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WORTMANN FX 76-100 (fx76100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 76-100 (fx76100-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.13 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx76100-il-1000000.txt
Download as CSV file: xf-fx76100-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 76-100                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.1030   0.09848   0.09586  -0.0035   1.0000   0.0092
 -16.750  -1.1315   0.08944   0.08670  -0.0084   1.0000   0.0091
 -16.500  -1.1691   0.07918   0.07627  -0.0140   1.0000   0.0091
 -16.000  -1.1997   0.06581   0.06269  -0.0218   1.0000   0.0091
 -15.750  -1.2268   0.05728   0.05395  -0.0271   1.0000   0.0093
 -15.500  -1.2283   0.05304   0.04963  -0.0299   1.0000   0.0092
 -15.250  -1.2413   0.04734   0.04376  -0.0334   1.0000   0.0092
 -15.000  -1.2587   0.04157   0.03781  -0.0365   1.0000   0.0092
 -14.750  -1.2846   0.03574   0.03174  -0.0382   1.0000   0.0095
 -14.500  -1.2888   0.03298   0.02884  -0.0380   1.0000   0.0095
 -14.250  -1.2932   0.03054   0.02630  -0.0370   1.0000   0.0099
 -14.000  -1.2908   0.02887   0.02451  -0.0355   1.0000   0.0097
 -13.750  -1.2907   0.02719   0.02272  -0.0333   1.0000   0.0101
 -13.500  -1.2837   0.02609   0.02155  -0.0313   1.0000   0.0103
 -13.250  -1.2749   0.02518   0.02057  -0.0292   1.0000   0.0105
 -13.000  -1.2663   0.02431   0.01962  -0.0267   1.0000   0.0107
 -12.750  -1.2562   0.02343   0.01866  -0.0244   1.0000   0.0110
 -12.500  -1.2411   0.02270   0.01786  -0.0228   1.0000   0.0113
 -12.250  -1.2272   0.02186   0.01693  -0.0210   1.0000   0.0116
 -12.000  -1.2125   0.02103   0.01601  -0.0193   1.0000   0.0117
 -11.750  -1.1926   0.02060   0.01551  -0.0182   1.0000   0.0121
 -11.500  -1.1820   0.01938   0.01417  -0.0158   1.0000   0.0126
 -11.250  -1.1673   0.01846   0.01318  -0.0139   1.0000   0.0130
 -11.000  -1.1475   0.01798   0.01269  -0.0127   1.0000   0.0137
 -10.750  -1.1286   0.01740   0.01205  -0.0114   1.0000   0.0143
 -10.500  -1.1085   0.01693   0.01153  -0.0101   1.0000   0.0148
 -10.250  -1.0875   0.01653   0.01107  -0.0090   1.0000   0.0154
 -10.000  -1.0671   0.01609   0.01057  -0.0077   1.0000   0.0158
  -9.750  -1.0522   0.01515   0.00957  -0.0056   1.0000   0.0169
  -9.500  -1.0320   0.01471   0.00912  -0.0043   1.0000   0.0179
  -9.250  -1.0113   0.01433   0.00871  -0.0030   1.0000   0.0188
  -9.000  -0.9904   0.01399   0.00833  -0.0017   1.0000   0.0196
  -8.750  -0.9690   0.01371   0.00800  -0.0004   1.0000   0.0201
  -8.500  -0.9521   0.01303   0.00729   0.0016   1.0000   0.0220
  -8.250  -0.9316   0.01271   0.00696   0.0030   1.0000   0.0233
  -8.000  -0.9110   0.01243   0.00666   0.0044   1.0000   0.0246
  -7.750  -0.8899   0.01222   0.00641   0.0057   1.0000   0.0255
  -7.500  -0.8723   0.01168   0.00585   0.0077   1.0000   0.0279
  -7.250  -0.8526   0.01138   0.00555   0.0093   1.0000   0.0297
  -7.000  -0.8324   0.01114   0.00528   0.0108   1.0000   0.0313
  -6.750  -0.8123   0.01089   0.00501   0.0123   1.0000   0.0332
  -6.500  -0.7925   0.01054   0.00467   0.0139   1.0000   0.0368
  -6.250  -0.7583   0.01030   0.00443   0.0124   0.9985   0.0399
  -6.000  -0.7251   0.00994   0.00410   0.0112   0.9968   0.0465
  -5.750  -0.6921   0.00966   0.00384   0.0099   0.9950   0.0535
  -5.500  -0.6600   0.00932   0.00356   0.0089   0.9928   0.0651
  -5.250  -0.6271   0.00896   0.00330   0.0077   0.9909   0.0826
  -5.000  -0.5935   0.00860   0.00306   0.0063   0.9893   0.1065
  -4.750  -0.5612   0.00825   0.00284   0.0052   0.9863   0.1336
  -4.500  -0.5257   0.00796   0.00265   0.0035   0.9835   0.1567
  -4.250  -0.4893   0.00768   0.00248   0.0016   0.9816   0.1785
  -4.000  -0.4573   0.00745   0.00232   0.0007   0.9784   0.1988
  -3.750  -0.4245   0.00724   0.00217  -0.0003   0.9748   0.2172
  -3.500  -0.3881   0.00698   0.00202  -0.0022   0.9720   0.2399
  -3.250  -0.3543   0.00677   0.00188  -0.0034   0.9668   0.2619
  -3.000  -0.3192   0.00652   0.00174  -0.0050   0.9614   0.2912
  -2.750  -0.2850   0.00628   0.00162  -0.0064   0.9553   0.3213
  -2.500  -0.2514   0.00605   0.00150  -0.0076   0.9464   0.3552
  -2.250  -0.2215   0.00581   0.00140  -0.0080   0.9353   0.3944
  -2.000  -0.1921   0.00560   0.00130  -0.0083   0.9226   0.4346
  -1.750  -0.1646   0.00541   0.00122  -0.0081   0.9086   0.4753
  -1.500  -0.1387   0.00523   0.00115  -0.0075   0.8925   0.5165
  -1.250  -0.1134   0.00510   0.00109  -0.0068   0.8744   0.5551
  -1.000  -0.0894   0.00496   0.00104  -0.0058   0.8542   0.5962
  -0.750  -0.0659   0.00488   0.00100  -0.0046   0.8293   0.6317
  -0.500  -0.0433   0.00481   0.00096  -0.0032   0.8026   0.6671
  -0.250  -0.0218   0.00476   0.00094  -0.0016   0.7712   0.7048
   0.000  -0.0001   0.00475   0.00093   0.0000   0.7388   0.7399
   0.250   0.0217   0.00476   0.00094   0.0016   0.7060   0.7733
   0.500   0.0435   0.00480   0.00096   0.0032   0.6693   0.8035
   0.750   0.0659   0.00487   0.00100   0.0046   0.6321   0.8298
   1.000   0.0892   0.00497   0.00104   0.0058   0.5937   0.8536
   1.250   0.1134   0.00510   0.00109   0.0068   0.5555   0.8742
   1.500   0.1387   0.00523   0.00115   0.0075   0.5169   0.8922
   1.750   0.1645   0.00542   0.00122   0.0081   0.4727   0.9091
   2.000   0.1921   0.00561   0.00131   0.0083   0.4334   0.9230
   2.250   0.2216   0.00580   0.00140   0.0080   0.3987   0.9351
   2.500   0.2514   0.00604   0.00150   0.0076   0.3554   0.9463
   2.750   0.2850   0.00629   0.00161   0.0064   0.3194   0.9552
   3.000   0.3194   0.00652   0.00174   0.0050   0.2914   0.9615
   3.250   0.3543   0.00676   0.00187   0.0035   0.2630   0.9667
   3.500   0.3883   0.00698   0.00202   0.0022   0.2401   0.9720
   3.750   0.4247   0.00724   0.00217   0.0003   0.2171   0.9749
   4.000   0.4573   0.00745   0.00232  -0.0007   0.1987   0.9784
   4.250   0.4894   0.00768   0.00247  -0.0016   0.1795   0.9816
   4.500   0.5256   0.00796   0.00265  -0.0035   0.1564   0.9835
   4.750   0.5613   0.00824   0.00284  -0.0052   0.1339   0.9863
   5.000   0.5936   0.00861   0.00307  -0.0063   0.1054   0.9893
   5.250   0.6273   0.00897   0.00331  -0.0077   0.0817   0.9909
   5.500   0.6600   0.00934   0.00357  -0.0089   0.0637   0.9929
   5.750   0.6920   0.00967   0.00384  -0.0099   0.0528   0.9950
   6.000   0.7252   0.00995   0.00411  -0.0112   0.0462   0.9968
   6.250   0.7583   0.01031   0.00443  -0.0124   0.0399   0.9986
   6.500   0.7926   0.01055   0.00468  -0.0139   0.0367   1.0000
   6.750   0.8120   0.01090   0.00501  -0.0123   0.0329   1.0000
   7.000   0.8322   0.01114   0.00528  -0.0108   0.0313   1.0000
   7.250   0.8524   0.01139   0.00555  -0.0092   0.0297   1.0000
   7.500   0.8722   0.01169   0.00585  -0.0077   0.0279   1.0000
   7.750   0.8895   0.01225   0.00644  -0.0056   0.0255   1.0000
   8.000   0.9105   0.01246   0.00670  -0.0043   0.0247   1.0000
   8.250   0.9315   0.01272   0.00697  -0.0029   0.0235   1.0000
   8.500   0.9519   0.01305   0.00732  -0.0015   0.0222   1.0000
   8.750   0.9699   0.01363   0.00791   0.0003   0.0204   1.0000
   9.000   0.9902   0.01401   0.00835   0.0017   0.0197   1.0000
   9.250   1.0110   0.01436   0.00874   0.0030   0.0189   1.0000
   9.500   1.0321   0.01470   0.00911   0.0043   0.0180   1.0000
   9.750   1.0524   0.01513   0.00955   0.0056   0.0171   1.0000
  10.000   1.0687   0.01594   0.01042   0.0075   0.0159   1.0000
  10.250   1.0887   0.01643   0.01097   0.0088   0.0154   1.0000
  10.500   1.1088   0.01691   0.01152   0.0101   0.0148   1.0000
  10.750   1.1289   0.01738   0.01203   0.0113   0.0142   1.0000
  11.000   1.1497   0.01779   0.01246   0.0124   0.0135   1.0000
  11.250   1.1680   0.01841   0.01313   0.0138   0.0130   1.0000
  11.500   1.1808   0.01950   0.01429   0.0159   0.0123   1.0000
  11.750   1.1953   0.02040   0.01530   0.0178   0.0120   1.0000
  12.000   1.2132   0.02100   0.01598   0.0192   0.0117   1.0000
  12.250   1.2290   0.02174   0.01680   0.0208   0.0114   1.0000
  12.500   1.2439   0.02252   0.01767   0.0225   0.0112   1.0000
  12.750   1.2587   0.02327   0.01848   0.0241   0.0108   1.0000
  13.000   1.2703   0.02411   0.01940   0.0262   0.0106   1.0000
  13.250   1.2773   0.02508   0.02045   0.0288   0.0104   1.0000
  13.500   1.2873   0.02591   0.02134   0.0309   0.0101   1.0000
  13.750   1.2914   0.02720   0.02272   0.0332   0.0099   1.0000
  14.000   1.2944   0.02866   0.02429   0.0352   0.0098   1.0000
  14.250   1.2924   0.03067   0.02640   0.0369   0.0096   1.0000
  14.500   1.2876   0.03317   0.02905   0.0379   0.0095   1.0000
  14.750   1.2781   0.03655   0.03258   0.0379   0.0093   1.0000
  15.000   1.2543   0.04230   0.03856   0.0360   0.0092   1.0000
  15.250   1.2454   0.04697   0.04339   0.0334   0.0091   1.0000
  15.500   1.2449   0.05082   0.04735   0.0309   0.0090   1.0000
  15.750   1.2257   0.05779   0.05449   0.0265   0.0091   1.0000
  16.000   1.2112   0.06434   0.06119   0.0223   0.0090   1.0000
  16.250   1.1902   0.07187   0.06886   0.0178   0.0091   1.0000
  16.500   1.1704   0.07930   0.07641   0.0136   0.0090   1.0000
  17.000   1.1143   0.09695   0.09430   0.0039   0.0091   1.0000
  17.250   1.0865   0.10622   0.10369  -0.0011   0.0091   1.0000
  17.500   1.0594   0.11560   0.11319  -0.0061   0.0092   1.0000
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