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WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 75-141 (fx75141-il)
Reynolds number: 500,000
Max Cl/Cd: 103.23 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75141-il-500000-n5.txt
Download as CSV file: xf-fx75141-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 75-141                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.6279   0.08891   0.08553  -0.0791   0.8523   0.0122
 -15.250  -0.6819   0.07338   0.06973  -0.0896   0.8482   0.0120
 -14.750  -0.7289   0.05493   0.05080  -0.1049   0.8390   0.0119
 -14.500  -0.7364   0.04930   0.04498  -0.1101   0.8347   0.0120
 -14.250  -0.7396   0.04466   0.04014  -0.1146   0.8308   0.0121
 -13.750  -0.7341   0.03783   0.03296  -0.1210   0.8245   0.0125
 -13.500  -0.7305   0.03492   0.02988  -0.1234   0.8216   0.0126
 -13.250  -0.7211   0.03279   0.02758  -0.1251   0.8187   0.0129
 -13.000  -0.7126   0.03068   0.02532  -0.1266   0.8159   0.0130
 -12.750  -0.7028   0.02881   0.02330  -0.1277   0.8132   0.0133
 -12.500  -0.6922   0.02712   0.02150  -0.1286   0.8109   0.0135
 -12.250  -0.6810   0.02570   0.01999  -0.1289   0.8089   0.0137
 -12.000  -0.6677   0.02454   0.01877  -0.1291   0.8069   0.0141
 -11.750  -0.6554   0.02342   0.01757  -0.1288   0.8049   0.0143
 -11.500  -0.6441   0.02245   0.01651  -0.1282   0.8028   0.0146
 -11.250  -0.6315   0.02157   0.01554  -0.1274   0.8010   0.0149
 -11.000  -0.6147   0.02081   0.01468  -0.1268   0.7993   0.0153
 -10.750  -0.5962   0.02014   0.01389  -0.1264   0.7976   0.0157
 -10.500  -0.5766   0.01950   0.01314  -0.1259   0.7960   0.0162
 -10.250  -0.5577   0.01879   0.01236  -0.1254   0.7944   0.0168
 -10.000  -0.5374   0.01818   0.01172  -0.1250   0.7930   0.0174
  -9.750  -0.5159   0.01765   0.01115  -0.1246   0.7917   0.0180
  -9.500  -0.4936   0.01715   0.01059  -0.1243   0.7903   0.0186
  -9.250  -0.4710   0.01665   0.01002  -0.1240   0.7889   0.0193
  -9.000  -0.4479   0.01618   0.00948  -0.1237   0.7875   0.0199
  -8.750  -0.4249   0.01567   0.00892  -0.1234   0.7859   0.0207
  -8.500  -0.4009   0.01525   0.00847  -0.1232   0.7844   0.0217
  -8.250  -0.3762   0.01489   0.00806  -0.1230   0.7831   0.0228
  -8.000  -0.3510   0.01454   0.00766  -0.1229   0.7819   0.0240
  -7.750  -0.3259   0.01416   0.00722  -0.1228   0.7807   0.0251
  -7.500  -0.3003   0.01381   0.00685  -0.1228   0.7793   0.0266
  -7.250  -0.2749   0.01350   0.00652  -0.1227   0.7779   0.0282
  -7.000  -0.2490   0.01323   0.00621  -0.1226   0.7763   0.0299
  -6.750  -0.2236   0.01288   0.00586  -0.1225   0.7743   0.0321
  -6.500  -0.1974   0.01261   0.00558  -0.1224   0.7723   0.0345
  -6.250  -0.1710   0.01235   0.00529  -0.1224   0.7704   0.0367
  -6.000  -0.1446   0.01208   0.00501  -0.1223   0.7685   0.0400
  -5.750  -0.1175   0.01187   0.00476  -0.1224   0.7666   0.0433
  -5.500  -0.0906   0.01162   0.00451  -0.1224   0.7648   0.0479
  -5.250  -0.0631   0.01145   0.00431  -0.1225   0.7631   0.0523
  -5.000  -0.0366   0.01119   0.00410  -0.1225   0.7612   0.0593
  -4.750  -0.0097   0.01098   0.00391  -0.1225   0.7591   0.0667
  -4.500   0.0174   0.01077   0.00373  -0.1225   0.7570   0.0769
  -4.250   0.0446   0.01054   0.00356  -0.1226   0.7550   0.0916
  -4.000   0.0718   0.01031   0.00339  -0.1227   0.7530   0.1107
  -3.750   0.0992   0.01007   0.00322  -0.1228   0.7510   0.1346
  -3.500   0.1266   0.00981   0.00306  -0.1229   0.7492   0.1681
  -3.250   0.1543   0.00957   0.00292  -0.1232   0.7473   0.2076
  -3.000   0.1808   0.00926   0.00280  -0.1232   0.7451   0.2557
  -2.750   0.2073   0.00890   0.00266  -0.1233   0.7425   0.3199
  -2.500   0.2336   0.00852   0.00256  -0.1233   0.7399   0.4012
  -2.250   0.2609   0.00832   0.00250  -0.1233   0.7373   0.4544
  -2.000   0.2884   0.00818   0.00245  -0.1233   0.7350   0.4930
  -1.750   0.3163   0.00808   0.00241  -0.1234   0.7329   0.5233
  -1.500   0.3441   0.00801   0.00240  -0.1233   0.7305   0.5478
  -1.250   0.3714   0.00795   0.00241  -0.1232   0.7273   0.5664
  -1.000   0.3987   0.00790   0.00243  -0.1231   0.7240   0.5893
  -0.750   0.4263   0.00788   0.00246  -0.1229   0.7207   0.6101
  -0.500   0.4543   0.00788   0.00247  -0.1229   0.7178   0.6245
  -0.250   0.4822   0.00789   0.00250  -0.1228   0.7146   0.6392
   0.000   0.5096   0.00792   0.00256  -0.1227   0.7104   0.6530
   0.250   0.5372   0.00794   0.00260  -0.1226   0.7061   0.6628
   0.500   0.5651   0.00795   0.00259  -0.1225   0.7021   0.6689
   0.750   0.5927   0.00796   0.00262  -0.1224   0.6975   0.6739
   1.000   0.6202   0.00798   0.00264  -0.1223   0.6918   0.6795
   1.250   0.6477   0.00799   0.00263  -0.1222   0.6865   0.6843
   1.500   0.6749   0.00801   0.00268  -0.1220   0.6802   0.6881
   1.750   0.7019   0.00803   0.00270  -0.1218   0.6733   0.6925
   2.000   0.7291   0.00806   0.00273  -0.1216   0.6660   0.6971
   2.250   0.7556   0.00810   0.00275  -0.1213   0.6571   0.7006
   2.500   0.7814   0.00814   0.00278  -0.1208   0.6448   0.7037
   2.750   0.8055   0.00824   0.00280  -0.1199   0.6262   0.7073
   3.000   0.8284   0.00841   0.00286  -0.1189   0.6028   0.7111
   3.250   0.8518   0.00860   0.00296  -0.1180   0.5838   0.7148
   3.500   0.8762   0.00875   0.00308  -0.1173   0.5710   0.7174
   3.750   0.9004   0.00891   0.00322  -0.1166   0.5597   0.7203
   4.000   0.9245   0.00908   0.00338  -0.1158   0.5476   0.7234
   4.250   0.9484   0.00925   0.00353  -0.1151   0.5344   0.7267
   4.500   0.9720   0.00944   0.00369  -0.1143   0.5210   0.7297
   4.750   0.9951   0.00964   0.00387  -0.1134   0.5077   0.7324
   5.000   1.0169   0.00986   0.00407  -0.1123   0.4912   0.7350
   5.250   1.0348   0.01021   0.00432  -0.1104   0.4626   0.7378
   5.500   1.0496   0.01067   0.00462  -0.1080   0.4251   0.7407
   5.750   1.0629   0.01120   0.00497  -0.1054   0.3866   0.7436
   6.000   1.0746   0.01177   0.00536  -0.1025   0.3467   0.7466
   6.250   1.0812   0.01243   0.00582  -0.0987   0.3042   0.7494
   6.500   1.0870   0.01306   0.00629  -0.0948   0.2682   0.7523
   6.750   1.0951   0.01370   0.00679  -0.0914   0.2378   0.7556
   7.000   1.1047   0.01431   0.00730  -0.0884   0.2139   0.7596
   7.250   1.1146   0.01493   0.00782  -0.0855   0.1917   0.7636
   7.500   1.1243   0.01555   0.00839  -0.0826   0.1732   0.7673
   8.000   1.1465   0.01681   0.00956  -0.0777   0.1428   0.7738
   8.250   1.1574   0.01750   0.01021  -0.0755   0.1281   0.7770
   8.500   1.1675   0.01828   0.01092  -0.0732   0.1116   0.7799
   8.750   1.1778   0.01908   0.01169  -0.0711   0.0973   0.7828
   9.000   1.1877   0.01995   0.01252  -0.0690   0.0834   0.7864
   9.250   1.1979   0.02085   0.01339  -0.0670   0.0721   0.7903
   9.500   1.2088   0.02175   0.01427  -0.0652   0.0636   0.7939
   9.750   1.2197   0.02267   0.01519  -0.0635   0.0561   0.7977
  10.000   1.2321   0.02352   0.01607  -0.0619   0.0510   0.8019
  10.250   1.2434   0.02449   0.01705  -0.0604   0.0461   0.8067
  10.500   1.2567   0.02539   0.01801  -0.0592   0.0426   0.8122
  10.750   1.2695   0.02635   0.01902  -0.0580   0.0396   0.8194
  11.000   1.2818   0.02739   0.02011  -0.0568   0.0371   0.8276
  11.250   1.2951   0.02835   0.02115  -0.0558   0.0344   0.8390
  11.500   1.3079   0.02944   0.02233  -0.0549   0.0322   0.8573
  11.750   1.3327   0.03072   0.02377  -0.0566   0.0300   0.9025
  12.250   1.3616   0.03318   0.02634  -0.0560   0.0267   1.0000
  12.500   1.3703   0.03461   0.02780  -0.0549   0.0253   1.0000
  12.750   1.3805   0.03594   0.02919  -0.0539   0.0243   1.0000
  13.000   1.3904   0.03732   0.03064  -0.0529   0.0234   1.0000
  13.250   1.3993   0.03881   0.03218  -0.0519   0.0224   1.0000
  13.500   1.4073   0.04042   0.03384  -0.0510   0.0215   1.0000
  13.750   1.4133   0.04225   0.03571  -0.0500   0.0206   1.0000
  14.000   1.4210   0.04395   0.03749  -0.0492   0.0198   1.0000
  14.250   1.4291   0.04567   0.03929  -0.0485   0.0190   1.0000
  14.500   1.4357   0.04758   0.04127  -0.0478   0.0184   1.0000
  14.750   1.4419   0.04958   0.04333  -0.0472   0.0177   1.0000
  15.000   1.4465   0.05177   0.04558  -0.0466   0.0171   1.0000
  15.250   1.4494   0.05419   0.04807  -0.0461   0.0166   1.0000
  15.500   1.4532   0.05660   0.05056  -0.0458   0.0161   1.0000
  15.750   1.4576   0.05898   0.05304  -0.0455   0.0157   1.0000
  16.000   1.4610   0.06154   0.05569  -0.0453   0.0152   1.0000
  16.250   1.4636   0.06421   0.05845  -0.0452   0.0147   1.0000
  16.500   1.4666   0.06689   0.06121  -0.0453   0.0142   1.0000
  16.750   1.4671   0.06995   0.06436  -0.0454   0.0139   1.0000
  17.000   1.4665   0.07321   0.06769  -0.0457   0.0135   1.0000
  17.250   1.4632   0.07690   0.07146  -0.0461   0.0131   1.0000
  17.500   1.4622   0.08032   0.07499  -0.0467   0.0129   1.0000
  17.750   1.4607   0.08390   0.07869  -0.0473   0.0126   1.0000
  18.000   1.4584   0.08765   0.08255  -0.0481   0.0124   1.0000
  18.250   1.4556   0.09155   0.08656  -0.0491   0.0121   1.0000
  18.500   1.4512   0.09577   0.09089  -0.0503   0.0119   1.0000
  18.750   1.4470   0.10001   0.09524  -0.0516   0.0116   1.0000
  19.000   1.4418   0.10448   0.09982  -0.0532   0.0114   1.0000
  19.250   1.4361   0.10913   0.10458  -0.0549   0.0112   1.0000
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