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NACA 63-215 AIRFOIL (n63215-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 63-215 AIRFOIL (n63215-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.92 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-n63215-il-1000000.txt
Download as CSV file: xf-n63215-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-215 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0256   0.12210   0.11948  -0.0120   1.0000   0.0124
 -19.500  -1.0434   0.11429   0.11155  -0.0167   1.0000   0.0124
 -19.250  -1.0621   0.10660   0.10373  -0.0212   1.0000   0.0125
 -19.000  -1.0750   0.10015   0.09718  -0.0249   1.0000   0.0126
 -18.750  -1.0873   0.09395   0.09088  -0.0285   1.0000   0.0126
 -18.500  -1.0987   0.08810   0.08492  -0.0317   1.0000   0.0127
 -18.250  -1.1104   0.08239   0.07911  -0.0348   1.0000   0.0128
 -18.000  -1.1174   0.07754   0.07417  -0.0374   1.0000   0.0129
 -17.750  -1.1238   0.07295   0.06949  -0.0397   1.0000   0.0130
 -17.500  -1.1319   0.06828   0.06471  -0.0419   1.0000   0.0130
 -17.250  -1.1346   0.06444   0.06079  -0.0438   1.0000   0.0132
 -17.000  -1.1398   0.06048   0.05673  -0.0455   1.0000   0.0132
 -16.750  -1.1417   0.05700   0.05316  -0.0469   1.0000   0.0134
 -16.500  -1.1425   0.05378   0.04985  -0.0482   1.0000   0.0135
 -16.250  -1.1420   0.05082   0.04680  -0.0492   1.0000   0.0137
 -16.000  -1.1409   0.04802   0.04391  -0.0501   1.0000   0.0139
 -15.750  -1.1419   0.04513   0.04093  -0.0507   1.0000   0.0140
 -15.500  -1.1375   0.04290   0.03861  -0.0512   1.0000   0.0142
 -15.250  -1.1341   0.04063   0.03626  -0.0516   1.0000   0.0143
 -15.000  -1.1265   0.03882   0.03437  -0.0519   1.0000   0.0145
 -14.750  -1.1221   0.03675   0.03222  -0.0520   1.0000   0.0147
 -14.500  -1.1261   0.03401   0.02938  -0.0518   1.0000   0.0150
 -14.250  -1.1229   0.03198   0.02729  -0.0515   1.0000   0.0152
 -14.000  -1.1174   0.03020   0.02547  -0.0513   1.0000   0.0155
 -13.750  -1.1098   0.02866   0.02387  -0.0509   1.0000   0.0157
 -13.500  -1.0993   0.02739   0.02256  -0.0505   1.0000   0.0160
 -13.250  -1.0891   0.02615   0.02128  -0.0500   1.0000   0.0163
 -13.000  -1.0785   0.02497   0.02005  -0.0493   1.0000   0.0166
 -12.750  -1.0680   0.02383   0.01886  -0.0486   1.0000   0.0170
 -12.500  -1.0571   0.02277   0.01774  -0.0477   1.0000   0.0172
 -12.250  -1.0441   0.02190   0.01682  -0.0469   1.0000   0.0175
 -12.000  -1.0309   0.02109   0.01595  -0.0459   1.0000   0.0178
 -11.750  -1.0251   0.01992   0.01472  -0.0442   1.0000   0.0182
 -11.500  -1.0212   0.01886   0.01362  -0.0419   1.0000   0.0186
 -11.250  -1.0136   0.01816   0.01291  -0.0396   1.0000   0.0191
 -11.000  -0.9967   0.01770   0.01244  -0.0384   1.0000   0.0197
 -10.750  -0.9597   0.01702   0.01171  -0.0414   0.9706   0.0204
 -10.500  -0.9259   0.01645   0.01107  -0.0435   0.9461   0.0212
 -10.250  -0.9048   0.01613   0.01063  -0.0427   0.9216   0.0217
 -10.000  -0.8912   0.01543   0.00982  -0.0409   0.9016   0.0225
  -9.750  -0.8726   0.01495   0.00929  -0.0397   0.8872   0.0234
  -9.500  -0.8512   0.01462   0.00888  -0.0389   0.8751   0.0243
  -9.250  -0.8286   0.01430   0.00851  -0.0383   0.8639   0.0253
  -9.000  -0.8046   0.01406   0.00820  -0.0378   0.8542   0.0261
  -8.500  -0.7607   0.01310   0.00714  -0.0365   0.8354   0.0290
  -8.250  -0.7363   0.01282   0.00680  -0.0361   0.8271   0.0303
  -8.000  -0.7105   0.01258   0.00652  -0.0360   0.8190   0.0313
  -7.500  -0.6617   0.01180   0.00566  -0.0353   0.8035   0.0353
  -7.250  -0.6356   0.01157   0.00538  -0.0352   0.7961   0.0370
  -7.000  -0.6099   0.01123   0.00501  -0.0350   0.7890   0.0395
  -6.750  -0.5838   0.01094   0.00471  -0.0349   0.7816   0.0424
  -6.500  -0.5569   0.01074   0.00446  -0.0349   0.7749   0.0447
  -6.250  -0.5307   0.01039   0.00413  -0.0348   0.7678   0.0508
  -5.750  -0.4779   0.00972   0.00355  -0.0347   0.7543   0.0784
  -5.500  -0.4519   0.00929   0.00324  -0.0347   0.7475   0.1093
  -5.250  -0.4259   0.00882   0.00295  -0.0348   0.7411   0.1508
  -5.000  -0.3997   0.00832   0.00265  -0.0349   0.7342   0.2020
  -4.750  -0.3739   0.00778   0.00234  -0.0349   0.7278   0.2664
  -4.500  -0.3474   0.00723   0.00208  -0.0351   0.7216   0.3365
  -4.250  -0.3199   0.00689   0.00191  -0.0353   0.7149   0.3917
  -4.000  -0.2916   0.00671   0.00180  -0.0355   0.7087   0.4234
  -3.750  -0.2628   0.00658   0.00171  -0.0358   0.7022   0.4454
  -3.500  -0.2341   0.00650   0.00164  -0.0360   0.6960   0.4637
  -3.250  -0.2050   0.00643   0.00158  -0.0363   0.6899   0.4793
  -3.000  -0.1759   0.00637   0.00153  -0.0365   0.6833   0.4940
  -2.750  -0.1470   0.00633   0.00149  -0.0367   0.6772   0.5105
  -2.500  -0.1177   0.00628   0.00146  -0.0370   0.6712   0.5258
  -2.250  -0.0885   0.00627   0.00143  -0.0373   0.6650   0.5365
  -2.000  -0.0593   0.00624   0.00140  -0.0375   0.6590   0.5446
  -1.750  -0.0299   0.00624   0.00138  -0.0378   0.6526   0.5545
  -1.500  -0.0009   0.00623   0.00137  -0.0380   0.6467   0.5643
  -1.250   0.0286   0.00623   0.00135  -0.0383   0.6410   0.5713
  -1.000   0.0578   0.00621   0.00134  -0.0386   0.6348   0.5781
  -0.750   0.0870   0.00624   0.00133  -0.0388   0.6287   0.5847
  -0.500   0.1165   0.00622   0.00133  -0.0391   0.6231   0.5910
  -0.250   0.1457   0.00622   0.00134  -0.0394   0.6171   0.5978
   0.000   0.1750   0.00626   0.00134  -0.0396   0.6112   0.6040
   0.250   0.2043   0.00624   0.00136  -0.0399   0.6053   0.6104
   0.500   0.2335   0.00628   0.00137  -0.0402   0.5990   0.6168
   0.750   0.2627   0.00629   0.00139  -0.0404   0.5931   0.6227
   1.000   0.2920   0.00630   0.00142  -0.0407   0.5867   0.6290
   1.250   0.3210   0.00637   0.00145  -0.0409   0.5804   0.6350
   1.500   0.3503   0.00636   0.00149  -0.0412   0.5746   0.6412
   1.750   0.3794   0.00639   0.00153  -0.0415   0.5682   0.6478
   2.000   0.4085   0.00645   0.00157  -0.0417   0.5619   0.6538
   2.250   0.4376   0.00646   0.00162  -0.0419   0.5540   0.6600
   2.500   0.4664   0.00652   0.00167  -0.0421   0.5448   0.6667
   2.750   0.4953   0.00656   0.00172  -0.0423   0.5361   0.6730
   3.000   0.5242   0.00661   0.00180  -0.0425   0.5285   0.6797
   3.250   0.5530   0.00669   0.00186  -0.0427   0.5183   0.6859
   3.500   0.5814   0.00674   0.00193  -0.0429   0.5050   0.6925
   3.750   0.6098   0.00684   0.00201  -0.0430   0.4904   0.6994
   4.000   0.6380   0.00695   0.00210  -0.0431   0.4748   0.7059
   4.250   0.6661   0.00706   0.00220  -0.0432   0.4601   0.7126
   4.500   0.6942   0.00720   0.00232  -0.0433   0.4435   0.7193
   4.750   0.7217   0.00735   0.00245  -0.0433   0.4244   0.7261
   5.000   0.7488   0.00757   0.00261  -0.0433   0.4006   0.7332
   5.250   0.7749   0.00788   0.00281  -0.0432   0.3661   0.7398
   5.500   0.7988   0.00839   0.00312  -0.0428   0.3142   0.7469
   5.750   0.8215   0.00903   0.00350  -0.0422   0.2567   0.7540
   6.000   0.8434   0.00969   0.00393  -0.0416   0.2039   0.7612
   6.250   0.8654   0.01035   0.00436  -0.0409   0.1569   0.7686
   6.500   0.8870   0.01097   0.00479  -0.0402   0.1172   0.7758
   6.750   0.9091   0.01154   0.00522  -0.0395   0.0877   0.7838
   7.000   0.9314   0.01205   0.00564  -0.0389   0.0668   0.7913
   7.250   0.9541   0.01250   0.00604  -0.0382   0.0533   0.7996
   7.500   0.9769   0.01291   0.00644  -0.0376   0.0455   0.8076
   7.750   0.9997   0.01331   0.00683  -0.0370   0.0409   0.8164
   8.000   1.0224   0.01366   0.00722  -0.0363   0.0377   0.8249
   8.250   1.0449   0.01402   0.00761  -0.0356   0.0354   0.8345
   8.500   1.0646   0.01451   0.00813  -0.0345   0.0326   0.8446
   8.750   1.0867   0.01481   0.00850  -0.0337   0.0314   0.8550
   9.000   1.1073   0.01517   0.00891  -0.0327   0.0298   0.8670
   9.250   1.1245   0.01564   0.00943  -0.0312   0.0281   0.8810
   9.500   1.1402   0.01611   0.00998  -0.0293   0.0267   0.8979
   9.750   1.1542   0.01639   0.01037  -0.0271   0.0256   0.9211
  10.000   1.1689   0.01670   0.01079  -0.0251   0.0244   1.0000
  10.250   1.1806   0.01739   0.01148  -0.0231   0.0230   1.0000
  10.500   1.1933   0.01808   0.01220  -0.0214   0.0221   1.0000
  10.750   1.2084   0.01867   0.01283  -0.0200   0.0212   1.0000
  11.000   1.2225   0.01934   0.01353  -0.0187   0.0204   1.0000
  11.250   1.2352   0.02013   0.01433  -0.0173   0.0197   1.0000
  11.500   1.2411   0.02138   0.01562  -0.0154   0.0186   1.0000
  11.750   1.2520   0.02239   0.01668  -0.0141   0.0183   1.0000
  12.000   1.2646   0.02332   0.01767  -0.0131   0.0179   1.0000
  12.250   1.2767   0.02433   0.01872  -0.0121   0.0174   1.0000
  12.500   1.2874   0.02547   0.01990  -0.0111   0.0170   1.0000
  12.750   1.2981   0.02665   0.02112  -0.0102   0.0165   1.0000
  13.000   1.3071   0.02800   0.02251  -0.0093   0.0160   1.0000
  13.250   1.3142   0.02954   0.02409  -0.0084   0.0157   1.0000
  13.500   1.3152   0.03166   0.02628  -0.0073   0.0153   1.0000
  13.750   1.3197   0.03354   0.02823  -0.0066   0.0150   1.0000
  14.000   1.3265   0.03528   0.03004  -0.0061   0.0149   1.0000
  14.250   1.3357   0.03685   0.03167  -0.0057   0.0146   1.0000
  14.500   1.3421   0.03870   0.03360  -0.0054   0.0144   1.0000
  14.750   1.3481   0.04066   0.03561  -0.0051   0.0141   1.0000
  15.000   1.3519   0.04288   0.03792  -0.0050   0.0139   1.0000
  15.250   1.3572   0.04503   0.04012  -0.0050   0.0136   1.0000
  15.500   1.3605   0.04746   0.04263  -0.0051   0.0135   1.0000
  15.750   1.3641   0.04995   0.04518  -0.0053   0.0133   1.0000
  16.000   1.3676   0.05251   0.04781  -0.0057   0.0132   1.0000
  16.250   1.3684   0.05545   0.05083  -0.0062   0.0130   1.0000
  16.500   1.3687   0.05856   0.05400  -0.0068   0.0128   1.0000
  16.750   1.3668   0.06204   0.05757  -0.0077   0.0127   1.0000
  17.000   1.3611   0.06609   0.06170  -0.0088   0.0125   1.0000
  17.250   1.3550   0.07033   0.06603  -0.0101   0.0123   1.0000
  17.500   1.3454   0.07516   0.07099  -0.0117   0.0121   1.0000
  17.750   1.3444   0.07898   0.07490  -0.0132   0.0121   1.0000
  18.000   1.3420   0.08306   0.07908  -0.0148   0.0120   1.0000
  18.250   1.3397   0.08728   0.08340  -0.0167   0.0120   1.0000
  18.500   1.3356   0.09183   0.08806  -0.0187   0.0119   1.0000
  18.750   1.3320   0.09642   0.09275  -0.0209   0.0118   1.0000
  19.000   1.3257   0.10153   0.09797  -0.0234   0.0118   1.0000
  19.250   1.3204   0.10660   0.10314  -0.0260   0.0117   1.0000
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