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WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il)
Reynolds number: 100,000
Max Cl/Cd: 29.45 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05188-il-100000-n5.txt
Download as CSV file: xf-fx05188-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-188 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4661   0.09146   0.08616  -0.0857   0.9839   0.0344
 -13.250  -0.5002   0.08056   0.07501  -0.0944   0.9715   0.0340
 -13.000  -0.5246   0.07260   0.06677  -0.1010   0.9602   0.0338
 -12.750  -0.5403   0.06628   0.06014  -0.1063   0.9510   0.0337
 -12.500  -0.5495   0.06091   0.05443  -0.1108   0.9431   0.0336
 -12.250  -0.5535   0.05647   0.04965  -0.1143   0.9346   0.0337
 -12.000  -0.5536   0.05255   0.04536  -0.1170   0.9265   0.0339
 -11.750  -0.5495   0.04931   0.04178  -0.1187   0.9182   0.0340
 -11.500  -0.5412   0.04642   0.03854  -0.1201   0.9111   0.0341
 -11.250  -0.5322   0.04409   0.03591  -0.1203   0.9032   0.0343
 -11.000  -0.5162   0.04180   0.03328  -0.1211   0.8975   0.0346
 -10.750  -0.5008   0.03998   0.03120  -0.1209   0.8908   0.0349
 -10.500  -0.4801   0.03831   0.02927  -0.1210   0.8851   0.0353
 -10.250  -0.4546   0.03676   0.02745  -0.1216   0.8808   0.0358
 -10.000  -0.4282   0.03550   0.02608  -0.1219   0.8767   0.0365
  -9.750  -0.4059   0.03455   0.02513  -0.1219   0.8718   0.0376
  -9.500  -0.3817   0.03363   0.02414  -0.1221   0.8673   0.0390
  -9.250  -0.3535   0.03273   0.02314  -0.1225   0.8637   0.0402
  -9.000  -0.3267   0.03197   0.02228  -0.1226   0.8600   0.0412
  -8.750  -0.3052   0.03135   0.02160  -0.1218   0.8553   0.0421
  -8.500  -0.2852   0.03065   0.02091  -0.1212   0.8510   0.0432
  -8.250  -0.2665   0.02995   0.02020  -0.1206   0.8471   0.0443
  -8.000  -0.2499   0.02929   0.01948  -0.1198   0.8431   0.0457
  -7.750  -0.2394   0.02876   0.01893  -0.1180   0.8379   0.0477
  -7.500  -0.2269   0.02820   0.01829  -0.1164   0.8333   0.0500
  -7.250  -0.2146   0.02750   0.01759  -0.1150   0.8294   0.0532
  -7.000  -0.2036   0.02696   0.01699  -0.1133   0.8255   0.0564
  -6.750  -0.1996   0.02651   0.01653  -0.1103   0.8201   0.0600
  -6.500  -0.1936   0.02599   0.01600  -0.1077   0.8156   0.0658
  -6.250  -0.1866   0.02541   0.01544  -0.1052   0.8120   0.0752
  -5.750  -0.1908   0.02423   0.01470  -0.0978   0.8016   0.1413
  -5.500  -0.1961   0.02297   0.01401  -0.0943   0.7972   0.2432
  -5.250  -0.1944   0.02175   0.01356  -0.0916   0.7941   0.3893
  -5.000  -0.1915   0.02196   0.01423  -0.0873   0.7880   0.4698
  -4.750  -0.1733   0.02249   0.01499  -0.0848   0.7841   0.5376
  -4.500  -0.1464   0.02382   0.01639  -0.0827   0.7813   0.5870
  -4.250  -0.1125   0.02580   0.01832  -0.0808   0.7793   0.6144
  -4.000  -0.0908   0.02672   0.01914  -0.0787   0.7757   0.6272
  -3.750  -0.0841   0.02668   0.01903  -0.0762   0.7697   0.6382
  -3.500  -0.0590   0.02694   0.01917  -0.0753   0.7666   0.6415
  -3.250  -0.0327   0.02691   0.01900  -0.0753   0.7641   0.6473
  -3.000  -0.0049   0.02658   0.01850  -0.0761   0.7621   0.6547
  -2.500   0.0191   0.02670   0.01850  -0.0722   0.7510   0.6686
  -2.250   0.0467   0.02681   0.01853  -0.0718   0.7486   0.6712
  -2.000   0.0763   0.02682   0.01843  -0.0720   0.7468   0.6747
  -1.750   0.0802   0.02693   0.01851  -0.0695   0.7396   0.6838
  -1.500   0.1014   0.02707   0.01861  -0.0683   0.7357   0.6871
  -1.250   0.1286   0.02710   0.01857  -0.0680   0.7331   0.6905
  -1.000   0.1592   0.02697   0.01836  -0.0688   0.7312   0.6958
  -0.750   0.1663   0.02729   0.01866  -0.0663   0.7247   0.7027
  -0.500   0.1821   0.02758   0.01894  -0.0642   0.7198   0.7062
  -0.250   0.2096   0.02755   0.01886  -0.0642   0.7171   0.7106
   0.000   0.2445   0.02723   0.01844  -0.0664   0.7152   0.7174
   0.250   0.2754   0.02715   0.01832  -0.0669   0.7136   0.7200
   0.750   0.2908   0.02804   0.01926  -0.0610   0.7005   0.7281
   1.000   0.3264   0.02779   0.01895  -0.0631   0.6985   0.7332
   1.250   0.3605   0.02759   0.01871  -0.0643   0.6970   0.7364
   1.750   0.3729   0.02857   0.01977  -0.0581   0.6829   0.7440
   2.000   0.4098   0.02832   0.01949  -0.0600   0.6811   0.7480
   2.250   0.4509   0.02797   0.01910  -0.0627   0.6796   0.7520
   2.750   0.4587   0.02900   0.02023  -0.0557   0.6649   0.7588
   3.000   0.4955   0.02873   0.01997  -0.0573   0.6634   0.7623
   3.500   0.5150   0.02994   0.02125  -0.0537   0.6489   0.7702
   3.750   0.5477   0.02963   0.02098  -0.0543   0.6473   0.7728
   4.250   0.5702   0.03111   0.02256  -0.0514   0.6330   0.7808
   4.500   0.6098   0.03069   0.02216  -0.0535   0.6316   0.7841
   5.000   0.6293   0.03223   0.02387  -0.0498   0.6174   0.7900
   5.250   0.6642   0.03176   0.02345  -0.0507   0.6160   0.7930
   5.750   0.6967   0.03328   0.02511  -0.0499   0.6019   0.8002
   6.000   0.7293   0.03272   0.02463  -0.0501   0.6004   0.8025
   6.500   0.7564   0.03414   0.02622  -0.0478   0.5860   0.8087
   6.750   0.7942   0.03348   0.02566  -0.0490   0.5845   0.8116
   7.250   0.8278   0.03468   0.02705  -0.0478   0.5697   0.8175
   7.750   0.8649   0.03522   0.02781  -0.0461   0.5545   0.8230
   8.000   0.9110   0.03347   0.02615  -0.0474   0.5507   0.8257
   8.250   0.9230   0.03412   0.02689  -0.0462   0.5376   0.8289
   8.500   0.9372   0.03457   0.02743  -0.0452   0.5240   0.8317
   8.750   0.9592   0.03435   0.02730  -0.0443   0.5129   0.8341
   9.000   0.9901   0.03362   0.02665  -0.0442   0.5028   0.8366
   9.250   0.9993   0.03455   0.02769  -0.0429   0.4879   0.8396
   9.500   1.0154   0.03503   0.02824  -0.0421   0.4715   0.8426
   9.750   1.0358   0.03525   0.02849  -0.0416   0.4532   0.8453
  10.000   1.0424   0.03646   0.02975  -0.0403   0.4310   0.8476
  10.250   1.0582   0.03668   0.02989  -0.0390   0.4014   0.8500
  10.500   1.0676   0.03754   0.03059  -0.0374   0.3655   0.8529
  10.750   1.0715   0.03900   0.03185  -0.0358   0.3237   0.8559
  11.000   1.0702   0.04106   0.03363  -0.0342   0.2766   0.8587
  11.250   1.0659   0.04362   0.03592  -0.0329   0.2343   0.8613
  11.500   1.0609   0.04627   0.03837  -0.0315   0.1994   0.8635
  11.750   1.0570   0.04895   0.04090  -0.0303   0.1698   0.8659
  12.000   1.0558   0.05155   0.04340  -0.0295   0.1457   0.8684
  12.250   1.0563   0.05413   0.04590  -0.0290   0.1249   0.8712
  13.000   1.0617   0.06192   0.05359  -0.0280   0.0863   0.8804
  13.250   1.0642   0.06446   0.05616  -0.0276   0.0782   0.8838
  13.500   1.0659   0.06721   0.05892  -0.0275   0.0719   0.8871
  13.750   1.0718   0.06962   0.06143  -0.0276   0.0662   0.8906
  14.000   1.0755   0.07224   0.06410  -0.0276   0.0618   0.8940
  14.250   1.0803   0.07456   0.06650  -0.0274   0.0583   0.8980
  14.500   1.0869   0.07680   0.06884  -0.0273   0.0551   0.9026
  14.750   1.0925   0.07926   0.07135  -0.0275   0.0525   0.9074
  15.000   1.0984   0.08141   0.07359  -0.0274   0.0501   0.9132
  15.250   1.1060   0.08342   0.07573  -0.0273   0.0480   0.9206
  15.500   1.1116   0.08548   0.07787  -0.0270   0.0462   0.9311
  15.750   1.1158   0.08735   0.07982  -0.0267   0.0450   0.9549
  16.000   1.1250   0.08935   0.08183  -0.0273   0.0438   1.0000
  16.250   1.1388   0.09130   0.08394  -0.0279   0.0425   1.0000
  16.500   1.1511   0.09347   0.08624  -0.0287   0.0411   1.0000
  16.750   1.1617   0.09587   0.08874  -0.0296   0.0399   1.0000
  17.000   1.1710   0.09845   0.09139  -0.0307   0.0388   1.0000
  17.250   1.1806   0.10091   0.09386  -0.0318   0.0378   1.0000
  17.500   1.1911   0.10328   0.09631  -0.0327   0.0369   1.0000
  17.750   1.1989   0.10614   0.09938  -0.0338   0.0362   1.0000
  18.000   1.2052   0.10923   0.10269  -0.0350   0.0356   1.0000
  18.250   1.2097   0.11259   0.10624  -0.0364   0.0350   1.0000
  18.500   1.2118   0.11634   0.11017  -0.0381   0.0344   1.0000
  18.750   1.2122   0.12036   0.11437  -0.0401   0.0339   1.0000
  19.000   1.2113   0.12459   0.11876  -0.0424   0.0333   1.0000
  19.250   1.2099   0.12892   0.12324  -0.0448   0.0329   1.0000
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