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FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 60-177 AIRFOIL (fx60177-il)
Reynolds number: 500,000
Max Cl/Cd: 74.64 at α=1.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60177-il-500000-n5.txt
Download as CSV file: xf-fx60177-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.6213   0.14955   0.14665  -0.0480   1.0001   0.0041
 -18.500  -0.6540   0.13796   0.13490  -0.0527   1.0001   0.0040
 -18.250  -0.6779   0.12901   0.12582  -0.0564   1.0001   0.0040
 -18.000  -0.7039   0.11999   0.11668  -0.0601   1.0001   0.0040
 -17.750  -0.7282   0.11167   0.10823  -0.0636   1.0001   0.0040
 -17.500  -0.7492   0.10361   0.10004  -0.0675   1.0000   0.0039
 -17.250  -0.7654   0.09572   0.09200  -0.0722   0.9995   0.0039
 -17.000  -0.7790   0.08857   0.08470  -0.0765   0.9989   0.0039
 -16.750  -0.7899   0.08205   0.07803  -0.0806   0.9982   0.0039
 -16.500  -0.7983   0.07612   0.07195  -0.0844   0.9974   0.0039
 -16.250  -0.8039   0.07079   0.06647  -0.0880   0.9965   0.0039
 -16.000  -0.8071   0.06593   0.06146  -0.0912   0.9956   0.0039
 -15.750  -0.8083   0.06154   0.05694  -0.0941   0.9947   0.0039
 -15.500  -0.8072   0.05765   0.05291  -0.0967   0.9938   0.0039
 -15.250  -0.8060   0.05411   0.04925  -0.0986   0.9920   0.0039
 -15.000  -0.8024   0.05092   0.04594  -0.1003   0.9902   0.0039
 -14.750  -0.7972   0.04800   0.04290  -0.1019   0.9886   0.0039
 -14.500  -0.7898   0.04531   0.04009  -0.1036   0.9870   0.0039
 -14.250  -0.7803   0.04283   0.03750  -0.1052   0.9857   0.0039
 -14.000  -0.7691   0.04055   0.03511  -0.1069   0.9846   0.0039
 -13.750  -0.7563   0.03847   0.03292  -0.1084   0.9837   0.0040
 -13.500  -0.7496   0.03673   0.03110  -0.1080   0.9797   0.0040
 -13.250  -0.7375   0.03501   0.02929  -0.1087   0.9772   0.0040
 -13.000  -0.7230   0.03339   0.02758  -0.1096   0.9753   0.0040
 -12.500  -0.6886   0.03033   0.02435  -0.1120   0.9725   0.0040
 -12.250  -0.6689   0.02892   0.02286  -0.1134   0.9716   0.0041
 -12.000  -0.6601   0.02785   0.02173  -0.1120   0.9662   0.0041
 -11.750  -0.6416   0.02669   0.02050  -0.1126   0.9638   0.0041
 -11.500  -0.6211   0.02559   0.01934  -0.1134   0.9620   0.0042
 -11.250  -0.5993   0.02457   0.01826  -0.1144   0.9603   0.0043
 -11.000  -0.5761   0.02360   0.01722  -0.1154   0.9589   0.0043
 -10.750  -0.5616   0.02286   0.01643  -0.1145   0.9543   0.0044
 -10.500  -0.5432   0.02208   0.01560  -0.1142   0.9507   0.0045
 -10.250  -0.5213   0.02132   0.01479  -0.1146   0.9482   0.0046
 -10.000  -0.4978   0.02056   0.01399  -0.1153   0.9460   0.0047
  -9.750  -0.4726   0.01984   0.01321  -0.1162   0.9442   0.0048
  -9.500  -0.4605   0.01935   0.01268  -0.1143   0.9383   0.0050
  -9.250  -0.4402   0.01876   0.01206  -0.1140   0.9348   0.0051
  -9.000  -0.4173   0.01816   0.01142  -0.1142   0.9320   0.0054
  -8.750  -0.3921   0.01755   0.01078  -0.1149   0.9298   0.0059
  -8.500  -0.3801   0.01714   0.01036  -0.1128   0.9238   0.0066
  -8.250  -0.3608   0.01664   0.00984  -0.1121   0.9196   0.0082
  -8.000  -0.3372   0.01613   0.00931  -0.1122   0.9165   0.0106
  -7.750  -0.3181   0.01571   0.00887  -0.1113   0.9125   0.0128
  -7.500  -0.3038   0.01535   0.00851  -0.1095   0.9075   0.0152
  -7.250  -0.2816   0.01492   0.00806  -0.1093   0.9041   0.0185
  -7.000  -0.2553   0.01443   0.00760  -0.1100   0.9016   0.0244
  -6.750  -0.2345   0.01403   0.00723  -0.1095   0.8977   0.0327
  -6.500  -0.2156   0.01371   0.00693  -0.1085   0.8930   0.0388
  -6.250  -0.1910   0.01335   0.00657  -0.1087   0.8896   0.0464
  -6.000  -0.1629   0.01292   0.00617  -0.1096   0.8868   0.0586
  -5.750  -0.1398   0.01241   0.00579  -0.1097   0.8827   0.0849
  -5.500  -0.1209   0.01182   0.00539  -0.1091   0.8771   0.1287
  -5.250  -0.0956   0.01099   0.00488  -0.1101   0.8732   0.2025
  -5.000  -0.0638   0.00977   0.00420  -0.1132   0.8704   0.3307
  -4.750  -0.0344   0.00889   0.00377  -0.1152   0.8663   0.4366
  -4.500  -0.0008   0.00839   0.00352  -0.1173   0.8622   0.5043
  -4.250   0.0341   0.00813   0.00338  -0.1192   0.8584   0.5451
  -4.000   0.0702   0.00798   0.00328  -0.1211   0.8552   0.5768
  -3.750   0.0975   0.00795   0.00328  -0.1212   0.8497   0.5941
  -3.500   0.1281   0.00791   0.00323  -0.1218   0.8443   0.6074
  -3.250   0.1620   0.00788   0.00315  -0.1232   0.8399   0.6189
  -3.000   0.1901   0.00789   0.00313  -0.1234   0.8336   0.6291
  -2.750   0.2201   0.00788   0.00311  -0.1238   0.8278   0.6354
  -2.500   0.2512   0.00788   0.00306  -0.1246   0.8225   0.6408
  -2.250   0.2804   0.00788   0.00302  -0.1250   0.8161   0.6461
  -2.000   0.3108   0.00789   0.00300  -0.1256   0.8097   0.6502
  -1.750   0.3387   0.00792   0.00301  -0.1257   0.8014   0.6550
  -1.250   0.3973   0.00796   0.00296  -0.1264   0.7843   0.6636
  -1.000   0.4260   0.00800   0.00297  -0.1266   0.7753   0.6668
  -0.750   0.4541   0.00805   0.00296  -0.1268   0.7633   0.6704
  -0.500   0.4824   0.00811   0.00295  -0.1270   0.7508   0.6747
  -0.250   0.5103   0.00817   0.00296  -0.1271   0.7391   0.6780
   0.000   0.5371   0.00825   0.00302  -0.1269   0.7277   0.6806
   0.250   0.5638   0.00834   0.00307  -0.1267   0.7150   0.6835
   0.500   0.5902   0.00845   0.00312  -0.1265   0.7000   0.6867
   0.750   0.6163   0.00857   0.00316  -0.1263   0.6829   0.6902
   1.000   0.6410   0.00873   0.00321  -0.1258   0.6619   0.6932
   1.250   0.6623   0.00893   0.00334  -0.1245   0.6369   0.6954
   1.500   0.6837   0.00916   0.00347  -0.1232   0.6129   0.6977
   1.750   0.7036   0.00943   0.00362  -0.1217   0.5876   0.7002
   2.000   0.7213   0.00974   0.00378  -0.1198   0.5555   0.7028
   2.250   0.7402   0.01006   0.00396  -0.1182   0.5275   0.7054
   2.500   0.7612   0.01036   0.00414  -0.1171   0.5024   0.7079
   2.750   0.7817   0.01067   0.00436  -0.1159   0.4798   0.7097
   3.000   0.8032   0.01097   0.00460  -0.1148   0.4605   0.7117
   3.250   0.8253   0.01128   0.00484  -0.1139   0.4401   0.7139
   3.500   0.8470   0.01161   0.00510  -0.1130   0.4198   0.7162
   3.750   0.8690   0.01195   0.00536  -0.1121   0.4010   0.7185
   4.000   0.8910   0.01230   0.00563  -0.1113   0.3804   0.7207
   4.250   0.9127   0.01269   0.00591  -0.1105   0.3593   0.7228
   4.500   0.9347   0.01305   0.00620  -0.1098   0.3426   0.7246
   4.750   0.9561   0.01339   0.00650  -0.1088   0.3286   0.7261
   5.000   0.9777   0.01373   0.00682  -0.1080   0.3139   0.7276
   5.250   0.9982   0.01413   0.00716  -0.1069   0.2957   0.7293
   5.500   1.0183   0.01457   0.00752  -0.1059   0.2785   0.7311
   5.750   1.0390   0.01498   0.00789  -0.1049   0.2633   0.7332
   6.000   1.0602   0.01539   0.00825  -0.1041   0.2505   0.7354
   6.250   1.0820   0.01577   0.00861  -0.1034   0.2401   0.7375
   6.500   1.1033   0.01619   0.00899  -0.1026   0.2299   0.7394
   6.750   1.1228   0.01665   0.00943  -0.1016   0.2192   0.7409
   7.000   1.1431   0.01707   0.00984  -0.1006   0.2071   0.7423
   7.250   1.1626   0.01754   0.01030  -0.0996   0.1954   0.7439
   7.500   1.1812   0.01805   0.01079  -0.0984   0.1849   0.7457
   7.750   1.1990   0.01863   0.01132  -0.0972   0.1747   0.7477
   8.000   1.2184   0.01914   0.01183  -0.0962   0.1642   0.7498
   8.250   1.2368   0.01971   0.01237  -0.0951   0.1538   0.7520
   8.500   1.2541   0.02035   0.01297  -0.0939   0.1418   0.7540
   8.750   1.2712   0.02104   0.01360  -0.0927   0.1318   0.7558
   9.000   1.2887   0.02162   0.01421  -0.0916   0.1242   0.7572
   9.250   1.3044   0.02233   0.01491  -0.0902   0.1163   0.7588
   9.500   1.3214   0.02296   0.01557  -0.0890   0.1080   0.7605
   9.750   1.3356   0.02379   0.01637  -0.0874   0.0979   0.7622
  10.000   1.3496   0.02466   0.01720  -0.0860   0.0892   0.7639
  10.250   1.3631   0.02556   0.01809  -0.0845   0.0792   0.7656
  10.500   1.3753   0.02657   0.01906  -0.0829   0.0680   0.7674
  10.750   1.3860   0.02770   0.02014  -0.0812   0.0590   0.7691
  11.000   1.3977   0.02880   0.02122  -0.0797   0.0514   0.7708
  11.250   1.4080   0.02999   0.02240  -0.0781   0.0442   0.7723
  11.500   1.4166   0.03128   0.02368  -0.0764   0.0361   0.7737
  11.750   1.4253   0.03259   0.02501  -0.0747   0.0317   0.7751
  12.000   1.4347   0.03389   0.02634  -0.0732   0.0275   0.7766
  12.250   1.4427   0.03534   0.02781  -0.0716   0.0231   0.7784
  12.500   1.4452   0.03727   0.02972  -0.0697   0.0140   0.7801
  12.750   1.4480   0.03924   0.03172  -0.0679   0.0094   0.7820
  13.000   1.4469   0.04164   0.03416  -0.0660   0.0037   0.7837
  13.250   1.4520   0.04357   0.03617  -0.0648   0.0032   0.7853
  13.500   1.4579   0.04549   0.03818  -0.0637   0.0029   0.7869
  13.750   1.4632   0.04750   0.04029  -0.0627   0.0028   0.7883
  14.000   1.4674   0.04964   0.04254  -0.0618   0.0027   0.7896
  14.250   1.4698   0.05204   0.04505  -0.0609   0.0025   0.7910
  14.500   1.4716   0.05458   0.04772  -0.0601   0.0024   0.7924
  14.750   1.4718   0.05736   0.05062  -0.0595   0.0023   0.7938
  15.000   1.4718   0.06025   0.05363  -0.0590   0.0022   0.7953
  15.250   1.4722   0.06319   0.05669  -0.0587   0.0022   0.7968
  15.500   1.4717   0.06632   0.05994  -0.0586   0.0021   0.7984
  15.750   1.4699   0.06970   0.06345  -0.0587   0.0021   0.8000
  16.000   1.4669   0.07335   0.06721  -0.0590   0.0020   0.8016
  16.250   1.4626   0.07723   0.07121  -0.0595   0.0020   0.8031
  16.500   1.4573   0.08131   0.07543  -0.0601   0.0019   0.8044
  16.750   1.4499   0.08577   0.08004  -0.0610   0.0019   0.8055
  17.000   1.4417   0.09045   0.08486  -0.0620   0.0018   0.8067
  17.250   1.4322   0.09543   0.08998  -0.0634   0.0018   0.8079
  17.500   1.4223   0.10052   0.09521  -0.0649   0.0018   0.8092
  17.750   1.4119   0.10579   0.10062  -0.0667   0.0018   0.8104
  18.000   1.3999   0.11142   0.10640  -0.0688   0.0018   0.8118
  18.250   1.3876   0.11723   0.11234  -0.0711   0.0018   0.8130
  18.500   1.3745   0.12325   0.11850  -0.0738   0.0017   0.8143
  18.750   1.3626   0.12912   0.12450  -0.0765   0.0017   0.8155
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