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WORTMANN FX 2 AIRFOIL (fx2-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 2 AIRFOIL (fx2-il)
Reynolds number: 100,000
Max Cl/Cd: 22.71 at α=11°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx2-il-100000-n5.txt
Download as CSV file: xf-fx2-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 2 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.1599   0.11369   0.10745  -0.1659   0.8963   0.0340
 -15.750  -0.3055   0.08209   0.07561  -0.1789   0.8959   0.0313
 -15.500  -0.3450   0.07484   0.06811  -0.1810   0.8950   0.0310
 -15.250  -0.3668   0.07051   0.06361  -0.1816   0.8941   0.0311
 -15.000  -0.3841   0.06701   0.05994  -0.1814   0.8930   0.0313
 -14.750  -0.3959   0.06429   0.05709  -0.1810   0.8919   0.0317
 -14.500  -0.4065   0.06178   0.05443  -0.1802   0.8907   0.0322
 -14.250  -0.4157   0.05958   0.05208  -0.1792   0.8897   0.0328
 -14.000  -0.4248   0.05749   0.04981  -0.1778   0.8888   0.0336
 -13.750  -0.4325   0.05559   0.04771  -0.1762   0.8880   0.0346
 -13.500  -0.4380   0.05365   0.04552  -0.1745   0.8872   0.0356
 -13.250  -0.4483   0.05234   0.04396  -0.1712   0.8861   0.0366
 -13.000  -0.4620   0.05172   0.04321  -0.1664   0.8846   0.0373
 -12.750  -0.4755   0.05165   0.04316  -0.1612   0.8828   0.0378
 -12.500  -0.4888   0.05152   0.04303  -0.1559   0.8803   0.0384
 -12.250  -0.5015   0.05138   0.04286  -0.1508   0.8786   0.0390
 -12.000  -0.5117   0.05112   0.04256  -0.1460   0.8771   0.0398
 -11.750  -0.5222   0.05086   0.04223  -0.1412   0.8757   0.0407
 -11.500  -0.5300   0.05046   0.04172  -0.1367   0.8745   0.0423
 -11.250  -0.5266   0.04968   0.04069  -0.1340   0.8734   0.0446
 -11.000  -0.5154   0.04887   0.03987  -0.1327   0.8726   0.0467
 -10.750  -0.5033   0.04816   0.03911  -0.1315   0.8718   0.0491
 -10.500  -0.5754   0.04972   0.04073  -0.1147   0.8681   0.0469
 -10.250  -0.5908   0.04959   0.04061  -0.1086   0.8661   0.0479
 -10.000  -0.5938   0.04917   0.04013  -0.1046   0.8642   0.0497
  -9.750  -0.5932   0.04872   0.03957  -0.1010   0.8630   0.0523
  -9.500  -0.5899   0.04824   0.03897  -0.0978   0.8620   0.0551
  -9.250  -0.5871   0.04772   0.03847  -0.0948   0.8609   0.0578
  -9.000  -0.5769   0.04717   0.03786  -0.0929   0.8596   0.0614
  -8.750  -0.5644   0.04668   0.03717  -0.0912   0.8584   0.0658
  -8.500  -0.5514   0.04603   0.03662  -0.0896   0.8576   0.0703
  -8.250  -0.5414   0.04558   0.03614  -0.0877   0.8568   0.0748
  -8.000  -0.5621   0.04541   0.03594  -0.0804   0.8541   0.0761
  -7.750  -0.5775   0.04510   0.03557  -0.0740   0.8511   0.0781
  -7.500  -0.5823   0.04471   0.03511  -0.0693   0.8490   0.0807
  -7.250  -0.5861   0.04402   0.03448  -0.0651   0.8465   0.0843
  -7.000  -0.5834   0.04344   0.03386  -0.0619   0.8445   0.0888
  -6.750  -0.5744   0.04296   0.03329  -0.0597   0.8431   0.0941
  -6.500  -0.5631   0.04230   0.03267  -0.0582   0.8417   0.1000
  -6.250  -0.5683   0.04175   0.03210  -0.0536   0.8381   0.1039
  -6.000  -0.5707   0.04127   0.03157  -0.0495   0.8351   0.1084
  -5.750  -0.5642   0.04067   0.03102  -0.0469   0.8323   0.1153
  -5.500  -0.5508   0.04010   0.03047  -0.0454   0.8298   0.1273
  -5.250  -0.5346   0.03946   0.02992  -0.0445   0.8279   0.1493
  -5.000  -0.5188   0.03859   0.02931  -0.0439   0.8265   0.1953
  -4.750  -0.5070   0.03664   0.02824  -0.0438   0.8252   0.3392
  -4.500  -0.5183   0.03618   0.02871  -0.0372   0.8194   0.4600
  -4.250  -0.5039   0.03742   0.03024  -0.0332   0.8164   0.5588
  -4.000  -0.4818   0.03838   0.03115  -0.0315   0.8142   0.5852
  -3.750  -0.4545   0.03906   0.03167  -0.0315   0.8122   0.6085
  -3.500  -0.4251   0.04046   0.03294  -0.0308   0.8105   0.6299
  -3.250  -0.4109   0.04125   0.03361  -0.0285   0.8067   0.6475
  -3.000  -0.4002   0.04215   0.03446  -0.0251   0.8025   0.6591
  -2.750  -0.3791   0.04278   0.03497  -0.0238   0.7995   0.6693
  -2.500  -0.3532   0.04322   0.03525  -0.0238   0.7972   0.6809
  -2.250  -0.3286   0.04416   0.03614  -0.0220   0.7955   0.6870
  -1.750  -0.3029   0.04472   0.03656  -0.0174   0.7871   0.7010
  -1.500  -0.2801   0.04484   0.03657  -0.0171   0.7841   0.7070
  -1.250  -0.2521   0.04471   0.03631  -0.0185   0.7821   0.7122
  -1.000  -0.2237   0.04479   0.03629  -0.0190   0.7805   0.7140
  -0.750  -0.2140   0.04477   0.03623  -0.0168   0.7750   0.7163
  -0.500  -0.1932   0.04472   0.03610  -0.0167   0.7713   0.7185
  -0.250  -0.1659   0.04468   0.03596  -0.0176   0.7688   0.7212
   0.000  -0.1339   0.04458   0.03575  -0.0196   0.7670   0.7242
   0.250  -0.0985   0.04446   0.03551  -0.0224   0.7656   0.7269
   0.500  -0.0965   0.04455   0.03561  -0.0191   0.7580   0.7285
   0.750  -0.0704   0.04460   0.03562  -0.0194   0.7552   0.7302
   1.000  -0.0403   0.04463   0.03559  -0.0204   0.7533   0.7321
   1.500  -0.0029   0.04479   0.03570  -0.0196   0.7436   0.7364
   1.750   0.0280   0.04479   0.03563  -0.0212   0.7411   0.7387
   2.000   0.0623   0.04477   0.03555  -0.0234   0.7393   0.7411
   2.250   0.0727   0.04498   0.03576  -0.0219   0.7320   0.7432
   2.500   0.0990   0.04501   0.03579  -0.0222   0.7286   0.7448
   2.750   0.1294   0.04501   0.03580  -0.0232   0.7265   0.7466
   3.000   0.1421   0.04526   0.03607  -0.0217   0.7196   0.7488
   3.250   0.1681   0.04533   0.03614  -0.0223   0.7157   0.7509
   3.500   0.2001   0.04527   0.03608  -0.0237   0.7132   0.7529
   4.000   0.2444   0.04561   0.03643  -0.0243   0.7020   0.7576
   4.250   0.2745   0.04551   0.03637  -0.0252   0.6993   0.7591
   4.750   0.3137   0.04584   0.03680  -0.0241   0.6874   0.7624
   5.000   0.3450   0.04568   0.03669  -0.0251   0.6847   0.7643
   5.500   0.3864   0.04607   0.03720  -0.0247   0.6721   0.7689
   5.750   0.4197   0.04586   0.03704  -0.0261   0.6695   0.7713
   6.000   0.4337   0.04642   0.03765  -0.0254   0.6600   0.7735
   6.250   0.4629   0.04623   0.03754  -0.0260   0.6562   0.7750
   6.500   0.4955   0.04585   0.03727  -0.0269   0.6538   0.7766
   6.750   0.5054   0.04651   0.03802  -0.0253   0.6430   0.7782
   7.000   0.5372   0.04614   0.03775  -0.0262   0.6397   0.7799
   7.500   0.5819   0.04632   0.03814  -0.0259   0.6255   0.7836
   7.750   0.6167   0.04571   0.03764  -0.0270   0.6227   0.7858
   8.000   0.6307   0.04624   0.03827  -0.0260   0.6108   0.7879
   8.250   0.6697   0.04499   0.03713  -0.0273   0.6068   0.7901
   8.500   0.6870   0.04480   0.03706  -0.0260   0.5932   0.7918
   8.750   0.7075   0.04446   0.03683  -0.0249   0.5801   0.7935
   9.000   0.7332   0.04392   0.03640  -0.0246   0.5690   0.7952
   9.250   0.7638   0.04309   0.03570  -0.0247   0.5585   0.7969
   9.500   0.7855   0.04306   0.03578  -0.0242   0.5433   0.7987
   9.750   0.8117   0.04268   0.03549  -0.0241   0.5267   0.8007
  10.000   0.8367   0.04244   0.03533  -0.0239   0.5064   0.8028
  10.250   0.8659   0.04190   0.03481  -0.0240   0.4816   0.8050
  10.500   0.8958   0.04141   0.03431  -0.0243   0.4553   0.8072
  10.750   0.9209   0.04112   0.03396  -0.0238   0.4233   0.8093
  11.000   0.9397   0.04137   0.03410  -0.0228   0.3848   0.8115
  11.250   0.9514   0.04222   0.03474  -0.0213   0.3391   0.8137
  11.500   0.9567   0.04365   0.03591  -0.0195   0.2904   0.8155
  11.750   0.9583   0.04550   0.03747  -0.0176   0.2434   0.8172
  12.000   0.9590   0.04757   0.03924  -0.0159   0.2004   0.8188
  12.250   0.9619   0.04959   0.04104  -0.0145   0.1661   0.8204
  12.500   0.9676   0.05147   0.04277  -0.0135   0.1402   0.8219
  12.750   0.9756   0.05320   0.04447  -0.0127   0.1195   0.8233
  13.000   0.9825   0.05500   0.04621  -0.0119   0.1035   0.8244
  13.250   0.9897   0.05683   0.04803  -0.0111   0.0920   0.8256
  13.500   0.9963   0.05875   0.04996  -0.0104   0.0819   0.8268
  14.000   1.0088   0.06284   0.05415  -0.0091   0.0646   0.8296
  14.250   1.0141   0.06505   0.05642  -0.0085   0.0572   0.8312
  14.500   1.0195   0.06732   0.05876  -0.0081   0.0515   0.8330
  14.750   1.0263   0.06951   0.06105  -0.0078   0.0460   0.8347
  15.000   1.0308   0.07198   0.06355  -0.0076   0.0427   0.8363
  15.250   1.0379   0.07423   0.06592  -0.0075   0.0398   0.8377
  15.500   1.0432   0.07663   0.06842  -0.0073   0.0369   0.8390
  15.750   1.0460   0.07932   0.07113  -0.0073   0.0351   0.8404
  16.000   1.0531   0.08158   0.07358  -0.0072   0.0332   0.8419
  16.250   1.0594   0.08397   0.07611  -0.0072   0.0318   0.8435
  16.500   1.0648   0.08650   0.07875  -0.0074   0.0305   0.8452
  16.750   1.0691   0.08919   0.08155  -0.0077   0.0293   0.8471
  17.000   1.0731   0.09192   0.08433  -0.0081   0.0283   0.8489
  17.250   1.0789   0.09457   0.08716  -0.0085   0.0272   0.8509
  17.500   1.0842   0.09730   0.09009  -0.0089   0.0262   0.8528
  17.750   1.0878   0.10017   0.09316  -0.0094   0.0254   0.8548
  18.000   1.0906   0.10318   0.09636  -0.0100   0.0248   0.8570
  18.250   1.0922   0.10638   0.09973  -0.0107   0.0242   0.8596
  18.500   1.0927   0.10979   0.10330  -0.0117   0.0237   0.8625
  18.750   1.0922   0.11337   0.10703  -0.0129   0.0232   0.8656
  19.000   1.0910   0.11700   0.11080  -0.0142   0.0228   0.8690
  19.250   1.0892   0.12068   0.11463  -0.0156   0.0223   0.8728
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