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FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 60-177 AIRFOIL (fx60177-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.52 at α=1.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx60177-il-1000000.txt
Download as CSV file: xf-fx60177-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 60-177 AIRFOIL                               
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.6979   0.12361   0.12136  -0.0562   1.0001   0.0053
 -17.750  -0.7341   0.11247   0.11006  -0.0612   1.0001   0.0052
 -17.500  -0.7632   0.10326   0.10070  -0.0654   1.0001   0.0052
 -17.250  -0.7847   0.09418   0.09146  -0.0710   0.9997   0.0052
 -17.000  -0.8025   0.08615   0.08326  -0.0761   0.9993   0.0051
 -16.750  -0.8165   0.07900   0.07594  -0.0808   0.9987   0.0051
 -16.500  -0.8275   0.07265   0.06943  -0.0849   0.9980   0.0051
 -16.250  -0.8354   0.06697   0.06360  -0.0886   0.9972   0.0050
 -16.000  -0.8404   0.06198   0.05845  -0.0919   0.9965   0.0050
 -15.750  -0.8430   0.05746   0.05378  -0.0948   0.9957   0.0050
 -15.500  -0.8417   0.05352   0.04970  -0.0975   0.9950   0.0050
 -15.250  -0.8386   0.04993   0.04598  -0.0999   0.9944   0.0050
 -15.000  -0.8338   0.04688   0.04281  -0.1017   0.9933   0.0050
 -14.750  -0.8286   0.04413   0.03994  -0.1029   0.9914   0.0050
 -14.500  -0.8206   0.04159   0.03729  -0.1042   0.9898   0.0050
 -14.250  -0.8099   0.03929   0.03489  -0.1057   0.9884   0.0050
 -14.000  -0.7976   0.03717   0.03267  -0.1071   0.9872   0.0051
 -13.750  -0.7836   0.03520   0.03060  -0.1086   0.9862   0.0051
 -13.500  -0.7679   0.03335   0.02866  -0.1101   0.9853   0.0051
 -13.250  -0.7509   0.03163   0.02685  -0.1116   0.9846   0.0051
 -13.000  -0.7328   0.02997   0.02511  -0.1132   0.9839   0.0051
 -12.750  -0.7235   0.02859   0.02366  -0.1125   0.9799   0.0051
 -12.500  -0.7075   0.02719   0.02218  -0.1131   0.9776   0.0051
 -12.250  -0.6882   0.02585   0.02077  -0.1142   0.9761   0.0051
 -12.000  -0.6668   0.02457   0.01942  -0.1156   0.9749   0.0052
 -11.750  -0.6434   0.02337   0.01815  -0.1171   0.9740   0.0052
 -11.500  -0.6193   0.02222   0.01695  -0.1187   0.9731   0.0052
 -11.250  -0.5946   0.02120   0.01587  -0.1202   0.9722   0.0052
 -11.000  -0.5804   0.02037   0.01499  -0.1193   0.9678   0.0052
 -10.750  -0.5605   0.01955   0.01413  -0.1193   0.9646   0.0052
 -10.500  -0.5373   0.01871   0.01324  -0.1200   0.9623   0.0053
 -10.250  -0.5131   0.01794   0.01242  -0.1208   0.9603   0.0053
 -10.000  -0.4882   0.01723   0.01167  -0.1216   0.9583   0.0054
  -9.750  -0.4747   0.01671   0.01111  -0.1199   0.9529   0.0054
  -9.500  -0.4529   0.01611   0.01048  -0.1199   0.9494   0.0055
  -9.250  -0.4290   0.01554   0.00987  -0.1202   0.9466   0.0055
  -9.000  -0.4052   0.01502   0.00931  -0.1204   0.9435   0.0056
  -8.750  -0.3894   0.01457   0.00884  -0.1190   0.9382   0.0058
  -8.500  -0.3673   0.01410   0.00834  -0.1187   0.9345   0.0060
  -8.250  -0.3433   0.01365   0.00787  -0.1189   0.9315   0.0064
  -8.000  -0.3219   0.01329   0.00749  -0.1184   0.9278   0.0069
  -7.750  -0.3054   0.01297   0.00716  -0.1169   0.9229   0.0079
  -7.500  -0.2817   0.01257   0.00676  -0.1169   0.9194   0.0107
  -7.250  -0.2555   0.01217   0.00635  -0.1174   0.9165   0.0145
  -7.000  -0.2315   0.01181   0.00601  -0.1175   0.9129   0.0194
  -6.750  -0.2098   0.01140   0.00566  -0.1172   0.9086   0.0301
  -6.500  -0.1836   0.01100   0.00531  -0.1177   0.9051   0.0410
  -6.250  -0.1543   0.01063   0.00497  -0.1188   0.9021   0.0530
  -6.000  -0.1288   0.01010   0.00459  -0.1195   0.8982   0.0851
  -5.750  -0.1051   0.00962   0.00427  -0.1196   0.8937   0.1216
  -5.500  -0.0778   0.00905   0.00389  -0.1205   0.8897   0.1725
  -5.250  -0.0468   0.00828   0.00345  -0.1226   0.8861   0.2552
  -5.000  -0.0184   0.00752   0.00306  -0.1241   0.8819   0.3496
  -4.750   0.0140   0.00690   0.00274  -0.1261   0.8780   0.4299
  -4.500   0.0498   0.00638   0.00246  -0.1287   0.8743   0.5030
  -4.250   0.0868   0.00610   0.00230  -0.1311   0.8704   0.5513
  -4.000   0.1164   0.00596   0.00224  -0.1317   0.8653   0.5767
  -3.750   0.1482   0.00587   0.00221  -0.1327   0.8606   0.6064
  -3.500   0.1812   0.00586   0.00219  -0.1339   0.8565   0.6247
  -3.250   0.2111   0.00586   0.00216  -0.1344   0.8516   0.6327
  -3.000   0.2402   0.00585   0.00215  -0.1347   0.8460   0.6399
  -2.750   0.2720   0.00587   0.00210  -0.1356   0.8410   0.6466
  -2.500   0.3008   0.00589   0.00214  -0.1359   0.8358   0.6527
  -2.250   0.3302   0.00591   0.00213  -0.1363   0.8300   0.6581
  -2.000   0.3609   0.00593   0.00208  -0.1370   0.8234   0.6620
  -1.750   0.3882   0.00593   0.00209  -0.1369   0.8149   0.6654
  -1.500   0.4175   0.00598   0.00209  -0.1372   0.8076   0.6687
  -1.250   0.4463   0.00601   0.00211  -0.1375   0.8006   0.6728
  -1.000   0.4764   0.00607   0.00211  -0.1381   0.7941   0.6764
  -0.750   0.5045   0.00608   0.00214  -0.1382   0.7870   0.6796
  -0.500   0.5327   0.00614   0.00217  -0.1383   0.7788   0.6824
  -0.250   0.5603   0.00619   0.00221  -0.1384   0.7692   0.6855
   0.000   0.5882   0.00627   0.00224  -0.1384   0.7592   0.6888
   0.250   0.6160   0.00636   0.00227  -0.1385   0.7480   0.6916
   0.500   0.6429   0.00642   0.00230  -0.1384   0.7350   0.6942
   0.750   0.6682   0.00652   0.00236  -0.1379   0.7190   0.6967
   1.000   0.6921   0.00666   0.00244  -0.1372   0.6998   0.6991
   1.250   0.7161   0.00683   0.00253  -0.1364   0.6793   0.7019
   1.500   0.7397   0.00701   0.00263  -0.1356   0.6574   0.7047
   1.750   0.7627   0.00723   0.00274  -0.1347   0.6339   0.7071
   2.000   0.7850   0.00746   0.00285  -0.1337   0.6085   0.7092
   2.250   0.8063   0.00768   0.00300  -0.1325   0.5842   0.7115
   2.500   0.8254   0.00796   0.00318  -0.1308   0.5562   0.7136
   2.750   0.8450   0.00825   0.00336  -0.1293   0.5305   0.7158
   3.000   0.8645   0.00857   0.00356  -0.1278   0.5026   0.7180
   3.250   0.8847   0.00890   0.00377  -0.1264   0.4765   0.7202
   3.500   0.9078   0.00918   0.00397  -0.1257   0.4551   0.7222
   3.750   0.9303   0.00951   0.00418  -0.1249   0.4299   0.7240
   4.000   0.9517   0.00985   0.00442  -0.1239   0.4054   0.7262
   4.250   0.9724   0.01021   0.00469  -0.1227   0.3800   0.7282
   4.500   0.9932   0.01058   0.00496  -0.1216   0.3573   0.7302
   4.750   1.0152   0.01090   0.00523  -0.1207   0.3408   0.7322
   5.000   1.0375   0.01122   0.00548  -0.1199   0.3243   0.7340
   5.250   1.0592   0.01158   0.00576  -0.1191   0.3048   0.7359
   5.500   1.0802   0.01196   0.00606  -0.1181   0.2868   0.7377
   5.750   1.1017   0.01233   0.00635  -0.1172   0.2707   0.7393
   6.000   1.1236   0.01266   0.00663  -0.1164   0.2565   0.7410
   6.250   1.1448   0.01301   0.00695  -0.1155   0.2432   0.7428
   6.500   1.1651   0.01340   0.00729  -0.1144   0.2300   0.7444
   6.750   1.1849   0.01381   0.00766  -0.1133   0.2176   0.7462
   7.000   1.2047   0.01424   0.00803  -0.1122   0.2030   0.7481
   7.250   1.2242   0.01469   0.00842  -0.1110   0.1891   0.7500
   7.500   1.2439   0.01513   0.00882  -0.1099   0.1788   0.7519
   7.750   1.2645   0.01554   0.00921  -0.1090   0.1712   0.7536
   8.000   1.2836   0.01603   0.00966  -0.1079   0.1604   0.7551
   8.250   1.3033   0.01648   0.01008  -0.1069   0.1489   0.7567
   8.500   1.3203   0.01706   0.01059  -0.1055   0.1365   0.7586
   8.750   1.3378   0.01761   0.01112  -0.1041   0.1266   0.7603
   9.000   1.3544   0.01822   0.01169  -0.1026   0.1167   0.7622
   9.250   1.3712   0.01881   0.01226  -0.1013   0.1063   0.7641
   9.500   1.3859   0.01954   0.01293  -0.0996   0.0949   0.7661
   9.750   1.4015   0.02025   0.01360  -0.0981   0.0851   0.7679
  10.000   1.4153   0.02106   0.01436  -0.0964   0.0745   0.7696
  10.250   1.4267   0.02205   0.01525  -0.0945   0.0615   0.7712
  10.500   1.4398   0.02292   0.01609  -0.0928   0.0538   0.7729
  10.750   1.4512   0.02391   0.01705  -0.0909   0.0443   0.7747
  11.000   1.4594   0.02510   0.01818  -0.0887   0.0340   0.7763
  11.250   1.4707   0.02612   0.01919  -0.0869   0.0287   0.7778
  11.500   1.4796   0.02732   0.02037  -0.0850   0.0220   0.7794
  11.750   1.4779   0.02929   0.02227  -0.0818   0.0090   0.7810
  12.000   1.4811   0.03098   0.02398  -0.0793   0.0035   0.7827
  12.250   1.4908   0.03224   0.02530  -0.0777   0.0030   0.7843
  12.500   1.5015   0.03346   0.02658  -0.0764   0.0029   0.7859
  12.750   1.5114   0.03477   0.02796  -0.0750   0.0028   0.7872
  13.000   1.5195   0.03624   0.02951  -0.0735   0.0026   0.7887
  13.250   1.5272   0.03777   0.03113  -0.0721   0.0025   0.7905
  13.500   1.5332   0.03949   0.03294  -0.0706   0.0024   0.7920
  13.750   1.5383   0.04133   0.03487  -0.0692   0.0024   0.7937
  14.000   1.5420   0.04335   0.03700  -0.0678   0.0023   0.7953
  14.250   1.5454   0.04547   0.03921  -0.0665   0.0022   0.7971
  14.500   1.5496   0.04757   0.04140  -0.0655   0.0022   0.7987
  14.750   1.5528   0.04984   0.04376  -0.0645   0.0022   0.8003
  15.000   1.5551   0.05228   0.04629  -0.0637   0.0022   0.8017
  15.250   1.5558   0.05497   0.04907  -0.0629   0.0021   0.8030
  15.500   1.5558   0.05781   0.05200  -0.0624   0.0021   0.8044
  15.750   1.5544   0.06087   0.05517  -0.0619   0.0020   0.8060
  16.000   1.5515   0.06421   0.05862  -0.0617   0.0020   0.8074
  16.250   1.5474   0.06779   0.06232  -0.0616   0.0020   0.8088
  16.500   1.5424   0.07160   0.06624  -0.0617   0.0020   0.8101
  16.750   1.5349   0.07583   0.07059  -0.0620   0.0019   0.8115
  17.000   1.5261   0.08033   0.07522  -0.0626   0.0019   0.8128
  17.250   1.5162   0.08512   0.08013  -0.0635   0.0019   0.8140
  17.500   1.5052   0.09019   0.08532  -0.0647   0.0019   0.8153
  17.750   1.4939   0.09541   0.09067  -0.0661   0.0019   0.8165
  18.000   1.4798   0.10112   0.09651  -0.0678   0.0019   0.8175
  18.250   1.4635   0.10732   0.10283  -0.0699   0.0018   0.8185
  18.500   1.4479   0.11354   0.10919  -0.0722   0.0018   0.8195
  18.750   1.4320   0.11991   0.11569  -0.0748   0.0018   0.8208
  19.000   1.4155   0.12651   0.12243  -0.0777   0.0018   0.8220
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