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WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 75-141 (fx75141-il)
Reynolds number: 1,000,000
Max Cl/Cd: 134.87 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx75141-il-1000000.txt
Download as CSV file: xf-fx75141-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7627   0.07353   0.07064  -0.0818   0.8556   0.0117
 -15.500  -0.7998   0.06213   0.05898  -0.0904   0.8499   0.0116
 -15.250  -0.8099   0.05576   0.05244  -0.0959   0.8444   0.0116
 -15.000  -0.8227   0.04947   0.04596  -0.1014   0.8403   0.0117
 -14.750  -0.8259   0.04486   0.04121  -0.1057   0.8366   0.0118
 -14.500  -0.8256   0.04070   0.03688  -0.1099   0.8330   0.0119
 -14.250  -0.8176   0.03732   0.03334  -0.1141   0.8298   0.0120
 -14.000  -0.8089   0.03415   0.02999  -0.1181   0.8266   0.0122
 -13.750  -0.7946   0.03234   0.02808  -0.1202   0.8244   0.0125
 -13.500  -0.7862   0.02982   0.02542  -0.1226   0.8221   0.0125
 -13.250  -0.7667   0.02862   0.02412  -0.1243   0.8200   0.0129
 -13.000  -0.7527   0.02678   0.02215  -0.1261   0.8178   0.0130
 -12.750  -0.7339   0.02552   0.02078  -0.1276   0.8157   0.0132
 -12.500  -0.7264   0.02303   0.01811  -0.1292   0.8133   0.0135
 -12.250  -0.7111   0.02159   0.01657  -0.1303   0.8110   0.0138
 -12.000  -0.6972   0.02061   0.01555  -0.1302   0.8096   0.0142
 -11.750  -0.6812   0.02002   0.01493  -0.1297   0.8080   0.0146
 -11.500  -0.6647   0.01917   0.01400  -0.1293   0.8062   0.0149
 -11.250  -0.6451   0.01855   0.01332  -0.1289   0.8045   0.0153
 -11.000  -0.6249   0.01794   0.01264  -0.1286   0.8030   0.0156
 -10.750  -0.6037   0.01739   0.01200  -0.1283   0.8016   0.0160
 -10.500  -0.5811   0.01694   0.01148  -0.1280   0.8003   0.0163
 -10.250  -0.5637   0.01595   0.01040  -0.1274   0.7988   0.0170
 -10.000  -0.5418   0.01536   0.00977  -0.1271   0.7973   0.0176
  -9.750  -0.5174   0.01496   0.00933  -0.1271   0.7956   0.0182
  -9.500  -0.4934   0.01459   0.00892  -0.1269   0.7944   0.0188
  -9.250  -0.4695   0.01419   0.00848  -0.1266   0.7934   0.0194
  -9.000  -0.4444   0.01390   0.00815  -0.1265   0.7923   0.0200
  -8.750  -0.4220   0.01326   0.00748  -0.1261   0.7911   0.0211
  -8.500  -0.3974   0.01288   0.00707  -0.1259   0.7898   0.0220
  -8.250  -0.3718   0.01258   0.00675  -0.1258   0.7883   0.0230
  -8.000  -0.3458   0.01230   0.00643  -0.1257   0.7868   0.0240
  -7.750  -0.3202   0.01196   0.00604  -0.1256   0.7852   0.0251
  -7.500  -0.2950   0.01155   0.00562  -0.1255   0.7835   0.0268
  -7.250  -0.2681   0.01136   0.00541  -0.1255   0.7818   0.0285
  -7.000  -0.2405   0.01123   0.00524  -0.1257   0.7797   0.0298
  -6.750  -0.2152   0.01082   0.00483  -0.1255   0.7783   0.0325
  -6.500  -0.1885   0.01060   0.00461  -0.1254   0.7769   0.0348
  -6.250  -0.1618   0.01035   0.00435  -0.1254   0.7752   0.0372
  -6.000  -0.1350   0.01010   0.00412  -0.1254   0.7735   0.0411
  -5.750  -0.1076   0.00993   0.00393  -0.1254   0.7718   0.0440
  -5.500  -0.0805   0.00967   0.00369  -0.1255   0.7702   0.0495
  -5.250  -0.0528   0.00949   0.00349  -0.1255   0.7686   0.0546
  -5.000  -0.0253   0.00929   0.00331  -0.1257   0.7669   0.0618
  -4.750   0.0024   0.00910   0.00316  -0.1258   0.7652   0.0723
  -4.500   0.0303   0.00895   0.00305  -0.1260   0.7632   0.0873
  -4.250   0.0572   0.00869   0.00289  -0.1260   0.7619   0.1090
  -4.000   0.0843   0.00844   0.00274  -0.1260   0.7602   0.1356
  -3.750   0.1113   0.00815   0.00260  -0.1261   0.7583   0.1751
  -3.500   0.1383   0.00784   0.00245  -0.1261   0.7562   0.2237
  -3.250   0.1652   0.00750   0.00231  -0.1262   0.7543   0.2828
  -3.000   0.1917   0.00708   0.00217  -0.1263   0.7524   0.3683
  -2.750   0.2188   0.00681   0.00208  -0.1264   0.7505   0.4393
  -2.500   0.2469   0.00670   0.00205  -0.1265   0.7484   0.4776
  -2.250   0.2748   0.00661   0.00204  -0.1266   0.7463   0.5072
  -2.000   0.3024   0.00650   0.00199  -0.1265   0.7443   0.5313
  -1.750   0.3302   0.00642   0.00196  -0.1265   0.7418   0.5511
  -1.500   0.3581   0.00633   0.00193  -0.1265   0.7393   0.5749
  -1.250   0.3862   0.00627   0.00191  -0.1265   0.7368   0.5957
  -1.000   0.4144   0.00624   0.00190  -0.1265   0.7344   0.6129
  -0.750   0.4432   0.00627   0.00192  -0.1266   0.7315   0.6259
  -0.500   0.4708   0.00624   0.00194  -0.1265   0.7289   0.6403
  -0.250   0.4988   0.00623   0.00195  -0.1265   0.7257   0.6523
   0.000   0.5269   0.00622   0.00195  -0.1264   0.7223   0.6609
   0.250   0.5551   0.00622   0.00194  -0.1264   0.7190   0.6694
   0.500   0.5835   0.00628   0.00198  -0.1264   0.7155   0.6783
   0.750   0.6109   0.00627   0.00201  -0.1263   0.7115   0.6857
   1.000   0.6386   0.00627   0.00203  -0.1262   0.7070   0.6907
   1.250   0.6665   0.00628   0.00203  -0.1261   0.7026   0.6955
   1.500   0.6942   0.00630   0.00204  -0.1260   0.6972   0.6994
   1.750   0.7211   0.00626   0.00202  -0.1257   0.6893   0.7032
   2.000   0.7476   0.00626   0.00202  -0.1254   0.6783   0.7069
   2.250   0.7735   0.00629   0.00201  -0.1249   0.6639   0.7106
   2.500   0.7993   0.00637   0.00203  -0.1244   0.6490   0.7140
   2.750   0.8249   0.00644   0.00207  -0.1239   0.6360   0.7173
   3.000   0.8503   0.00654   0.00215  -0.1234   0.6238   0.7203
   3.250   0.8754   0.00667   0.00224  -0.1228   0.6103   0.7232
   3.500   0.9006   0.00680   0.00234  -0.1222   0.5969   0.7263
   3.750   0.9258   0.00695   0.00245  -0.1217   0.5844   0.7292
   4.000   0.9509   0.00709   0.00256  -0.1212   0.5726   0.7319
   4.250   0.9751   0.00723   0.00268  -0.1205   0.5594   0.7347
   4.500   0.9983   0.00742   0.00283  -0.1196   0.5410   0.7372
   4.750   1.0202   0.00766   0.00300  -0.1184   0.5187   0.7398
   5.000   1.0423   0.00791   0.00317  -0.1173   0.4995   0.7427
   5.250   1.0648   0.00814   0.00334  -0.1163   0.4793   0.7453
   5.500   1.0861   0.00841   0.00354  -0.1151   0.4566   0.7475
   5.750   1.1054   0.00872   0.00376  -0.1135   0.4297   0.7501
   6.000   1.1224   0.00913   0.00403  -0.1115   0.3955   0.7527
   6.250   1.1364   0.00965   0.00437  -0.1090   0.3561   0.7553
   6.500   1.1470   0.01029   0.00479  -0.1059   0.3105   0.7579
   6.750   1.1572   0.01090   0.00521  -0.1027   0.2710   0.7605
   7.000   1.1642   0.01147   0.00560  -0.0989   0.2377   0.7628
   7.250   1.1736   0.01198   0.00601  -0.0955   0.2112   0.7658
   7.500   1.1831   0.01252   0.00645  -0.0923   0.1885   0.7688
   7.750   1.1945   0.01302   0.00688  -0.0895   0.1707   0.7721
   8.000   1.2052   0.01355   0.00734  -0.0866   0.1526   0.7758
   8.250   1.2156   0.01410   0.00782  -0.0838   0.1362   0.7796
   8.500   1.2238   0.01475   0.00840  -0.0808   0.1178   0.7833
   8.750   1.2318   0.01546   0.00903  -0.0779   0.1008   0.7864
   9.000   1.2402   0.01622   0.00973  -0.0752   0.0851   0.7897
   9.250   1.2488   0.01703   0.01048  -0.0727   0.0722   0.7929
   9.500   1.2583   0.01784   0.01126  -0.0704   0.0620   0.7962
   9.750   1.2681   0.01867   0.01207  -0.0682   0.0543   0.8001
  10.000   1.2797   0.01945   0.01286  -0.0664   0.0489   0.8044
  10.250   1.2914   0.02027   0.01368  -0.0646   0.0441   0.8087
  10.500   1.3030   0.02109   0.01453  -0.0629   0.0405   0.8135
  10.750   1.3141   0.02199   0.01546  -0.0612   0.0372   0.8194
  11.000   1.3280   0.02273   0.01626  -0.0598   0.0355   0.8262
  11.250   1.3396   0.02362   0.01720  -0.0583   0.0333   0.8366
  11.500   1.3490   0.02468   0.01834  -0.0566   0.0307   0.8547
  11.750   1.3796   0.02550   0.01939  -0.0589   0.0291   0.9148
  12.000   1.4272   0.02706   0.02099  -0.0655   0.0264   1.0000
  12.250   1.4381   0.02831   0.02228  -0.0644   0.0249   1.0000
  12.500   1.4522   0.02934   0.02336  -0.0636   0.0238   1.0000
  12.750   1.4643   0.03050   0.02454  -0.0626   0.0227   1.0000
  13.000   1.4746   0.03180   0.02587  -0.0615   0.0218   1.0000
  13.250   1.4797   0.03353   0.02763  -0.0601   0.0205   1.0000
  13.500   1.4908   0.03479   0.02896  -0.0591   0.0200   1.0000
  13.750   1.5016   0.03609   0.03030  -0.0582   0.0193   1.0000
  14.000   1.5116   0.03747   0.03173  -0.0573   0.0184   1.0000
  14.250   1.5195   0.03907   0.03337  -0.0563   0.0178   1.0000
  14.500   1.5244   0.04097   0.03530  -0.0552   0.0171   1.0000
  14.750   1.5252   0.04327   0.03768  -0.0539   0.0164   1.0000
  15.000   1.5346   0.04484   0.03931  -0.0533   0.0160   1.0000
  15.250   1.5423   0.04661   0.04114  -0.0526   0.0155   1.0000
  15.500   1.5491   0.04849   0.04308  -0.0519   0.0150   1.0000
  15.750   1.5539   0.05061   0.04527  -0.0512   0.0146   1.0000
  16.000   1.5576   0.05285   0.04757  -0.0506   0.0142   1.0000
  16.250   1.5582   0.05546   0.05023  -0.0500   0.0136   1.0000
  16.500   1.5542   0.05866   0.05351  -0.0494   0.0133   1.0000
  16.750   1.5546   0.06143   0.05637  -0.0490   0.0129   1.0000
  17.000   1.5575   0.06395   0.05897  -0.0487   0.0127   1.0000
  17.250   1.5591   0.06663   0.06173  -0.0485   0.0124   1.0000
  17.500   1.5577   0.06971   0.06490  -0.0484   0.0122   1.0000
  17.750   1.5578   0.07267   0.06794  -0.0484   0.0119   1.0000
  18.000   1.5566   0.07583   0.07118  -0.0485   0.0117   1.0000
  18.250   1.5543   0.07919   0.07462  -0.0487   0.0114   1.0000
  18.500   1.5494   0.08289   0.07840  -0.0490   0.0112   1.0000
  18.750   1.5438   0.08678   0.08237  -0.0495   0.0110   1.0000
  19.000   1.5354   0.09114   0.08682  -0.0503   0.0108   1.0000
  19.250   1.5246   0.09596   0.09174  -0.0514   0.0107   1.0000
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