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FX 71-L-150/30 AIRFOIL (fx71l150-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX 71-L-150/30 AIRFOIL (fx71l150-il)
Reynolds number: 100,000
Max Cl/Cd: 35.18 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx71l150-il-100000-n5.txt
Download as CSV file: xf-fx71l150-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 71-L-150/30 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7380   0.14024   0.13453   0.0098   1.0000   0.0290
 -15.500  -0.7914   0.12042   0.11454  -0.0017   1.0000   0.0284
 -15.250  -0.8360   0.10566   0.09954  -0.0111   1.0000   0.0279
 -15.000  -0.8695   0.09497   0.08858  -0.0180   1.0000   0.0277
 -14.750  -0.8926   0.08718   0.08056  -0.0225   1.0000   0.0275
 -14.500  -0.9111   0.08077   0.07391  -0.0259   1.0000   0.0274
 -14.250  -0.9271   0.07516   0.06807  -0.0285   1.0000   0.0275
 -14.000  -0.9388   0.07040   0.06309  -0.0303   1.0000   0.0276
 -13.750  -0.9463   0.06630   0.05877  -0.0315   1.0000   0.0276
 -13.500  -0.9509   0.06265   0.05492  -0.0324   1.0000   0.0277
 -13.250  -0.9555   0.05913   0.05115  -0.0329   1.0000   0.0282
 -13.000  -0.9560   0.05612   0.04791  -0.0332   1.0000   0.0286
 -12.750  -0.9526   0.05348   0.04506  -0.0331   1.0000   0.0288
 -12.500  -0.9460   0.05131   0.04282  -0.0330   1.0000   0.0293
 -12.250  -0.9379   0.04934   0.04079  -0.0328   1.0000   0.0297
 -12.000  -0.9303   0.04742   0.03882  -0.0325   1.0000   0.0304
 -11.750  -0.9201   0.04559   0.03689  -0.0321   1.0000   0.0309
 -11.500  -0.9095   0.04382   0.03501  -0.0315   1.0000   0.0317
 -11.250  -0.8973   0.04218   0.03325  -0.0309   1.0000   0.0323
 -11.000  -0.8846   0.04061   0.03156  -0.0302   1.0000   0.0330
 -10.750  -0.8740   0.03904   0.03002  -0.0295   1.0000   0.0336
 -10.500  -0.8638   0.03751   0.02849  -0.0288   1.0000   0.0344
 -10.250  -0.8534   0.03603   0.02697  -0.0281   1.0000   0.0353
 -10.000  -0.8433   0.03458   0.02546  -0.0273   1.0000   0.0364
  -9.750  -0.8338   0.03312   0.02395  -0.0264   1.0000   0.0377
  -9.500  -0.8253   0.03171   0.02255  -0.0255   1.0000   0.0389
  -9.250  -0.8168   0.03035   0.02116  -0.0243   1.0000   0.0411
  -9.000  -0.8087   0.02907   0.01987  -0.0230   1.0000   0.0433
  -8.750  -0.8007   0.02790   0.01869  -0.0214   1.0000   0.0465
  -8.500  -0.7926   0.02681   0.01762  -0.0196   1.0000   0.0502
  -8.250  -0.7822   0.02576   0.01661  -0.0182   1.0000   0.0558
  -8.000  -0.7593   0.02465   0.01551  -0.0191   0.9352   0.0654
  -7.750  -0.7325   0.02362   0.01447  -0.0204   0.9017   0.0823
  -7.250  -0.6970   0.02179   0.01279  -0.0190   0.8640   0.1284
  -7.000  -0.6817   0.02094   0.01205  -0.0178   0.8515   0.1586
  -6.750  -0.6669   0.02006   0.01135  -0.0164   0.8420   0.1957
  -6.500  -0.6524   0.01917   0.01068  -0.0150   0.8339   0.2454
  -6.250  -0.6383   0.01829   0.01015  -0.0134   0.8264   0.3086
  -6.000  -0.6217   0.01768   0.00988  -0.0118   0.8194   0.3746
  -5.750  -0.6011   0.01743   0.00985  -0.0105   0.8132   0.4294
  -5.500  -0.5782   0.01740   0.00989  -0.0094   0.8068   0.4710
  -5.250  -0.5540   0.01744   0.00988  -0.0085   0.8011   0.5000
  -5.000  -0.5290   0.01754   0.00993  -0.0077   0.7947   0.5229
  -4.750  -0.5040   0.01761   0.00988  -0.0070   0.7892   0.5414
  -4.500  -0.4779   0.01778   0.00997  -0.0063   0.7836   0.5568
  -4.250  -0.4515   0.01800   0.01015  -0.0056   0.7781   0.5701
  -4.000  -0.4255   0.01816   0.01018  -0.0049   0.7735   0.5834
  -3.750  -0.3990   0.01830   0.01026  -0.0045   0.7676   0.5954
  -3.500  -0.3719   0.01849   0.01039  -0.0039   0.7625   0.6044
  -3.250  -0.3455   0.01859   0.01039  -0.0035   0.7578   0.6137
  -3.000  -0.3186   0.01867   0.01043  -0.0032   0.7529   0.6210
  -2.750  -0.2919   0.01879   0.01046  -0.0028   0.7486   0.6289
  -2.500  -0.2657   0.01883   0.01041  -0.0024   0.7446   0.6367
  -2.250  -0.2387   0.01890   0.01046  -0.0022   0.7398   0.6432
  -2.000  -0.2130   0.01886   0.01030  -0.0019   0.7352   0.6510
  -1.750  -0.1860   0.01895   0.01036  -0.0014   0.7301   0.6561
  -1.500  -0.1600   0.01893   0.01028  -0.0012   0.7241   0.6632
  -1.250  -0.1333   0.01895   0.01024  -0.0008   0.7198   0.6682
  -1.000  -0.1066   0.01899   0.01030  -0.0006   0.7135   0.6730
  -0.750  -0.0803   0.01897   0.01021  -0.0005   0.7092   0.6796
  -0.500  -0.0532   0.01903   0.01030  -0.0003   0.7047   0.6839
  -0.250  -0.0267   0.01908   0.01036  -0.0001   0.6995   0.6897
   0.000   0.0000   0.01906   0.01032   0.0000   0.6953   0.6953
   0.250   0.0267   0.01908   0.01036   0.0001   0.6897   0.6995
   0.500   0.0532   0.01903   0.01030   0.0003   0.6839   0.7048
   0.750   0.0803   0.01897   0.01021   0.0005   0.6796   0.7092
   1.000   0.1066   0.01899   0.01030   0.0006   0.6730   0.7135
   1.250   0.1333   0.01895   0.01024   0.0008   0.6682   0.7198
   1.500   0.1600   0.01893   0.01028   0.0012   0.6632   0.7241
   1.750   0.1860   0.01895   0.01036   0.0014   0.6561   0.7301
   2.000   0.2130   0.01886   0.01030   0.0019   0.6510   0.7352
   2.250   0.2387   0.01890   0.01046   0.0022   0.6432   0.7398
   2.500   0.2657   0.01883   0.01041   0.0024   0.6367   0.7446
   2.750   0.2919   0.01878   0.01045   0.0028   0.6288   0.7486
   3.000   0.3186   0.01867   0.01042   0.0032   0.6210   0.7529
   3.250   0.3456   0.01859   0.01039   0.0035   0.6136   0.7578
   3.500   0.3719   0.01849   0.01038   0.0039   0.6043   0.7625
   3.750   0.3990   0.01830   0.01026   0.0045   0.5954   0.7676
   4.000   0.4255   0.01816   0.01019   0.0049   0.5835   0.7735
   4.250   0.4515   0.01800   0.01015   0.0056   0.5701   0.7781
   4.500   0.4780   0.01778   0.00997   0.0063   0.5569   0.7836
   4.750   0.5040   0.01761   0.00988   0.0070   0.5414   0.7892
   5.000   0.5290   0.01754   0.00993   0.0077   0.5229   0.7947
   5.250   0.5540   0.01744   0.00988   0.0085   0.5001   0.8011
   5.500   0.5782   0.01740   0.00989   0.0094   0.4709   0.8068
   5.750   0.6012   0.01743   0.00985   0.0105   0.4299   0.8132
   6.000   0.6219   0.01768   0.00989   0.0118   0.3759   0.8194
   6.250   0.6385   0.01828   0.01015   0.0134   0.3095   0.8264
   6.500   0.6525   0.01917   0.01068   0.0150   0.2456   0.8340
   6.750   0.6670   0.02005   0.01135   0.0164   0.1960   0.8420
   7.000   0.6816   0.02094   0.01206   0.0178   0.1576   0.8515
   7.250   0.6971   0.02180   0.01279   0.0190   0.1280   0.8639
   7.750   0.7327   0.02362   0.01447   0.0203   0.0821   0.9019
   8.000   0.7595   0.02465   0.01551   0.0190   0.0655   0.9352
   8.250   0.7824   0.02576   0.01660   0.0181   0.0557   1.0000
   8.500   0.7929   0.02681   0.01762   0.0196   0.0502   1.0000
   8.750   0.8008   0.02791   0.01870   0.0214   0.0462   1.0000
   9.000   0.8089   0.02908   0.01987   0.0230   0.0432   1.0000
   9.250   0.8172   0.03034   0.02115   0.0243   0.0410   1.0000
   9.500   0.8259   0.03169   0.02253   0.0254   0.0390   1.0000
   9.750   0.8343   0.03311   0.02394   0.0263   0.0377   1.0000
  10.000   0.8439   0.03455   0.02543   0.0272   0.0364   1.0000
  10.250   0.8540   0.03602   0.02696   0.0280   0.0353   1.0000
  10.500   0.8643   0.03751   0.02848   0.0288   0.0343   1.0000
  10.750   0.8751   0.03899   0.02998   0.0294   0.0338   1.0000
  11.000   0.8854   0.04057   0.03154   0.0301   0.0331   1.0000
  11.250   0.8982   0.04214   0.03320   0.0308   0.0324   1.0000
  11.500   0.9106   0.04378   0.03497   0.0315   0.0318   1.0000
  11.750   0.9212   0.04557   0.03687   0.0320   0.0310   1.0000
  12.000   0.9317   0.04738   0.03878   0.0324   0.0306   1.0000
  12.250   0.9390   0.04932   0.04078   0.0327   0.0298   1.0000
  12.500   0.9473   0.05130   0.04283   0.0329   0.0294   1.0000
  12.750   0.9535   0.05345   0.04503   0.0330   0.0288   1.0000
  13.000   0.9558   0.05620   0.04801   0.0330   0.0284   1.0000
  13.250   0.9547   0.05928   0.05132   0.0327   0.0280   1.0000
  13.500   0.9533   0.06248   0.05473   0.0323   0.0279   1.0000
  13.750   0.9478   0.06626   0.05872   0.0314   0.0277   1.0000
  14.000   0.9400   0.07039   0.06307   0.0302   0.0276   1.0000
  14.250   0.9292   0.07503   0.06793   0.0284   0.0276   1.0000
  14.500   0.9139   0.08051   0.07365   0.0259   0.0276   1.0000
  14.750   0.8940   0.08715   0.08052   0.0224   0.0276   1.0000
  15.000   0.8695   0.09520   0.08882   0.0176   0.0277   1.0000
  15.250   0.8394   0.10519   0.09906   0.0113   0.0280   1.0000
  15.500   0.7905   0.12098   0.11510   0.0012   0.0284   1.0000
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