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FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 60-177 AIRFOIL (fx60177-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.76 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx60177-il-1000000-n5.txt
Download as CSV file: xf-fx60177-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.7101   0.12767   0.12502  -0.0617   0.9990   0.0028
 -18.750  -0.7271   0.11940   0.11665  -0.0662   0.9987   0.0027
 -18.500  -0.7441   0.11142   0.10856  -0.0706   0.9983   0.0027
 -18.250  -0.7605   0.10360   0.10063  -0.0750   0.9980   0.0027
 -18.000  -0.7756   0.09618   0.09309  -0.0793   0.9976   0.0027
 -17.750  -0.7884   0.08935   0.08614  -0.0834   0.9971   0.0027
 -17.500  -0.7997   0.08285   0.07951  -0.0874   0.9966   0.0027
 -17.250  -0.8094   0.07679   0.07333  -0.0913   0.9961   0.0027
 -17.000  -0.8168   0.07128   0.06769  -0.0948   0.9955   0.0027
 -16.750  -0.8225   0.06617   0.06245  -0.0980   0.9950   0.0027
 -16.500  -0.8264   0.06148   0.05764  -0.1011   0.9944   0.0027
 -16.250  -0.8276   0.05737   0.05342  -0.1036   0.9937   0.0027
 -16.000  -0.8289   0.05363   0.04957  -0.1054   0.9922   0.0027
 -15.750  -0.8276   0.05019   0.04603  -0.1073   0.9907   0.0027
 -15.500  -0.8231   0.04716   0.04289  -0.1090   0.9893   0.0027
 -15.250  -0.8175   0.04428   0.03991  -0.1107   0.9880   0.0027
 -15.000  -0.8096   0.04169   0.03723  -0.1123   0.9868   0.0027
 -14.750  -0.8003   0.03929   0.03473  -0.1138   0.9858   0.0027
 -14.500  -0.7893   0.03705   0.03240  -0.1154   0.9849   0.0027
 -14.250  -0.7765   0.03500   0.03026  -0.1169   0.9841   0.0027
 -14.000  -0.7652   0.03320   0.02838  -0.1176   0.9823   0.0027
 -13.750  -0.7555   0.03160   0.02671  -0.1175   0.9789   0.0027
 -13.500  -0.7414   0.03002   0.02506  -0.1183   0.9767   0.0027
 -13.250  -0.7257   0.02854   0.02351  -0.1192   0.9748   0.0027
 -13.000  -0.7085   0.02718   0.02207  -0.1201   0.9731   0.0028
 -12.750  -0.6897   0.02585   0.02068  -0.1212   0.9715   0.0028
 -12.500  -0.6777   0.02481   0.01958  -0.1205   0.9664   0.0028
 -12.250  -0.6605   0.02373   0.01844  -0.1207   0.9631   0.0028
 -12.000  -0.6408   0.02271   0.01736  -0.1213   0.9605   0.0028
 -11.750  -0.6206   0.02175   0.01635  -0.1219   0.9578   0.0028
 -11.500  -0.6056   0.02094   0.01549  -0.1212   0.9527   0.0028
 -11.250  -0.5866   0.02014   0.01464  -0.1212   0.9486   0.0028
 -11.000  -0.5661   0.01936   0.01380  -0.1214   0.9453   0.0028
 -10.750  -0.5477   0.01871   0.01310  -0.1210   0.9412   0.0029
 -10.500  -0.5297   0.01806   0.01241  -0.1205   0.9364   0.0029
 -10.250  -0.5093   0.01743   0.01174  -0.1204   0.9323   0.0029
 -10.000  -0.4883   0.01685   0.01111  -0.1203   0.9288   0.0029
  -9.750  -0.4698   0.01633   0.01055  -0.1196   0.9243   0.0029
  -9.500  -0.4496   0.01581   0.01000  -0.1192   0.9199   0.0030
  -9.250  -0.4276   0.01533   0.00947  -0.1191   0.9160   0.0030
  -9.000  -0.4070   0.01486   0.00898  -0.1187   0.9119   0.0030
  -8.750  -0.3862   0.01443   0.00851  -0.1183   0.9075   0.0031
  -8.500  -0.3639   0.01401   0.00805  -0.1181   0.9035   0.0031
  -8.000  -0.3206   0.01325   0.00724  -0.1173   0.8963   0.0032
  -7.750  -0.3009   0.01293   0.00690  -0.1165   0.8919   0.0033
  -7.500  -0.2785   0.01261   0.00655  -0.1162   0.8880   0.0034
  -7.250  -0.2538   0.01230   0.00620  -0.1163   0.8848   0.0035
  -7.000  -0.2316   0.01200   0.00591  -0.1159   0.8807   0.0036
  -6.750  -0.2078   0.01171   0.00560  -0.1158   0.8764   0.0038
  -6.500  -0.1822   0.01143   0.00530  -0.1160   0.8725   0.0043
  -6.250  -0.1569   0.01109   0.00498  -0.1163   0.8688   0.0093
  -6.000  -0.1322   0.01080   0.00471  -0.1164   0.8642   0.0133
  -5.750  -0.1059   0.01052   0.00444  -0.1167   0.8596   0.0181
  -5.500  -0.0789   0.01015   0.00412  -0.1173   0.8553   0.0342
  -5.250  -0.0535   0.00987   0.00389  -0.1174   0.8500   0.0466
  -5.000  -0.0279   0.00947   0.00361  -0.1178   0.8444   0.0756
  -4.500   0.0258   0.00838   0.00297  -0.1194   0.8342   0.1939
  -4.250   0.0556   0.00762   0.00258  -0.1211   0.8273   0.2931
  -4.000   0.0871   0.00713   0.00232  -0.1228   0.8204   0.3615
  -3.750   0.1224   0.00653   0.00203  -0.1255   0.8137   0.4511
  -3.500   0.1605   0.00603   0.00183  -0.1286   0.8076   0.5403
  -3.250   0.1920   0.00594   0.00177  -0.1296   0.8007   0.5661
  -3.000   0.2225   0.00591   0.00173  -0.1303   0.7929   0.5813
  -2.750   0.2528   0.00589   0.00172  -0.1310   0.7847   0.5946
  -2.500   0.2826   0.00590   0.00171  -0.1316   0.7771   0.6070
  -2.250   0.3124   0.00591   0.00170  -0.1321   0.7693   0.6160
  -2.000   0.3407   0.00596   0.00170  -0.1323   0.7579   0.6218
  -1.750   0.3680   0.00603   0.00170  -0.1323   0.7429   0.6268
  -1.500   0.3950   0.00612   0.00170  -0.1322   0.7270   0.6307
  -1.250   0.4225   0.00619   0.00174  -0.1322   0.7135   0.6356
  -1.000   0.4502   0.00627   0.00177  -0.1323   0.7006   0.6409
  -0.750   0.4775   0.00636   0.00179  -0.1323   0.6866   0.6450
  -0.500   0.5039   0.00648   0.00185  -0.1321   0.6706   0.6483
  -0.250   0.5290   0.00663   0.00193  -0.1317   0.6499   0.6522
   0.000   0.5529   0.00683   0.00202  -0.1310   0.6231   0.6563
   0.250   0.5769   0.00705   0.00211  -0.1303   0.5994   0.6599
   0.500   0.6008   0.00727   0.00222  -0.1297   0.5730   0.6627
   0.750   0.6232   0.00755   0.00237  -0.1287   0.5424   0.6655
   1.000   0.6457   0.00783   0.00252  -0.1278   0.5127   0.6688
   1.250   0.6678   0.00811   0.00267  -0.1268   0.4849   0.6723
   1.500   0.6910   0.00835   0.00281  -0.1261   0.4622   0.6754
   1.750   0.7148   0.00857   0.00294  -0.1255   0.4411   0.6778
   2.000   0.7386   0.00880   0.00310  -0.1249   0.4212   0.6801
   2.250   0.7629   0.00902   0.00325  -0.1243   0.4053   0.6826
   2.500   0.7875   0.00924   0.00342  -0.1239   0.3895   0.6852
   2.750   0.8118   0.00949   0.00359  -0.1234   0.3709   0.6879
   3.000   0.8352   0.00979   0.00379  -0.1228   0.3505   0.6901
   3.250   0.8588   0.01009   0.00399  -0.1222   0.3319   0.6921
   3.500   0.8832   0.01033   0.00419  -0.1218   0.3167   0.6941
   3.750   0.9073   0.01058   0.00440  -0.1213   0.3026   0.6964
   4.000   0.9302   0.01089   0.00464  -0.1206   0.2864   0.6988
   4.250   0.9526   0.01122   0.00489  -0.1198   0.2690   0.7011
   4.500   0.9748   0.01157   0.00516  -0.1190   0.2505   0.7031
   4.750   0.9981   0.01185   0.00540  -0.1184   0.2390   0.7049
   5.000   1.0216   0.01212   0.00563  -0.1179   0.2302   0.7067
   5.250   1.0439   0.01245   0.00591  -0.1171   0.2195   0.7082
   5.500   1.0665   0.01275   0.00618  -0.1165   0.2071   0.7099
   5.750   1.0871   0.01316   0.00652  -0.1154   0.1907   0.7116
   6.000   1.1092   0.01348   0.00682  -0.1147   0.1819   0.7133
   6.250   1.1307   0.01384   0.00715  -0.1138   0.1742   0.7151
   6.500   1.1526   0.01417   0.00747  -0.1130   0.1655   0.7171
   6.750   1.1729   0.01459   0.00785  -0.1120   0.1537   0.7191
   7.000   1.1918   0.01509   0.00826  -0.1108   0.1391   0.7210
   7.250   1.2113   0.01555   0.00868  -0.1097   0.1296   0.7226
   7.500   1.2308   0.01602   0.00911  -0.1086   0.1201   0.7241
   7.750   1.2510   0.01644   0.00952  -0.1076   0.1136   0.7257
   8.000   1.2688   0.01699   0.01003  -0.1063   0.1016   0.7273
   8.250   1.2854   0.01762   0.01060  -0.1048   0.0904   0.7290
   8.500   1.3017   0.01827   0.01120  -0.1033   0.0789   0.7311
   8.750   1.3154   0.01908   0.01192  -0.1014   0.0633   0.7332
   9.000   1.3306   0.01980   0.01260  -0.0999   0.0548   0.7353
   9.250   1.3466   0.02049   0.01326  -0.0984   0.0471   0.7371
   9.500   1.3587   0.02142   0.01413  -0.0965   0.0358   0.7387
   9.750   1.3726   0.02225   0.01492  -0.0948   0.0301   0.7403
  10.000   1.3882   0.02297   0.01566  -0.0934   0.0262   0.7420
  10.250   1.3980   0.02409   0.01674  -0.0913   0.0161   0.7435
  10.500   1.4063   0.02531   0.01795  -0.0891   0.0089   0.7450
  10.750   1.4146   0.02656   0.01922  -0.0869   0.0028   0.7466
  11.000   1.4275   0.02751   0.02022  -0.0853   0.0024   0.7482
  11.250   1.4411   0.02843   0.02119  -0.0840   0.0022   0.7498
  11.500   1.4541   0.02939   0.02221  -0.0826   0.0021   0.7514
  11.750   1.4663   0.03042   0.02329  -0.0812   0.0020   0.7529
  12.000   1.4777   0.03153   0.02446  -0.0797   0.0018   0.7543
  12.250   1.4881   0.03275   0.02574  -0.0782   0.0017   0.7556
  12.500   1.4981   0.03403   0.02710  -0.0768   0.0016   0.7570
  12.750   1.5069   0.03543   0.02857  -0.0753   0.0015   0.7586
  13.000   1.5166   0.03676   0.02998  -0.0740   0.0014   0.7601
  13.250   1.5257   0.03819   0.03148  -0.0728   0.0014   0.7618
  13.500   1.5341   0.03972   0.03307  -0.0715   0.0014   0.7635
  13.750   1.5414   0.04138   0.03481  -0.0703   0.0013   0.7652
  14.000   1.5481   0.04314   0.03664  -0.0691   0.0013   0.7668
  14.250   1.5537   0.04504   0.03862  -0.0680   0.0012   0.7682
  14.500   1.5586   0.04704   0.04071  -0.0670   0.0012   0.7696
  14.750   1.5626   0.04920   0.04294  -0.0660   0.0012   0.7709
  15.250   1.5681   0.05398   0.04790  -0.0644   0.0011   0.7734
  15.500   1.5695   0.05662   0.05063  -0.0638   0.0011   0.7748
  15.750   1.5698   0.05943   0.05354  -0.0633   0.0011   0.7761
  16.000   1.5691   0.06243   0.05663  -0.0629   0.0010   0.7775
  16.250   1.5668   0.06571   0.06002  -0.0627   0.0010   0.7788
  16.500   1.5640   0.06915   0.06356  -0.0627   0.0010   0.7802
  16.750   1.5588   0.07299   0.06751  -0.0628   0.0010   0.7815
  17.000   1.5527   0.07702   0.07164  -0.0632   0.0010   0.7828
  17.250   1.5447   0.08140   0.07615  -0.0638   0.0009   0.7841
  17.500   1.5363   0.08596   0.08082  -0.0646   0.0009   0.7854
  17.750   1.5268   0.09077   0.08574  -0.0657   0.0009   0.7865
  18.000   1.5146   0.09607   0.09116  -0.0671   0.0009   0.7875
  18.250   1.5015   0.10156   0.09678  -0.0687   0.0009   0.7885
  18.500   1.4870   0.10741   0.10277  -0.0706   0.0009   0.7897
  18.750   1.4732   0.11323   0.10872  -0.0728   0.0009   0.7908
  19.000   1.4565   0.11967   0.11530  -0.0754   0.0009   0.7918
  19.250   1.4411   0.12597   0.12172  -0.0781   0.0009   0.7929
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