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WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 73-170 (fx73170-il)
Reynolds number: 1,000,000
Max Cl/Cd: 147.35 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx73170-il-1000000-n5.txt
Download as CSV file: xf-fx73170-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 73-170                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.5449   0.06863   0.06522  -0.1140   0.7411   0.0055
 -15.000  -0.5322   0.06581   0.06236  -0.1169   0.7397   0.0055
 -14.750  -0.5931   0.04989   0.04606  -0.1296   0.7388   0.0055
 -14.500  -0.5938   0.04608   0.04215  -0.1329   0.7379   0.0056
 -14.250  -0.6117   0.04052   0.03635  -0.1366   0.7368   0.0055
 -14.000  -0.6037   0.03838   0.03415  -0.1384   0.7353   0.0056
 -13.750  -0.6029   0.03549   0.03111  -0.1403   0.7338   0.0056
 -13.500  -0.6067   0.03224   0.02765  -0.1418   0.7322   0.0055
 -13.250  -0.5975   0.03040   0.02572  -0.1429   0.7304   0.0057
 -13.000  -0.5846   0.02896   0.02420  -0.1439   0.7290   0.0057
 -12.750  -0.5716   0.02756   0.02268  -0.1446   0.7276   0.0056
 -12.500  -0.5630   0.02573   0.02071  -0.1452   0.7261   0.0059
 -12.250  -0.5454   0.02481   0.01972  -0.1457   0.7246   0.0059
 -12.000  -0.5262   0.02408   0.01893  -0.1463   0.7232   0.0060
 -11.750  -0.5147   0.02266   0.01740  -0.1463   0.7221   0.0061
 -11.500  -0.5021   0.02141   0.01603  -0.1461   0.7209   0.0059
 -11.250  -0.4843   0.02069   0.01527  -0.1460   0.7194   0.0063
 -11.000  -0.4707   0.01969   0.01418  -0.1455   0.7178   0.0061
 -10.750  -0.4560   0.01892   0.01335  -0.1448   0.7162   0.0064
 -10.500  -0.4447   0.01816   0.01250  -0.1434   0.7146   0.0065
 -10.250  -0.4277   0.01762   0.01189  -0.1426   0.7132   0.0067
 -10.000  -0.4111   0.01693   0.01111  -0.1416   0.7119   0.0068
  -9.750  -0.3925   0.01637   0.01048  -0.1409   0.7105   0.0068
  -9.500  -0.3723   0.01590   0.00994  -0.1403   0.7091   0.0071
  -9.250  -0.3514   0.01546   0.00943  -0.1398   0.7078   0.0072
  -9.000  -0.3293   0.01508   0.00901  -0.1394   0.7067   0.0074
  -8.750  -0.3089   0.01453   0.00840  -0.1387   0.7053   0.0074
  -8.500  -0.2886   0.01395   0.00778  -0.1381   0.7040   0.0076
  -8.250  -0.2665   0.01351   0.00730  -0.1377   0.7026   0.0078
  -8.000  -0.2435   0.01312   0.00689  -0.1373   0.7013   0.0081
  -7.750  -0.2195   0.01282   0.00656  -0.1371   0.7000   0.0084
  -7.500  -0.1952   0.01252   0.00622  -0.1369   0.6987   0.0088
  -7.250  -0.1708   0.01222   0.00589  -0.1367   0.6975   0.0090
  -7.000  -0.1462   0.01193   0.00556  -0.1365   0.6962   0.0093
  -6.750  -0.1213   0.01166   0.00525  -0.1364   0.6948   0.0096
  -6.500  -0.0959   0.01144   0.00498  -0.1363   0.6934   0.0100
  -6.250  -0.0706   0.01115   0.00468  -0.1362   0.6922   0.0103
  -6.000  -0.0452   0.01086   0.00438  -0.1362   0.6910   0.0111
  -5.750  -0.0189   0.01067   0.00419  -0.1363   0.6898   0.0120
  -5.500   0.0076   0.01047   0.00397  -0.1363   0.6886   0.0130
  -5.250   0.0339   0.01025   0.00375  -0.1364   0.6874   0.0139
  -5.000   0.0604   0.01005   0.00355  -0.1364   0.6862   0.0150
  -4.750   0.0872   0.00989   0.00336  -0.1365   0.6848   0.0163
  -4.500   0.1139   0.00971   0.00318  -0.1366   0.6835   0.0186
  -4.250   0.1406   0.00955   0.00302  -0.1367   0.6821   0.0221
  -4.000   0.1673   0.00938   0.00287  -0.1368   0.6807   0.0283
  -3.750   0.1940   0.00921   0.00273  -0.1369   0.6793   0.0381
  -3.500   0.2208   0.00907   0.00261  -0.1370   0.6780   0.0510
  -3.250   0.2473   0.00884   0.00248  -0.1371   0.6770   0.0763
  -3.000   0.2731   0.00854   0.00234  -0.1371   0.6759   0.1226
  -2.750   0.2986   0.00823   0.00221  -0.1371   0.6746   0.1809
  -2.500   0.3228   0.00779   0.00206  -0.1369   0.6732   0.2689
  -2.250   0.3458   0.00730   0.00189  -0.1366   0.6718   0.3759
  -2.000   0.3641   0.00660   0.00178  -0.1352   0.6702   0.5656
  -1.750   0.3919   0.00662   0.00181  -0.1354   0.6688   0.5861
  -1.500   0.4199   0.00668   0.00187  -0.1355   0.6675   0.6043
  -1.250   0.4482   0.00674   0.00189  -0.1357   0.6662   0.6136
  -1.000   0.4761   0.00680   0.00195  -0.1359   0.6649   0.6211
  -0.750   0.5043   0.00688   0.00199  -0.1361   0.6635   0.6263
  -0.500   0.5325   0.00693   0.00202  -0.1363   0.6622   0.6299
  -0.250   0.5605   0.00694   0.00203  -0.1365   0.6609   0.6322
   0.000   0.5885   0.00695   0.00205  -0.1368   0.6595   0.6339
   0.250   0.6165   0.00697   0.00207  -0.1370   0.6581   0.6349
   0.500   0.6445   0.00699   0.00209  -0.1372   0.6567   0.6359
   0.750   0.6723   0.00701   0.00210  -0.1374   0.6551   0.6368
   1.000   0.7000   0.00703   0.00212  -0.1376   0.6535   0.6377
   1.250   0.7276   0.00706   0.00214  -0.1377   0.6520   0.6386
   1.500   0.7552   0.00710   0.00217  -0.1379   0.6504   0.6395
   1.750   0.7827   0.00715   0.00220  -0.1381   0.6488   0.6405
   2.000   0.8103   0.00718   0.00225  -0.1382   0.6474   0.6416
   2.250   0.8377   0.00721   0.00230  -0.1384   0.6459   0.6426
   2.500   0.8651   0.00724   0.00235  -0.1385   0.6443   0.6434
   2.750   0.8923   0.00727   0.00240  -0.1386   0.6423   0.6443
   3.000   0.9193   0.00731   0.00246  -0.1387   0.6403   0.6450
   3.250   0.9460   0.00735   0.00251  -0.1387   0.6381   0.6457
   3.500   0.9722   0.00740   0.00255  -0.1386   0.6353   0.6464
   3.750   0.9982   0.00744   0.00261  -0.1384   0.6321   0.6472
   4.000   1.0237   0.00746   0.00267  -0.1381   0.6271   0.6482
   4.250   1.0488   0.00750   0.00273  -0.1378   0.6230   0.6492
   4.500   1.0730   0.00756   0.00280  -0.1373   0.6183   0.6504
   4.750   1.0977   0.00760   0.00289  -0.1369   0.6120   0.6514
   5.000   1.1205   0.00768   0.00297  -0.1361   0.6056   0.6524
   5.250   1.1434   0.00776   0.00307  -0.1353   0.5971   0.6533
   5.500   1.1623   0.00789   0.00318  -0.1337   0.5835   0.6543
   5.750   1.1783   0.00808   0.00333  -0.1315   0.5667   0.6553
   6.000   1.1845   0.00837   0.00353  -0.1272   0.5439   0.6563
   6.250   1.1824   0.00888   0.00390  -0.1214   0.5105   0.6573
   6.500   1.1771   0.00960   0.00446  -0.1153   0.4761   0.6585
   6.750   1.1667   0.01060   0.00528  -0.1086   0.4393   0.6595
   7.000   1.1519   0.01209   0.00657  -0.1021   0.3962   0.6606
   7.250   1.1481   0.01356   0.00790  -0.0981   0.3631   0.6615
   7.500   1.1517   0.01488   0.00911  -0.0955   0.3367   0.6624
   7.750   1.1474   0.01678   0.01082  -0.0922   0.2971   0.6634
   8.000   1.1494   0.01842   0.01232  -0.0899   0.2636   0.6650
   8.250   1.1531   0.02000   0.01376  -0.0878   0.2332   0.6661
   8.500   1.1586   0.02148   0.01513  -0.0860   0.2072   0.6672
   8.750   1.1643   0.02297   0.01650  -0.0843   0.1802   0.6684
   9.000   1.1732   0.02427   0.01772  -0.0829   0.1601   0.6695
   9.250   1.1820   0.02559   0.01897  -0.0816   0.1398   0.6707
   9.500   1.1887   0.02711   0.02037  -0.0800   0.1167   0.6717
   9.750   1.1998   0.02834   0.02155  -0.0790   0.1018   0.6729
  10.000   1.2089   0.02974   0.02288  -0.0779   0.0852   0.6740
  10.250   1.2220   0.03089   0.02400  -0.0771   0.0754   0.6752
  10.500   1.2320   0.03227   0.02532  -0.0760   0.0621   0.6762
  10.750   1.2442   0.03351   0.02654  -0.0752   0.0541   0.6773
  11.000   1.2560   0.03477   0.02776  -0.0744   0.0463   0.6783
  11.250   1.2692   0.03599   0.02899  -0.0738   0.0411   0.6794
  11.500   1.2829   0.03726   0.03026  -0.0733   0.0366   0.6807
  11.750   1.2970   0.03847   0.03149  -0.0729   0.0333   0.6821
  12.000   1.3106   0.03968   0.03273  -0.0724   0.0304   0.6834
  12.250   1.3246   0.04092   0.03401  -0.0720   0.0285   0.6850
  12.500   1.3374   0.04226   0.03535  -0.0715   0.0259   0.6867
  12.750   1.3501   0.04358   0.03670  -0.0710   0.0239   0.6885
  13.000   1.3639   0.04484   0.03801  -0.0706   0.0226   0.6899
  13.250   1.3754   0.04627   0.03947  -0.0700   0.0209   0.6915
  13.500   1.3868   0.04770   0.04092  -0.0694   0.0194   0.6932
  13.750   1.3987   0.04909   0.04235  -0.0689   0.0179   0.6945
  14.000   1.4102   0.05064   0.04394  -0.0685   0.0166   0.6962
  14.250   1.4216   0.05221   0.04555  -0.0682   0.0156   0.6981
  14.500   1.4329   0.05378   0.04716  -0.0678   0.0144   0.7000
  14.750   1.4437   0.05541   0.04885  -0.0675   0.0135   0.7020
  15.000   1.4537   0.05708   0.05058  -0.0671   0.0130   0.7041
  15.250   1.4620   0.05889   0.05241  -0.0665   0.0115   0.7060
  15.500   1.4714   0.06066   0.05424  -0.0662   0.0108   0.7082
  15.750   1.4800   0.06249   0.05612  -0.0657   0.0101   0.7102
  16.000   1.4892   0.06435   0.05805  -0.0655   0.0096   0.7125
  16.250   1.4969   0.06641   0.06018  -0.0653   0.0092   0.7152
  16.500   1.5040   0.06849   0.06232  -0.0650   0.0084   0.7179
  16.750   1.5109   0.07060   0.06449  -0.0647   0.0077   0.7207
  17.000   1.5166   0.07284   0.06679  -0.0644   0.0073   0.7237
  17.500   1.5270   0.07760   0.07169  -0.0642   0.0065   0.7302
  17.750   1.5322   0.08004   0.07421  -0.0641   0.0062   0.7345
  18.000   1.5368   0.08257   0.07684  -0.0641   0.0059   0.7388
  18.250   1.5416   0.08514   0.07949  -0.0642   0.0056   0.7440
  18.500   1.5450   0.08790   0.08235  -0.0645   0.0054   0.7495
  18.750   1.5473   0.09078   0.08531  -0.0647   0.0050   0.7557
  19.000   1.5498   0.09382   0.08845  -0.0652   0.0050   0.7627
  19.250   1.5528   0.09686   0.09159  -0.0658   0.0048   0.7716
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