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WORTMANN FX 60-126 AIRFOIL (fx60126-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 60-126 AIRFOIL (fx60126-il)
Reynolds number: 100,000
Max Cl/Cd: 58.51 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60126-il-100000-n5.txt
Download as CSV file: xf-fx60126-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 60-126 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.4727   0.07588   0.07058  -0.0577   1.0000   0.0222
 -10.500  -0.4942   0.06878   0.06346  -0.0621   1.0000   0.0219
 -10.250  -0.5165   0.06266   0.05732  -0.0658   1.0000   0.0217
 -10.000  -0.5395   0.05766   0.05228  -0.0684   1.0000   0.0215
  -9.750  -0.5653   0.05394   0.04853  -0.0688   1.0000   0.0213
  -9.500  -0.5903   0.05112   0.04569  -0.0682   1.0000   0.0211
  -9.250  -0.6082   0.04793   0.04237  -0.0689   1.0000   0.0210
  -9.000  -0.6199   0.04477   0.03897  -0.0690   1.0000   0.0212
  -8.750  -0.6233   0.04173   0.03561  -0.0691   1.0000   0.0215
  -8.500  -0.6032   0.03768   0.03095  -0.0733   0.9955   0.0223
  -8.250  -0.5752   0.03503   0.02806  -0.0764   0.9905   0.0229
  -8.000  -0.5450   0.03277   0.02558  -0.0793   0.9855   0.0236
  -7.750  -0.5137   0.03075   0.02333  -0.0817   0.9808   0.0245
  -7.500  -0.4837   0.02897   0.02134  -0.0835   0.9754   0.0255
  -7.250  -0.4506   0.02730   0.01942  -0.0856   0.9711   0.0270
  -7.000  -0.4201   0.02591   0.01795  -0.0873   0.9658   0.0285
  -6.750  -0.3875   0.02472   0.01666  -0.0893   0.9602   0.0315
  -6.500  -0.3504   0.02348   0.01532  -0.0922   0.9560   0.0368
  -6.250  -0.3189   0.02225   0.01401  -0.0939   0.9496   0.0443
  -6.000  -0.2834   0.02118   0.01291  -0.0963   0.9443   0.0599
  -5.750  -0.2450   0.02003   0.01187  -0.0994   0.9408   0.0864
  -5.500  -0.2139   0.01914   0.01112  -0.1010   0.9344   0.1228
  -5.250  -0.1785   0.01824   0.01039  -0.1034   0.9291   0.1702
  -5.000  -0.1398   0.01757   0.00980  -0.1060   0.9251   0.2181
  -4.750  -0.1098   0.01718   0.00948  -0.1067   0.9171   0.2625
  -4.500  -0.0740   0.01690   0.00921  -0.1083   0.9116   0.3049
  -4.250  -0.0414   0.01676   0.00908  -0.1091   0.9051   0.3392
  -4.000  -0.0097   0.01670   0.00896  -0.1097   0.8981   0.3686
  -3.750   0.0262   0.01660   0.00877  -0.1110   0.8934   0.3908
  -3.500   0.0537   0.01659   0.00869  -0.1108   0.8845   0.4101
  -3.250   0.0881   0.01651   0.00853  -0.1117   0.8788   0.4296
  -3.000   0.1163   0.01650   0.00845  -0.1115   0.8696   0.4459
  -2.750   0.1495   0.01640   0.00828  -0.1121   0.8629   0.4613
  -2.500   0.1773   0.01636   0.00819  -0.1118   0.8531   0.4740
  -2.250   0.2097   0.01624   0.00802  -0.1122   0.8465   0.4859
  -2.000   0.2367   0.01621   0.00795  -0.1118   0.8363   0.4968
  -1.750   0.2682   0.01610   0.00775  -0.1122   0.8289   0.5082
  -1.500   0.2955   0.01607   0.00771  -0.1117   0.8188   0.5184
  -1.250   0.3241   0.01600   0.00762  -0.1115   0.8090   0.5288
  -1.000   0.3546   0.01589   0.00742  -0.1116   0.7996   0.5395
  -0.750   0.3813   0.01583   0.00737  -0.1111   0.7876   0.5476
  -0.500   0.4096   0.01577   0.00726  -0.1109   0.7766   0.5572
  -0.250   0.4390   0.01569   0.00715  -0.1108   0.7670   0.5669
   0.000   0.4661   0.01568   0.00714  -0.1104   0.7552   0.5765
   0.250   0.4941   0.01567   0.00711  -0.1102   0.7436   0.5872
   0.500   0.5219   0.01562   0.00706  -0.1098   0.7319   0.5967
   0.750   0.5502   0.01557   0.00698  -0.1095   0.7197   0.6064
   1.000   0.5780   0.01556   0.00695  -0.1092   0.7064   0.6167
   1.250   0.6048   0.01557   0.00697  -0.1087   0.6929   0.6258
   1.500   0.6322   0.01560   0.00700  -0.1084   0.6802   0.6364
   1.750   0.6597   0.01564   0.00704  -0.1081   0.6679   0.6477
   2.000   0.6869   0.01568   0.00708  -0.1077   0.6553   0.6589
   2.250   0.7139   0.01573   0.00713  -0.1072   0.6418   0.6711
   2.500   0.7407   0.01580   0.00720  -0.1067   0.6278   0.6844
   2.750   0.7670   0.01589   0.00732  -0.1062   0.6137   0.6983
   3.000   0.7931   0.01600   0.00746  -0.1057   0.6002   0.7128
   3.250   0.8188   0.01611   0.00760  -0.1050   0.5855   0.7286
   3.500   0.8437   0.01621   0.00775  -0.1042   0.5697   0.7462
   3.750   0.8679   0.01631   0.00788  -0.1033   0.5534   0.7666
   4.000   0.8912   0.01641   0.00802  -0.1021   0.5369   0.7922
   4.250   0.9125   0.01646   0.00819  -0.1006   0.5213   0.8287
   4.500   0.9335   0.01638   0.00825  -0.0989   0.5059   1.0000
   4.750   0.9604   0.01670   0.00850  -0.0988   0.4889   1.0000
   5.000   0.9865   0.01703   0.00877  -0.0986   0.4720   1.0000
   5.250   1.0121   0.01739   0.00909  -0.0983   0.4556   1.0000
   5.500   1.0371   0.01775   0.00944  -0.0979   0.4384   1.0000
   5.750   1.0614   0.01814   0.00982  -0.0973   0.4195   1.0000
   6.000   1.0849   0.01856   0.01020  -0.0967   0.3999   1.0000
   6.250   1.1078   0.01902   0.01062  -0.0959   0.3799   1.0000
   6.500   1.1301   0.01951   0.01107  -0.0951   0.3592   1.0000
   6.750   1.1515   0.02005   0.01158  -0.0942   0.3378   1.0000
   7.000   1.1722   0.02064   0.01212  -0.0932   0.3167   1.0000
   7.250   1.1925   0.02126   0.01271  -0.0922   0.2957   1.0000
   7.500   1.2115   0.02196   0.01336  -0.0910   0.2747   1.0000
   7.750   1.2294   0.02272   0.01409  -0.0897   0.2523   1.0000
   8.000   1.2460   0.02355   0.01485  -0.0883   0.2314   1.0000
   8.250   1.2618   0.02444   0.01569  -0.0868   0.2129   1.0000
   8.500   1.2770   0.02535   0.01659  -0.0852   0.1964   1.0000
   8.750   1.2906   0.02635   0.01756  -0.0835   0.1823   1.0000
   9.000   1.3025   0.02736   0.01857  -0.0815   0.1691   1.0000
   9.250   1.3136   0.02840   0.01963  -0.0795   0.1564   1.0000
   9.500   1.3235   0.02953   0.02077  -0.0774   0.1451   1.0000
   9.750   1.3316   0.03079   0.02201  -0.0753   0.1359   1.0000
  10.000   1.3396   0.03212   0.02336  -0.0734   0.1275   1.0000
  10.250   1.3480   0.03349   0.02481  -0.0715   0.1201   1.0000
  10.500   1.3555   0.03496   0.02634  -0.0698   0.1130   1.0000
  10.750   1.3632   0.03648   0.02795  -0.0682   0.1070   1.0000
  11.000   1.3699   0.03810   0.02965  -0.0667   0.1015   1.0000
  11.250   1.3746   0.03995   0.03151  -0.0653   0.0974   1.0000
  11.500   1.3819   0.04171   0.03341  -0.0640   0.0928   1.0000
  11.750   1.3867   0.04369   0.03549  -0.0629   0.0890   1.0000
  12.000   1.3894   0.04595   0.03772  -0.0617   0.0858   1.0000
  12.250   1.3967   0.04792   0.03991  -0.0608   0.0820   1.0000
  12.500   1.4020   0.05011   0.04224  -0.0600   0.0786   1.0000
  12.750   1.4060   0.05245   0.04469  -0.0594   0.0760   1.0000
  13.000   1.4093   0.05494   0.04720  -0.0588   0.0739   1.0000
  13.250   1.4149   0.05736   0.04983  -0.0582   0.0716   1.0000
  13.500   1.4189   0.05997   0.05263  -0.0579   0.0693   1.0000
  13.750   1.4217   0.06274   0.05555  -0.0577   0.0673   1.0000
  14.000   1.4233   0.06563   0.05857  -0.0577   0.0655   1.0000
  14.250   1.4248   0.06859   0.06160  -0.0578   0.0639   1.0000
  14.500   1.4266   0.07168   0.06481  -0.0579   0.0623   1.0000
  14.750   1.4256   0.07530   0.06867  -0.0583   0.0609   1.0000
  15.000   1.4239   0.07910   0.07270  -0.0589   0.0596   1.0000
  15.250   1.4212   0.08311   0.07692  -0.0598   0.0584   1.0000
  15.500   1.4176   0.08733   0.08133  -0.0609   0.0573   1.0000
  15.750   1.4134   0.09173   0.08591  -0.0622   0.0563   1.0000
  16.000   1.4090   0.09620   0.09052  -0.0638   0.0553   1.0000
  16.250   1.4063   0.10042   0.09485  -0.0653   0.0542   1.0000
  16.500   1.4072   0.10408   0.09857  -0.0664   0.0530   1.0000
  16.750   1.3957   0.11016   0.10484  -0.0692   0.0522   1.0000
  17.000   1.3753   0.11816   0.11315  -0.0738   0.0518   1.0000
  17.250   1.3509   0.12743   0.12270  -0.0796   0.0514   1.0000
  17.500   1.3196   0.13886   0.13441  -0.0872   0.0513   1.0000
  17.750   1.2665   0.15690   0.15272  -0.0999   0.0516   1.0000
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