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NACA 63(3)-618 (naca633618-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NACA 63(3)-618 (naca633618-il)
Reynolds number: 500,000
Max Cl/Cd: 107.65 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca633618-il-500000.txt
Download as CSV file: xf-naca633618-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(3)-618                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.8251   0.09367   0.09003  -0.0706   1.0000   0.0217
 -18.250  -0.8330   0.08870   0.08498  -0.0735   1.0000   0.0219
 -18.000  -0.8430   0.08350   0.07968  -0.0764   1.0000   0.0220
 -17.750  -0.8478   0.07919   0.07530  -0.0788   1.0000   0.0224
 -17.500  -0.8561   0.07456   0.07055  -0.0813   1.0000   0.0226
 -17.250  -0.8619   0.07036   0.06626  -0.0835   1.0000   0.0229
 -17.000  -0.8682   0.06626   0.06204  -0.0855   1.0000   0.0231
 -16.750  -0.8725   0.06255   0.05821  -0.0873   1.0000   0.0234
 -16.500  -0.8763   0.05903   0.05457  -0.0888   1.0000   0.0237
 -16.250  -0.8790   0.05575   0.05115  -0.0902   1.0000   0.0241
 -16.000  -0.8816   0.05256   0.04782  -0.0916   1.0000   0.0244
 -15.750  -0.8815   0.04999   0.04517  -0.0919   1.0000   0.0248
 -15.500  -0.8783   0.04783   0.04301  -0.0922   1.0000   0.0252
 -15.250  -0.8739   0.04583   0.04098  -0.0926   1.0000   0.0256
 -15.000  -0.8700   0.04387   0.03899  -0.0928   1.0000   0.0260
 -14.750  -0.8661   0.04199   0.03706  -0.0930   1.0000   0.0265
 -14.500  -0.8625   0.04017   0.03517  -0.0928   1.0000   0.0271
 -14.250  -0.8593   0.03838   0.03329  -0.0926   1.0000   0.0277
 -14.000  -0.8561   0.03674   0.03155  -0.0922   1.0000   0.0283
 -13.750  -0.8539   0.03516   0.02993  -0.0911   1.0000   0.0289
 -13.500  -0.8520   0.03385   0.02865  -0.0897   1.0000   0.0294
 -13.250  -0.8445   0.03262   0.02742  -0.0894   0.9990   0.0301
 -13.000  -0.8169   0.03102   0.02577  -0.0928   0.9893   0.0312
 -12.750  -0.7901   0.02948   0.02411  -0.0959   0.9795   0.0324
 -12.500  -0.7624   0.02791   0.02248  -0.0989   0.9702   0.0336
 -12.250  -0.7290   0.02656   0.02113  -0.1028   0.9616   0.0349
 -12.000  -0.6909   0.02530   0.01979  -0.1075   0.9532   0.0365
 -11.750  -0.6532   0.02409   0.01844  -0.1119   0.9410   0.0382
 -11.500  -0.6216   0.02288   0.01722  -0.1150   0.9259   0.0398
 -11.250  -0.5977   0.02206   0.01629  -0.1163   0.9091   0.0413
 -11.000  -0.5806   0.02135   0.01546  -0.1160   0.8935   0.0425
 -10.750  -0.5648   0.02075   0.01471  -0.1152   0.8803   0.0434
 -10.500  -0.5572   0.01973   0.01366  -0.1135   0.8677   0.0449
 -10.250  -0.5464   0.01902   0.01292  -0.1120   0.8564   0.0461
 -10.000  -0.5345   0.01844   0.01224  -0.1105   0.8465   0.0474
  -9.750  -0.5245   0.01794   0.01167  -0.1086   0.8366   0.0486
  -9.500  -0.5077   0.01752   0.01111  -0.1076   0.8287   0.0497
  -9.250  -0.4968   0.01664   0.01024  -0.1062   0.8200   0.0514
  -9.000  -0.4779   0.01618   0.00972  -0.1054   0.8127   0.0532
  -8.750  -0.4573   0.01576   0.00925  -0.1048   0.8055   0.0551
  -8.500  -0.4346   0.01544   0.00885  -0.1044   0.7986   0.0568
  -8.250  -0.4157   0.01478   0.00816  -0.1038   0.7922   0.0595
  -8.000  -0.3928   0.01438   0.00774  -0.1034   0.7854   0.0621
  -7.750  -0.3684   0.01406   0.00734  -0.1032   0.7790   0.0647
  -7.500  -0.3455   0.01353   0.00680  -0.1030   0.7731   0.0688
  -7.250  -0.3202   0.01319   0.00644  -0.1029   0.7669   0.0735
  -7.000  -0.2956   0.01271   0.00597  -0.1029   0.7608   0.0815
  -6.750  -0.2700   0.01229   0.00555  -0.1030   0.7552   0.0945
  -6.500  -0.2446   0.01175   0.00515  -0.1032   0.7491   0.1203
  -6.250  -0.2187   0.01119   0.00474  -0.1036   0.7433   0.1582
  -6.000  -0.1919   0.01066   0.00436  -0.1040   0.7380   0.2045
  -5.750  -0.1649   0.01004   0.00400  -0.1047   0.7322   0.2654
  -5.500  -0.1370   0.00950   0.00369  -0.1053   0.7264   0.3285
  -5.250  -0.1082   0.00921   0.00352  -0.1059   0.7212   0.3821
  -5.000  -0.0789   0.00906   0.00344  -0.1064   0.7159   0.4144
  -4.750  -0.0496   0.00898   0.00337  -0.1067   0.7102   0.4362
  -4.500  -0.0202   0.00894   0.00330  -0.1071   0.7049   0.4528
  -4.250   0.0093   0.00893   0.00326  -0.1074   0.6998   0.4669
  -4.000   0.0388   0.00891   0.00322  -0.1078   0.6944   0.4789
  -3.750   0.0684   0.00893   0.00318  -0.1081   0.6892   0.4918
  -3.500   0.0979   0.00898   0.00321  -0.1084   0.6842   0.5055
  -3.250   0.1272   0.00897   0.00322  -0.1087   0.6789   0.5160
  -3.000   0.1567   0.00901   0.00321  -0.1090   0.6735   0.5252
  -2.750   0.1861   0.00903   0.00318  -0.1092   0.6688   0.5323
  -2.500   0.2155   0.00907   0.00320  -0.1095   0.6641   0.5397
  -2.250   0.2450   0.00910   0.00321  -0.1099   0.6589   0.5482
  -2.000   0.2741   0.00912   0.00323  -0.1101   0.6539   0.5551
  -1.750   0.3036   0.00920   0.00322  -0.1104   0.6491   0.5610
  -1.500   0.3330   0.00919   0.00321  -0.1107   0.6443   0.5663
  -1.250   0.3620   0.00918   0.00323  -0.1110   0.6395   0.5714
  -1.000   0.3914   0.00923   0.00324  -0.1113   0.6350   0.5769
  -0.750   0.4210   0.00932   0.00325  -0.1117   0.6305   0.5824
  -0.500   0.4499   0.00929   0.00328  -0.1119   0.6257   0.5875
  -0.250   0.4789   0.00932   0.00331  -0.1121   0.6208   0.5925
   0.000   0.5082   0.00939   0.00333  -0.1124   0.6164   0.5979
   0.250   0.5376   0.00946   0.00337  -0.1128   0.6121   0.6029
   0.500   0.5663   0.00946   0.00342  -0.1130   0.6075   0.6075
   0.750   0.5953   0.00950   0.00347  -0.1133   0.6029   0.6125
   1.000   0.6245   0.00960   0.00351  -0.1136   0.5984   0.6180
   1.250   0.6535   0.00965   0.00358  -0.1139   0.5942   0.6229
   1.500   0.6821   0.00968   0.00366  -0.1141   0.5896   0.6276
   1.750   0.7109   0.00973   0.00372  -0.1143   0.5850   0.6328
   2.000   0.7400   0.00986   0.00378  -0.1146   0.5806   0.6383
   2.250   0.7684   0.00990   0.00389  -0.1148   0.5761   0.6435
   2.500   0.7967   0.00995   0.00399  -0.1149   0.5713   0.6488
   2.750   0.8253   0.01003   0.00406  -0.1151   0.5667   0.6545
   3.000   0.8542   0.01018   0.00417  -0.1154   0.5622   0.6597
   3.250   0.8819   0.01021   0.00430  -0.1155   0.5578   0.6649
   3.500   0.9101   0.01028   0.00441  -0.1156   0.5530   0.6707
   3.750   0.9385   0.01040   0.00451  -0.1159   0.5485   0.6767
   4.000   0.9664   0.01052   0.00466  -0.1159   0.5439   0.6823
   4.250   0.9938   0.01058   0.00481  -0.1160   0.5389   0.6882
   4.500   1.0215   0.01067   0.00491  -0.1160   0.5335   0.6943
   4.750   1.0489   0.01082   0.00504  -0.1160   0.5276   0.6998
   5.000   1.0753   0.01086   0.00519  -0.1158   0.5213   0.7060
   5.250   1.1022   0.01097   0.00531  -0.1158   0.5150   0.7128
   5.500   1.1286   0.01110   0.00547  -0.1156   0.5090   0.7187
   5.750   1.1546   0.01117   0.00563  -0.1154   0.5021   0.7250
   6.000   1.1807   0.01134   0.00577  -0.1152   0.4953   0.7318
   6.250   1.2060   0.01143   0.00597  -0.1148   0.4880   0.7380
   6.500   1.2303   0.01158   0.00612  -0.1142   0.4790   0.7451
   6.750   1.2545   0.01171   0.00630  -0.1137   0.4681   0.7520
   7.000   1.2768   0.01188   0.00650  -0.1128   0.4564   0.7585
   7.250   1.2992   0.01210   0.00672  -0.1120   0.4448   0.7662
   7.500   1.3219   0.01228   0.00697  -0.1112   0.4339   0.7732
   7.750   1.3428   0.01253   0.00724  -0.1101   0.4221   0.7808
   8.000   1.3621   0.01283   0.00754  -0.1088   0.4087   0.7885
   8.250   1.3791   0.01317   0.00789  -0.1071   0.3935   0.7965
   8.500   1.3931   0.01355   0.00825  -0.1048   0.3759   0.8053
   8.750   1.4023   0.01401   0.00871  -0.1017   0.3553   0.8142
   9.000   1.4074   0.01471   0.00933  -0.0982   0.3315   0.8240
   9.250   1.4100   0.01556   0.01011  -0.0945   0.3070   0.8350
   9.500   1.4098   0.01658   0.01107  -0.0906   0.2825   0.8469
   9.750   1.4095   0.01772   0.01215  -0.0870   0.2585   0.8605
  10.000   1.4073   0.01901   0.01339  -0.0834   0.2357   0.8768
  10.250   1.4039   0.02037   0.01473  -0.0797   0.2152   0.8988
  10.500   1.3987   0.02165   0.01603  -0.0758   0.1971   0.9549
  10.750   1.4001   0.02339   0.01768  -0.0739   0.1769   1.0000
  11.000   1.4005   0.02535   0.01953  -0.0721   0.1583   1.0000
  11.250   1.4014   0.02734   0.02144  -0.0705   0.1415   1.0000
  11.500   1.4020   0.02943   0.02345  -0.0690   0.1250   1.0000
  11.750   1.4022   0.03162   0.02558  -0.0676   0.1101   1.0000
  12.000   1.4016   0.03396   0.02786  -0.0663   0.0962   1.0000
  12.250   1.4006   0.03642   0.03025  -0.0651   0.0838   1.0000
  12.500   1.3999   0.03896   0.03275  -0.0641   0.0731   1.0000
  12.750   1.4007   0.04145   0.03522  -0.0633   0.0650   1.0000
  13.000   1.4020   0.04399   0.03776  -0.0627   0.0589   1.0000
  13.250   1.4021   0.04672   0.04048  -0.0621   0.0541   1.0000
  13.500   1.4063   0.04911   0.04291  -0.0618   0.0506   1.0000
  13.750   1.4062   0.05202   0.04583  -0.0615   0.0477   1.0000
  14.000   1.4110   0.05447   0.04835  -0.0613   0.0456   1.0000
  14.250   1.4145   0.05712   0.05104  -0.0613   0.0435   1.0000
  14.500   1.4146   0.06024   0.05419  -0.0613   0.0418   1.0000
  14.750   1.4170   0.06313   0.05715  -0.0614   0.0404   1.0000
  15.000   1.4217   0.06578   0.05988  -0.0616   0.0390   1.0000
  15.250   1.4241   0.06880   0.06294  -0.0619   0.0377   1.0000
  15.500   1.4237   0.07221   0.06639  -0.0623   0.0365   1.0000
  15.750   1.4235   0.07565   0.06990  -0.0628   0.0354   1.0000
  16.000   1.4276   0.07858   0.07291  -0.0633   0.0344   1.0000
  16.250   1.4311   0.08162   0.07602  -0.0638   0.0333   1.0000
  16.500   1.4323   0.08504   0.07950  -0.0646   0.0322   1.0000
  16.750   1.4298   0.08900   0.08350  -0.0655   0.0313   1.0000
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