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LWK 80-150/K25 (lwk80150k25-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: LWK 80-150/K25 (lwk80150k25-il)
Reynolds number: 100,000
Max Cl/Cd: 26.69 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lwk80150k25-il-100000-n5.txt
Download as CSV file: xf-lwk80150k25-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LWK 80-150/K25                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.7611   0.10633   0.10057  -0.0343   1.0000   0.0389
 -15.250  -0.8126   0.09190   0.08591  -0.0436   1.0000   0.0383
 -15.000  -0.8454   0.08290   0.07670  -0.0487   1.0000   0.0378
 -14.750  -0.8750   0.07565   0.06919  -0.0522   1.0000   0.0379
 -14.500  -0.9003   0.06965   0.06291  -0.0542   1.0000   0.0381
 -14.250  -0.9208   0.06466   0.05765  -0.0551   1.0000   0.0384
 -14.000  -0.9367   0.06041   0.05311  -0.0553   1.0000   0.0387
 -13.750  -0.9488   0.05669   0.04909  -0.0549   1.0000   0.0391
 -13.500  -0.9562   0.05345   0.04557  -0.0541   1.0000   0.0396
 -13.250  -0.9511   0.05130   0.04335  -0.0535   1.0000   0.0401
 -13.000  -0.9463   0.04933   0.04131  -0.0528   1.0000   0.0409
 -12.750  -0.9412   0.04728   0.03913  -0.0520   1.0000   0.0416
 -12.500  -0.9365   0.04547   0.03718  -0.0510   1.0000   0.0429
 -12.250  -0.9286   0.04352   0.03504  -0.0500   1.0000   0.0439
 -12.000  -0.9217   0.04162   0.03284  -0.0488   1.0000   0.0456
 -11.750  -0.9090   0.04006   0.03122  -0.0480   1.0000   0.0470
 -11.500  -0.8961   0.03874   0.02990  -0.0472   1.0000   0.0483
 -11.250  -0.8825   0.03739   0.02847  -0.0463   1.0000   0.0500
 -11.000  -0.8683   0.03610   0.02703  -0.0453   1.0000   0.0522
 -10.750  -0.8531   0.03484   0.02567  -0.0444   1.0000   0.0544
 -10.500  -0.8407   0.03381   0.02466  -0.0432   1.0000   0.0565
 -10.250  -0.8282   0.03284   0.02366  -0.0418   1.0000   0.0590
 -10.000  -0.8160   0.03196   0.02265  -0.0402   1.0000   0.0620
  -9.750  -0.8028   0.03090   0.02164  -0.0391   0.9929   0.0649
  -9.500  -0.7772   0.02990   0.02057  -0.0402   0.9787   0.0694
  -9.250  -0.7502   0.02881   0.01941  -0.0415   0.9704   0.0742
  -9.000  -0.7237   0.02782   0.01840  -0.0427   0.9636   0.0804
  -8.750  -0.6974   0.02682   0.01736  -0.0439   0.9577   0.0871
  -8.500  -0.6704   0.02597   0.01643  -0.0450   0.9523   0.0958
  -8.250  -0.6471   0.02506   0.01556  -0.0456   0.9461   0.1049
  -8.000  -0.6215   0.02421   0.01471  -0.0464   0.9412   0.1159
  -7.750  -0.6011   0.02350   0.01401  -0.0462   0.9348   0.1285
  -7.500  -0.5804   0.02278   0.01335  -0.0460   0.9294   0.1444
  -7.250  -0.5604   0.02211   0.01274  -0.0456   0.9247   0.1641
  -7.000  -0.5456   0.02153   0.01224  -0.0441   0.9189   0.1874
  -6.750  -0.5309   0.02088   0.01176  -0.0427   0.9137   0.2183
  -6.500  -0.5190   0.02027   0.01134  -0.0406   0.9085   0.2559
  -6.250  -0.5135   0.01975   0.01106  -0.0373   0.9023   0.2988
  -6.000  -0.5051   0.01915   0.01073  -0.0344   0.8976   0.3555
  -5.750  -0.4957   0.01859   0.01054  -0.0315   0.8936   0.4237
  -5.500  -0.4820   0.01841   0.01084  -0.0287   0.8890   0.5013
  -5.250  -0.4465   0.01899   0.01173  -0.0286   0.8866   0.5738
  -5.000  -0.4206   0.01946   0.01221  -0.0275   0.8833   0.6122
  -4.750  -0.4010   0.01976   0.01244  -0.0257   0.8801   0.6394
  -4.500  -0.3861   0.02001   0.01261  -0.0232   0.8765   0.6603
  -4.250  -0.3711   0.02038   0.01291  -0.0206   0.8719   0.6775
  -4.000  -0.3539   0.02070   0.01315  -0.0184   0.8678   0.6931
  -3.750  -0.3343   0.02107   0.01343  -0.0165   0.8647   0.7084
  -3.500  -0.2949   0.02191   0.01420  -0.0173   0.8633   0.7178
  -3.250  -0.2744   0.02230   0.01452  -0.0156   0.8601   0.7292
  -3.000  -0.2640   0.02254   0.01472  -0.0125   0.8549   0.7416
  -2.750  -0.2274   0.02313   0.01526  -0.0132   0.8526   0.7474
  -2.500  -0.2098   0.02326   0.01532  -0.0113   0.8493   0.7576
  -2.250  -0.1788   0.02349   0.01550  -0.0116   0.8471   0.7630
  -2.000  -0.1482   0.02369   0.01565  -0.0118   0.8448   0.7680
  -1.750  -0.1480   0.02371   0.01565  -0.0074   0.8386   0.7780
  -1.500  -0.1176   0.02393   0.01585  -0.0077   0.8357   0.7817
  -1.250  -0.0915   0.02401   0.01589  -0.0074   0.8326   0.7866
  -1.000  -0.0791   0.02382   0.01564  -0.0049   0.8293   0.7949
  -0.750  -0.0565   0.02402   0.01586  -0.0041   0.8249   0.7981
  -0.500  -0.0369   0.02413   0.01597  -0.0029   0.8202   0.8022
  -0.250  -0.0211   0.02405   0.01587  -0.0010   0.8160   0.8083
   0.000   0.0000   0.02391   0.01570   0.0000   0.8129   0.8129
   0.250   0.0210   0.02405   0.01587   0.0010   0.8082   0.8160
   0.500   0.0369   0.02413   0.01597   0.0029   0.8022   0.8202
   0.750   0.0567   0.02401   0.01585   0.0041   0.7980   0.8250
   1.000   0.0793   0.02382   0.01564   0.0049   0.7949   0.8293
   1.250   0.0914   0.02400   0.01589   0.0074   0.7866   0.8326
   1.500   0.1172   0.02394   0.01586   0.0077   0.7817   0.8357
   1.750   0.1473   0.02373   0.01567   0.0075   0.7781   0.8387
   2.000   0.1476   0.02370   0.01566   0.0119   0.7681   0.8451
   2.250   0.1791   0.02348   0.01549   0.0115   0.7629   0.8472
   2.500   0.2094   0.02326   0.01533   0.0114   0.7573   0.8494
   2.750   0.2277   0.02311   0.01524   0.0132   0.7473   0.8526
   3.000   0.2613   0.02258   0.01476   0.0129   0.7408   0.8552
   3.250   0.2744   0.02229   0.01452   0.0156   0.7292   0.8601
   3.500   0.2950   0.02189   0.01419   0.0173   0.7177   0.8633
   3.750   0.3342   0.02108   0.01343   0.0165   0.7085   0.8647
   4.000   0.3533   0.02074   0.01319   0.0184   0.6934   0.8679
   4.250   0.3710   0.02039   0.01292   0.0206   0.6776   0.8720
   4.500   0.3860   0.02001   0.01261   0.0232   0.6604   0.8765
   4.750   0.4008   0.01976   0.01244   0.0257   0.6391   0.8802
   5.000   0.4207   0.01945   0.01220   0.0275   0.6121   0.8834
   5.250   0.4465   0.01898   0.01173   0.0287   0.5733   0.8867
   5.500   0.4821   0.01841   0.01083   0.0287   0.5009   0.8890
   5.750   0.4959   0.01858   0.01054   0.0315   0.4247   0.8936
   6.000   0.5053   0.01914   0.01073   0.0344   0.3557   0.8976
   6.250   0.5138   0.01975   0.01105   0.0372   0.2992   0.9023
   6.500   0.5190   0.02028   0.01134   0.0406   0.2558   0.9085
   6.750   0.5311   0.02087   0.01175   0.0426   0.2188   0.9137
   7.000   0.5461   0.02152   0.01224   0.0440   0.1877   0.9189
   7.250   0.5608   0.02209   0.01273   0.0455   0.1647   0.9247
   7.500   0.5806   0.02278   0.01334   0.0460   0.1445   0.9294
   7.750   0.6014   0.02350   0.01401   0.0461   0.1286   0.9348
   8.000   0.6220   0.02420   0.01472   0.0464   0.1165   0.9412
   8.250   0.6475   0.02505   0.01555   0.0455   0.1050   0.9461
   8.500   0.6706   0.02597   0.01641   0.0449   0.0961   0.9524
   8.750   0.6980   0.02680   0.01735   0.0438   0.0874   0.9577
   9.000   0.7242   0.02782   0.01839   0.0427   0.0804   0.9637
   9.250   0.7508   0.02879   0.01940   0.0413   0.0743   0.9705
   9.500   0.7777   0.02985   0.02054   0.0401   0.0692   0.9789
   9.750   0.8031   0.03086   0.02161   0.0390   0.0647   0.9936
  10.000   0.8159   0.03193   0.02262   0.0402   0.0618   1.0000
  10.250   0.8285   0.03283   0.02365   0.0418   0.0590   1.0000
  10.500   0.8407   0.03379   0.02465   0.0432   0.0563   1.0000
  10.750   0.8530   0.03484   0.02564   0.0443   0.0542   1.0000
  11.000   0.8679   0.03609   0.02704   0.0453   0.0517   1.0000
  11.250   0.8826   0.03738   0.02846   0.0462   0.0498   1.0000
  11.500   0.8963   0.03872   0.02988   0.0471   0.0482   1.0000
  11.750   0.9096   0.04006   0.03122   0.0479   0.0468   1.0000
  12.000   0.9229   0.04164   0.03286   0.0487   0.0457   1.0000
  12.250   0.9305   0.04357   0.03508   0.0498   0.0441   1.0000
  12.500   0.9365   0.04547   0.03718   0.0509   0.0426   1.0000
  12.750   0.9421   0.04732   0.03916   0.0519   0.0416   1.0000
  13.000   0.9472   0.04923   0.04118   0.0527   0.0407   1.0000
  13.250   0.9526   0.05124   0.04327   0.0534   0.0400   1.0000
  13.500   0.9578   0.05347   0.04555   0.0540   0.0394   1.0000
  13.750   0.9492   0.05674   0.04915   0.0547   0.0390   1.0000
  14.000   0.9363   0.06057   0.05329   0.0551   0.0386   1.0000
  14.250   0.9208   0.06477   0.05777   0.0549   0.0383   1.0000
  14.500   0.8998   0.06983   0.06311   0.0539   0.0379   1.0000
  14.750   0.8760   0.07568   0.06922   0.0520   0.0378   1.0000
  15.000   0.8440   0.08336   0.07717   0.0482   0.0377   1.0000
  15.250   0.8053   0.09357   0.08762   0.0422   0.0382   1.0000
  15.500   0.7414   0.11140   0.10571   0.0307   0.0389   1.0000
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