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WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 75-141 (fx75141-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.64 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx75141-il-1000000-n5.txt
Download as CSV file: xf-fx75141-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.6674   0.12252   0.11967  -0.0531   0.8149   0.0089
 -17.250  -0.7426   0.10353   0.10050  -0.0634   0.8145   0.0088
 -17.000  -0.8293   0.08375   0.08046  -0.0751   0.8138   0.0085
 -16.500  -0.9185   0.05933   0.05561  -0.0917   0.8097   0.0085
 -16.250  -0.9401   0.05172   0.04781  -0.0976   0.8074   0.0084
 -16.000  -0.9470   0.04676   0.04272  -0.1018   0.8050   0.0085
 -15.750  -0.9497   0.04251   0.03834  -0.1055   0.8025   0.0086
 -15.500  -0.9488   0.03878   0.03448  -0.1090   0.8002   0.0087
 -15.250  -0.9400   0.03602   0.03160  -0.1120   0.7981   0.0087
 -14.750  -0.9193   0.03124   0.02660  -0.1171   0.7943   0.0090
 -14.500  -0.9074   0.02933   0.02460  -0.1188   0.7927   0.0091
 -14.250  -0.8934   0.02770   0.02288  -0.1204   0.7910   0.0093
 -14.000  -0.8796   0.02605   0.02113  -0.1218   0.7892   0.0094
 -13.750  -0.8621   0.02484   0.01984  -0.1229   0.7873   0.0096
 -13.500  -0.8459   0.02353   0.01844  -0.1240   0.7855   0.0098
 -13.250  -0.8277   0.02248   0.01729  -0.1248   0.7838   0.0100
 -13.000  -0.8100   0.02147   0.01620  -0.1255   0.7823   0.0101
 -12.750  -0.7929   0.02055   0.01519  -0.1258   0.7807   0.0103
 -12.500  -0.7806   0.01956   0.01411  -0.1254   0.7791   0.0104
 -12.250  -0.7638   0.01872   0.01323  -0.1251   0.7781   0.0108
 -12.000  -0.7443   0.01808   0.01254  -0.1248   0.7770   0.0112
 -11.750  -0.7238   0.01750   0.01191  -0.1246   0.7758   0.0114
 -11.500  -0.7025   0.01696   0.01132  -0.1243   0.7747   0.0117
 -11.250  -0.6808   0.01642   0.01074  -0.1240   0.7735   0.0120
 -11.000  -0.6583   0.01595   0.01021  -0.1238   0.7722   0.0123
 -10.750  -0.6353   0.01550   0.00971  -0.1235   0.7708   0.0126
 -10.500  -0.6118   0.01508   0.00922  -0.1233   0.7696   0.0129
 -10.250  -0.5881   0.01466   0.00875  -0.1231   0.7685   0.0133
 -10.000  -0.5645   0.01418   0.00824  -0.1229   0.7674   0.0138
  -9.750  -0.5399   0.01380   0.00783  -0.1228   0.7663   0.0144
  -9.500  -0.5147   0.01347   0.00746  -0.1228   0.7652   0.0149
  -9.250  -0.4892   0.01315   0.00710  -0.1228   0.7640   0.0155
  -9.000  -0.4635   0.01285   0.00676  -0.1227   0.7629   0.0161
  -8.750  -0.4379   0.01253   0.00640  -0.1226   0.7620   0.0167
  -8.500  -0.4123   0.01218   0.00604  -0.1226   0.7610   0.0175
  -8.250  -0.3861   0.01188   0.00574  -0.1226   0.7601   0.0184
  -8.000  -0.3597   0.01162   0.00545  -0.1226   0.7590   0.0192
  -7.750  -0.3330   0.01138   0.00518  -0.1226   0.7577   0.0201
  -7.500  -0.3066   0.01109   0.00489  -0.1226   0.7561   0.0213
  -7.250  -0.2800   0.01084   0.00464  -0.1226   0.7544   0.0228
  -7.000  -0.2531   0.01063   0.00440  -0.1226   0.7525   0.0242
  -6.750  -0.2261   0.01041   0.00415  -0.1226   0.7507   0.0256
  -6.500  -0.1990   0.01020   0.00393  -0.1227   0.7488   0.0276
  -6.250  -0.1714   0.01003   0.00374  -0.1228   0.7470   0.0295
  -6.000  -0.1442   0.00981   0.00354  -0.1228   0.7456   0.0323
  -5.750  -0.1167   0.00962   0.00336  -0.1229   0.7441   0.0350
  -5.500  -0.0890   0.00944   0.00318  -0.1230   0.7425   0.0378
  -5.250  -0.0614   0.00926   0.00302  -0.1231   0.7409   0.0417
  -5.000  -0.0336   0.00910   0.00286  -0.1232   0.7391   0.0458
  -4.750  -0.0059   0.00893   0.00271  -0.1233   0.7374   0.0508
  -4.500   0.0219   0.00876   0.00256  -0.1234   0.7357   0.0578
  -4.250   0.0498   0.00861   0.00242  -0.1235   0.7339   0.0654
  -4.000   0.0777   0.00847   0.00230  -0.1236   0.7321   0.0751
  -3.750   0.1055   0.00829   0.00218  -0.1238   0.7303   0.0909
  -3.500   0.1333   0.00810   0.00206  -0.1239   0.7283   0.1090
  -3.250   0.1612   0.00791   0.00196  -0.1240   0.7263   0.1308
  -3.000   0.1889   0.00770   0.00186  -0.1242   0.7241   0.1608
  -2.750   0.2166   0.00750   0.00176  -0.1243   0.7219   0.1932
  -2.500   0.2442   0.00730   0.00166  -0.1244   0.7196   0.2288
  -2.250   0.2715   0.00705   0.00156  -0.1245   0.7172   0.2794
  -2.000   0.2986   0.00676   0.00146  -0.1246   0.7149   0.3439
  -1.750   0.3260   0.00651   0.00140  -0.1247   0.7122   0.4051
  -1.500   0.3534   0.00631   0.00137  -0.1247   0.7089   0.4589
  -1.250   0.3813   0.00621   0.00134  -0.1248   0.7056   0.4890
  -1.000   0.4091   0.00614   0.00131  -0.1248   0.7022   0.5107
  -0.750   0.4371   0.00609   0.00129  -0.1248   0.6988   0.5262
  -0.500   0.4651   0.00602   0.00129  -0.1248   0.6944   0.5494
  -0.250   0.4927   0.00597   0.00129  -0.1248   0.6895   0.5722
   0.000   0.5202   0.00594   0.00129  -0.1247   0.6846   0.5892
   0.250   0.5480   0.00592   0.00132  -0.1246   0.6784   0.6083
   0.500   0.5752   0.00592   0.00135  -0.1244   0.6716   0.6281
   0.750   0.6027   0.00595   0.00140  -0.1243   0.6638   0.6421
   1.000   0.6298   0.00600   0.00141  -0.1241   0.6552   0.6503
   1.250   0.6570   0.00605   0.00146  -0.1240   0.6453   0.6559
   1.500   0.6835   0.00612   0.00150  -0.1237   0.6340   0.6613
   1.750   0.7091   0.00625   0.00155  -0.1232   0.6181   0.6662
   2.000   0.7328   0.00643   0.00164  -0.1223   0.5959   0.6703
   2.250   0.7563   0.00664   0.00176  -0.1214   0.5714   0.6743
   2.500   0.7804   0.00684   0.00187  -0.1206   0.5509   0.6784
   2.750   0.8058   0.00700   0.00197  -0.1202   0.5374   0.6821
   3.000   0.8315   0.00712   0.00208  -0.1197   0.5278   0.6852
   3.250   0.8567   0.00726   0.00220  -0.1192   0.5161   0.6882
   3.500   0.8820   0.00740   0.00232  -0.1188   0.5037   0.6913
   3.750   0.9068   0.00757   0.00244  -0.1182   0.4907   0.6944
   4.000   0.9313   0.00774   0.00258  -0.1176   0.4772   0.6975
   4.250   0.9555   0.00792   0.00272  -0.1169   0.4637   0.6999
   4.500   0.9769   0.00821   0.00292  -0.1157   0.4382   0.7023
   4.750   0.9937   0.00869   0.00320  -0.1136   0.3936   0.7048
   5.000   1.0076   0.00930   0.00356  -0.1111   0.3424   0.7076
   5.250   1.0218   0.00988   0.00392  -0.1087   0.2972   0.7103
   5.500   1.0363   0.01044   0.00429  -0.1063   0.2584   0.7127
   5.750   1.0505   0.01098   0.00465  -0.1039   0.2236   0.7149
   6.000   1.0662   0.01139   0.00497  -0.1017   0.2011   0.7172
   6.250   1.0807   0.01173   0.00525  -0.0992   0.1836   0.7195
   6.500   1.0944   0.01212   0.00557  -0.0967   0.1661   0.7218
   6.750   1.1093   0.01251   0.00591  -0.0944   0.1513   0.7241
   7.000   1.1236   0.01291   0.00626  -0.0920   0.1376   0.7265
   7.250   1.1374   0.01335   0.00663  -0.0896   0.1238   0.7290
   7.750   1.1611   0.01437   0.00754  -0.0844   0.0939   0.7350
   8.000   1.1717   0.01495   0.00807  -0.0817   0.0804   0.7387
   8.250   1.1835   0.01552   0.00860  -0.0793   0.0703   0.7421
   8.500   1.1945   0.01617   0.00920  -0.0769   0.0601   0.7447
   8.750   1.2065   0.01681   0.00982  -0.0748   0.0530   0.7468
   9.000   1.2193   0.01742   0.01044  -0.0728   0.0479   0.7489
   9.250   1.2326   0.01805   0.01108  -0.0710   0.0437   0.7511
   9.500   1.2458   0.01871   0.01175  -0.0693   0.0401   0.7537
   9.750   1.2591   0.01940   0.01245  -0.0676   0.0372   0.7563
  10.000   1.2731   0.02008   0.01315  -0.0661   0.0345   0.7588
  10.250   1.2857   0.02086   0.01393  -0.0645   0.0315   0.7612
  10.750   1.3127   0.02236   0.01549  -0.0616   0.0276   0.7662
  11.000   1.3254   0.02318   0.01633  -0.0601   0.0261   0.7693
  11.250   1.3383   0.02401   0.01720  -0.0587   0.0248   0.7728
  11.500   1.3515   0.02483   0.01808  -0.0574   0.0236   0.7764
  11.750   1.3640   0.02572   0.01900  -0.0561   0.0225   0.7799
  12.000   1.3756   0.02668   0.01999  -0.0547   0.0212   0.7841
  12.250   1.3872   0.02766   0.02102  -0.0534   0.0203   0.7887
  12.500   1.3993   0.02863   0.02204  -0.0522   0.0192   0.7937
  12.750   1.4109   0.02964   0.02312  -0.0509   0.0184   0.8001
  13.000   1.4214   0.03075   0.02429  -0.0497   0.0176   0.8078
  13.250   1.4314   0.03192   0.02552  -0.0485   0.0167   0.8189
  13.500   1.4420   0.03307   0.02678  -0.0474   0.0161   0.8390
  13.750   1.4697   0.03442   0.02837  -0.0500   0.0154   0.9080
  14.000   1.5211   0.03663   0.03068  -0.0583   0.0139   0.9536
  14.500   1.5379   0.03970   0.03383  -0.0562   0.0129   1.0000
  14.750   1.5465   0.04129   0.03548  -0.0554   0.0125   1.0000
  15.000   1.5546   0.04292   0.03716  -0.0545   0.0120   1.0000
  15.250   1.5616   0.04470   0.03900  -0.0537   0.0117   1.0000
  15.500   1.5679   0.04656   0.04092  -0.0530   0.0112   1.0000
  15.750   1.5734   0.04857   0.04298  -0.0522   0.0109   1.0000
  16.000   1.5776   0.05073   0.04519  -0.0516   0.0105   1.0000
  16.250   1.5819   0.05289   0.04742  -0.0509   0.0101   1.0000
  16.500   1.5861   0.05511   0.04971  -0.0504   0.0100   1.0000
  16.750   1.5897   0.05743   0.05210  -0.0499   0.0097   1.0000
  17.000   1.5928   0.05985   0.05459  -0.0495   0.0094   1.0000
  17.250   1.5949   0.06241   0.05722  -0.0492   0.0091   1.0000
  17.500   1.5954   0.06514   0.06003  -0.0489   0.0090   1.0000
  17.750   1.5951   0.06803   0.06300  -0.0487   0.0087   1.0000
  18.000   1.5941   0.07104   0.06608  -0.0486   0.0085   1.0000
  18.250   1.5915   0.07431   0.06942  -0.0486   0.0083   1.0000
  18.500   1.5882   0.07771   0.07290  -0.0487   0.0081   1.0000
  18.750   1.5835   0.08133   0.07660  -0.0490   0.0079   1.0000
  19.000   1.5794   0.08492   0.08029  -0.0494   0.0078   1.0000
  19.250   1.5753   0.08861   0.08407  -0.0499   0.0077   1.0000
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