242   0.7844   0.1578
  -5.750  -0.4966   0.01324   0.00612  -0.0229   0.7836   0.1708
  -5.500  -0.4791   0.01290   0.00584  -0.0215   0.7829   0.1855
  -5.250  -0.4623   0.01258   0.00558  -0.0198   0.7822   0.2019
  -5.000  -0.4474   0.01228   0.00536  -0.0178   0.7815   0.2214
  -4.750  -0.4344   0.01198   0.00517  -0.0154   0.7807   0.2442
  -4.500  -0.4195   0.01171   0.00499  -0.0132   0.7800   0.2699
  -4.250  -0.4041   0.01138   0.00480  -0.0113   0.7793   0.3022
  -4.000  -0.3892   0.01101   0.00460  -0.0092   0.7785   0.3417
  -3.750  -0.3740   0.01059   0.00439  -0.0072   0.7776   0.3869
  -3.500  -0.3597   0.01011   0.00417  -0.0051   0.7767   0.4406
  -3.250  -0.3466   0.00956   0.00392  -0.0027   0.7758   0.5074
  -3.000  -0.3333   0.00898   0.00371  -0.0003   0.7748   0.5856
  -2.750  -0.3139   0.00883   0.00398   0.0015   0.7740   0.6649
  -2.500  -0.2862   0.00897   0.00417   0.0015   0.7731   0.6925
  -2.250  -0.2580   0.00906   0.00425   0.0014   0.7721   0.7051
  -2.000  -0.2299   0.00912   0.00427   0.0012   0.7712   0.7146
  -1.750  -0.2012   0.00923   0.00439   0.0010   0.7704   0.7211
  -1.500  -0.1730   0.00929   0.00440   0.0008   0.7694   0.7277
  -1.250  -0.1441   0.00940   0.00452   0.0006   0.7684   0.7326
  -1.000  -0.1152   0.00954   0.00467   0.0004   0.7675   0.7383
  -0.750  -0.0873   0.00966   0.00475   0.0004   0.7665   0.7457
  -0.500  -0.0573   0.00995   0.00511   0.0002   0.7654   0.7526
  -0.250  -0.0286   0.01012   0.00527   0.0002   0.7642   0.7593
   0.000   0.0000   0.01016   0.00527   0.0000   0.7627   0.7627
   0.250   0.0286   0.01012   0.00527  -0.0002   0.7593   0.7642
   0.500   0.0573   0.00995   0.00511  -0.0002   0.7526   0.7654
   0.750   0.0873   0.00966   0.00475  -0.0004   0.7457   0.7665
   1.000   0.1152   0.00954   0.00467  -0.0004   0.7383   0.7675
   1.250   0.1441   0.00940   0.00452  -0.0006   0.7327   0.7684
   1.500   0.1730   0.00929   0.00440  -0.0008   0.7277   0.7694
   1.750   0.2011   0.00923   0.00439  -0.0010   0.7212   0.7704
   2.000   0.2299   0.00912   0.00427  -0.0012   0.7146   0.7712
   2.250   0.2580   0.00906   0.00425  -0.0014   0.7051   0.7721
   2.500   0.2862   0.00896   0.00416  -0.0015   0.6922   0.7731
   2.750   0.3139   0.00883   0.00398  -0.0015   0.6651   0.7740
   3.000   0.3335   0.00897   0.00371   0.0002   0.5865   0.7748
   3.250   0.3466   0.00956   0.00392   0.0027   0.5073   0.7758
   3.500   0.3602   0.01010   0.00416   0.0050   0.4425   0.7767
   3.750   0.3741   0.01059   0.00439   0.0072   0.3874   0.7776
   4.000   0.3895   0.01100   0.00460   0.0092   0.3427   0.7785
   4.250   0.4040   0.01138   0.00480   0.0113   0.3018   0.7793
   4.500   0.4194   0.01171   0.00499   0.0133   0.2696   0.7800
   4.750   0.4343   0.01199   0.00517   0.0154   0.2439   0.7807
   5.250   0.4624   0.01258   0.00558   0.0198   0.2019   0.7822
   5.500   0.4790   0.01291   0.00584   0.0215   0.1849   0.7829
   5.750   0.4966   0.01324   0.00612   0.0229   0.1706   0.7836
   6.000   0.5149   0.01358   0.00640   0.0242   0.1576   0.7844
   6.250   0.5341   0.01389   0.00668   0.0253   0.1469   0.7851
   6.500   0.5531   0.01423   0.00698   0.0264   0.1369   0.7860
   6.750   0.5722   0.01457   0.00729   0.0275   0.1279   0.7870
   7.000   0.5921   0.01489   0.00759   0.0285   0.1203   0.7878
   7.250   0.6112   0.01526   0.00792   0.0295   0.1129   0.7886
   7.500   0.6314   0.01557   0.00824   0.0304   0.1066   0.7894
   7.750   0.6504   0.01595   0.00858   0.0313   0.1000   0.7901
   8.000   0.6704   0.01629   0.00892   0.0322   0.0947   0.7909
   8.250   0.6900   0.01667   0.00927   0.0331   0.0893   0.7916
   8.500   0.7091   0.01706   0.00966   0.0340   0.0846   0.7924
   8.750   0.7289   0.01744   0.01004   0.0348   0.0802   0.7931
   9.000   0.7477   0.01787   0.01044   0.0357   0.0758   0.7938
   9.250   0.7669   0.01828   0.01086   0.0366   0.0722   0.7945
   9.500   0.7861   0.01870   0.01129   0.0374   0.0684   0.7952
   9.750   0.8040   0.01918   0.01175   0.0384   0.0646   0.7959
  10.000   0.8231   0.01959   0.01220   0.0392   0.0618   0.7967
  10.250   0.8414   0.02005   0.01268   0.0401   0.0585   0.7976
  10.500   0.8587   0.02058   0.01321   0.0410   0.0555   0.7984
  10.750   0.8768   0.02107   0.01374   0.0419   0.0533   0.7993
  11.000   0.8948   0.02157   0.01427   0.0428   0.0508   0.8002
  11.250   0.9116   0.02214   0.01485   0.0437   0.0485   0.8012
  11.500   0.9281   0.02274   0.01548   0.0447   0.0462   0.8024
  11.750   0.9453   0.02330   0.01609   0.0455   0.0442   0.8035
  12.000   0.9617   0.02392   0.01674   0.0464   0.0424   0.8046
  12.250   0.9769   0.02462   0.01745   0.0474   0.0406   0.8056
  12.500   0.9925   0.02530   0.01818   0.0483   0.0391   0.8067
  12.750   1.0083   0.02598   0.01891   0.0491   0.0375   0.8077
  13.000   1.0231   0.02673   0.01969   0.0500   0.0359   0.8088
  13.250   1.0365   0.02758   0.02056   0.0510   0.0344   0.8099
  13.500   1.0503   0.02842   0.02145   0.0519   0.0332   0.8109
  13.750   1.0645   0.02924   0.02233   0.0527   0.0320   0.8120
  14.000   1.0770   0.03015   0.02330   0.0536   0.0305   0.8132
  14.250   1.0887   0.03116   0.02435   0.0545   0.0295   0.8145
  14.500   1.0989   0.03227   0.02552   0.0555   0.0285   0.8158
  14.750   1.1108   0.03330   0.02664   0.0563   0.0275   0.8172
  15.000   1.1215   0.03444   0.02786   0.0571   0.0267   0.8187
  15.250   1.1311   0.03570   0.02918   0.0579   0.0256   0.8203
  15.500   1.1397   0.03707   0.03060   0.0586   0.0248   0.8219
  15.750   1.1457   0.03870   0.03229   0.0593   0.0241   0.8236
  16.000   1.1538   0.04020   0.03389   0.0599   0.0236   0.8253
  16.250   1.1610   0.04183   0.03561   0.0603   0.0229   0.8270
  16.750   1.1716   0.04558   0.03955   0.0610   0.0219   0.8308
  17.000   1.1748   0.04775   0.04182   0.0612   0.0214   0.8331
  17.250   1.1762   0.05018   0.04434   0.0611   0.0207   0.8357
  17.500   1.1761   0.05291   0.04716   0.0609   0.0204   0.8385
  17.750   1.1758   0.05578   0.05014   0.0604   0.0199   0.8414
  18.000   1.1754   0.05881   0.05329   0.0597   0.0196   0.8442
  18.250   1.1734   0.06210   0.05672   0.0588   0.0192   0.8473
  18.500   1.1700   0.06570   0.06046   0.0576   0.0189   0.8508
  18.750   1.1638   0.06985   0.06476   0.0560   0.0186   0.8545
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