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J5012 12% (j5012-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: J5012 12% (j5012-il)
Reynolds number: 200,000
Max Cl/Cd: 45.73 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-j5012-il-200000-n5.txt
Download as CSV file: xf-j5012-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: J5012   12%                                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.8530   0.10026   0.09591  -0.0277   1.0000   0.0202
 -15.500  -0.8930   0.08788   0.08329  -0.0355   1.0000   0.0200
 -15.250  -0.9201   0.07903   0.07423  -0.0411   1.0000   0.0201
 -15.000  -0.9442   0.07147   0.06646  -0.0454   1.0000   0.0199
 -14.750  -0.9622   0.06544   0.06023  -0.0487   1.0000   0.0200
 -14.500  -0.9770   0.06033   0.05491  -0.0510   1.0000   0.0202
 -14.250  -0.9891   0.05600   0.05037  -0.0526   1.0000   0.0206
 -14.000  -0.9992   0.05208   0.04625  -0.0533   1.0000   0.0206
 -13.750  -1.0071   0.04874   0.04269  -0.0535   1.0000   0.0209
 -13.500  -1.0133   0.04579   0.03951  -0.0532   1.0000   0.0212
 -13.250  -1.0166   0.04327   0.03676  -0.0523   1.0000   0.0215
 -13.000  -1.0178   0.04094   0.03433  -0.0512   1.0000   0.0218
 -12.750  -1.0166   0.03897   0.03226  -0.0498   1.0000   0.0221
 -12.500  -1.0139   0.03726   0.03046  -0.0483   1.0000   0.0225
 -12.250  -1.0102   0.03576   0.02887  -0.0465   1.0000   0.0228
 -12.000  -1.0057   0.03428   0.02728  -0.0446   1.0000   0.0232
 -11.750  -1.0005   0.03290   0.02578  -0.0425   1.0000   0.0236
 -11.500  -0.9946   0.03166   0.02442  -0.0402   1.0000   0.0242
 -11.250  -0.9880   0.03046   0.02309  -0.0378   1.0000   0.0249
 -11.000  -0.9807   0.02936   0.02186  -0.0352   1.0000   0.0256
 -10.750  -0.9726   0.02841   0.02077  -0.0326   1.0000   0.0264
 -10.500  -0.9668   0.02737   0.01967  -0.0295   1.0000   0.0272
 -10.250  -0.9613   0.02646   0.01873  -0.0262   1.0000   0.0279
 -10.000  -0.9538   0.02570   0.01792  -0.0231   1.0000   0.0288
  -9.750  -0.9439   0.02490   0.01705  -0.0204   1.0000   0.0298
  -9.500  -0.9333   0.02410   0.01617  -0.0177   1.0000   0.0309
  -9.250  -0.9223   0.02334   0.01533  -0.0150   1.0000   0.0319
  -9.000  -0.9109   0.02262   0.01452  -0.0123   1.0000   0.0331
  -8.750  -0.9013   0.02184   0.01373  -0.0094   1.0000   0.0346
  -8.500  -0.8891   0.02122   0.01307  -0.0068   1.0000   0.0364
  -8.250  -0.8759   0.02068   0.01246  -0.0043   1.0000   0.0389
  -8.000  -0.8636   0.02007   0.01180  -0.0016   1.0000   0.0413
  -7.750  -0.8516   0.01946   0.01119   0.0011   1.0000   0.0439
  -7.500  -0.8380   0.01896   0.01064   0.0036   1.0000   0.0471
  -7.250  -0.8244   0.01846   0.01008   0.0061   1.0000   0.0506
  -7.000  -0.8107   0.01796   0.00960   0.0085   1.0000   0.0553
  -6.750  -0.7958   0.01756   0.00914   0.0108   1.0000   0.0603
  -6.500  -0.7816   0.01709   0.00871   0.0131   1.0000   0.0666
  -6.250  -0.7566   0.01663   0.00825   0.0132   0.9980   0.0757
  -6.000  -0.7249   0.01614   0.00780   0.0119   0.9943   0.0889
  -5.750  -0.6949   0.01565   0.00737   0.0110   0.9902   0.1054
  -5.500  -0.6640   0.01517   0.00697   0.0099   0.9859   0.1267
  -5.000  -0.6043   0.01422   0.00625   0.0082   0.9768   0.1835
  -4.750  -0.5736   0.01373   0.00593   0.0071   0.9723   0.2212
  -4.500  -0.5433   0.01326   0.00563   0.0062   0.9678   0.2622
  -4.250  -0.5162   0.01284   0.00536   0.0061   0.9615   0.3033
  -4.000  -0.4846   0.01241   0.00511   0.0050   0.9572   0.3496
  -3.750  -0.4572   0.01202   0.00490   0.0049   0.9514   0.3959
  -3.500  -0.4290   0.01165   0.00470   0.0047   0.9453   0.4414
  -3.250  -0.3963   0.01129   0.00453   0.0036   0.9414   0.4874
  -3.000  -0.3704   0.01101   0.00438   0.0041   0.9339   0.5257
  -2.750  -0.3390   0.01074   0.00425   0.0034   0.9283   0.5640
  -2.500  -0.3077   0.01050   0.00413   0.0029   0.9228   0.5999
  -2.250  -0.2805   0.01030   0.00404   0.0032   0.9146   0.6322
  -2.000  -0.2463   0.01010   0.00393   0.0021   0.9096   0.6635
  -1.750  -0.2202   0.00997   0.00388   0.0028   0.8996   0.6900
  -1.500  -0.1858   0.00982   0.00380   0.0017   0.8934   0.7150
  -1.250  -0.1582   0.00972   0.00376   0.0021   0.8828   0.7378
  -1.000  -0.1264   0.00963   0.00372   0.0016   0.8735   0.7587
  -0.750  -0.0934   0.00955   0.00367   0.0009   0.8638   0.7782
  -0.500  -0.0633   0.00951   0.00366   0.0008   0.8517   0.7957
  -0.250  -0.0320   0.00948   0.00364   0.0005   0.8393   0.8118
   0.000   0.0000   0.00947   0.00364   0.0000   0.8263   0.8263
   0.250   0.0320   0.00948   0.00365  -0.0005   0.8118   0.8394
   0.500   0.0633   0.00951   0.00366  -0.0008   0.7958   0.8516
   0.750   0.0934   0.00955   0.00367  -0.0009   0.7782   0.8638
   1.000   0.1264   0.00963   0.00372  -0.0016   0.7588   0.8735
   1.250   0.1582   0.00972   0.00375  -0.0021   0.7379   0.8828
   1.500   0.1857   0.00982   0.00380  -0.0017   0.7150   0.8935
   1.750   0.2201   0.00997   0.00388  -0.0028   0.6899   0.8996
   2.000   0.2462   0.01010   0.00393  -0.0021   0.6631   0.9096
   2.250   0.2804   0.01030   0.00404  -0.0032   0.6322   0.9146
   2.500   0.3078   0.01050   0.00413  -0.0029   0.6000   0.9228
   2.750   0.3390   0.01074   0.00425  -0.0034   0.5651   0.9283
   3.000   0.3705   0.01101   0.00438  -0.0041   0.5260   0.9339
   3.250   0.3962   0.01129   0.00452  -0.0036   0.4870   0.9413
   3.500   0.4289   0.01164   0.00470  -0.0047   0.4413   0.9452
   3.750   0.4571   0.01202   0.00489  -0.0049   0.3957   0.9513
   4.000   0.4847   0.01241   0.00511  -0.0050   0.3502   0.9572
   4.250   0.5162   0.01284   0.00536  -0.0061   0.3040   0.9615
   4.500   0.5433   0.01326   0.00562  -0.0062   0.2622   0.9678
   4.750   0.5736   0.01373   0.00593  -0.0072   0.2213   0.9723
   5.000   0.6044   0.01421   0.00624  -0.0082   0.1841   0.9768
   5.250   0.6316   0.01470   0.00660  -0.0085   0.1535   0.9825
   5.500   0.6639   0.01517   0.00697  -0.0099   0.1263   0.9859
   5.750   0.6949   0.01565   0.00736  -0.0110   0.1053   0.9902
   6.000   0.7250   0.01614   0.00780  -0.0119   0.0889   0.9943
   6.250   0.7567   0.01662   0.00825  -0.0132   0.0759   0.9980
   6.500   0.7816   0.01709   0.00871  -0.0131   0.0666   1.0000
   6.750   0.7958   0.01755   0.00914  -0.0108   0.0602   1.0000
   7.000   0.8107   0.01796   0.00960  -0.0085   0.0551   1.0000
   7.250   0.8244   0.01846   0.01008  -0.0061   0.0505   1.0000
   7.500   0.8380   0.01896   0.01064  -0.0035   0.0470   1.0000
   7.750   0.8516   0.01946   0.01119  -0.0011   0.0439   1.0000
   8.000   0.8634   0.02009   0.01181   0.0016   0.0410   1.0000
   8.250   0.8762   0.02066   0.01244   0.0042   0.0387   1.0000
   8.500   0.8891   0.02123   0.01308   0.0068   0.0365   1.0000
   8.750   0.9014   0.02183   0.01372   0.0094   0.0345   1.0000
   9.000   0.9105   0.02265   0.01452   0.0123   0.0330   1.0000
   9.250   0.9224   0.02334   0.01532   0.0150   0.0318   1.0000
   9.500   0.9334   0.02409   0.01617   0.0177   0.0306   1.0000
   9.750   0.9439   0.02489   0.01703   0.0204   0.0296   1.0000
  10.000   0.9538   0.02570   0.01791   0.0231   0.0287   1.0000
  10.250   0.9613   0.02647   0.01874   0.0262   0.0279   1.0000
  10.500   0.9669   0.02737   0.01966   0.0295   0.0271   1.0000
  10.750   0.9726   0.02846   0.02082   0.0326   0.0264   1.0000
  11.000   0.9806   0.02943   0.02194   0.0352   0.0256   1.0000
  11.250   0.9881   0.03049   0.02313   0.0377   0.0249   1.0000
  11.500   0.9948   0.03169   0.02445   0.0402   0.0243   1.0000
  11.750   1.0009   0.03295   0.02582   0.0424   0.0238   1.0000
  12.000   1.0062   0.03430   0.02731   0.0445   0.0233   1.0000
  12.250   1.0106   0.03575   0.02885   0.0465   0.0228   1.0000
  12.500   1.0143   0.03728   0.03048   0.0482   0.0224   1.0000
  12.750   1.0171   0.03899   0.03228   0.0498   0.0221   1.0000
  13.000   1.0186   0.04092   0.03431   0.0511   0.0218   1.0000
  13.250   1.0178   0.04324   0.03672   0.0522   0.0215   1.0000
  13.500   1.0135   0.04586   0.03958   0.0531   0.0212   1.0000
  13.750   1.0075   0.04883   0.04277   0.0534   0.0210   1.0000
  14.000   1.0003   0.05204   0.04620   0.0532   0.0206   1.0000
  14.250   0.9899   0.05593   0.05031   0.0523   0.0204   1.0000
  14.500   0.9776   0.06040   0.05498   0.0509   0.0203   1.0000
  14.750   0.9632   0.06546   0.06024   0.0485   0.0201   1.0000
  15.000   0.9444   0.07164   0.06663   0.0453   0.0201   1.0000
  15.250   0.9232   0.07871   0.07391   0.0411   0.0200   1.0000
  15.500   0.8962   0.08751   0.08292   0.0355   0.0200   1.0000
  15.750   0.8544   0.10023   0.09587   0.0276   0.0203   1.0000
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