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NACA 63(2)-215 MOD B (n63215b-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 63(2)-215 MOD B (n63215b-il)
Reynolds number: 200,000
Max Cl/Cd: 47.85 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63215b-il-200000-n5.txt
Download as CSV file: xf-n63215b-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63(2)-215 MOD B                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7921   0.10984   0.10523  -0.0204   1.0000   0.0207
 -16.250  -0.8386   0.09558   0.09065  -0.0298   1.0000   0.0205
 -16.000  -0.8681   0.08597   0.08080  -0.0360   1.0000   0.0205
 -15.750  -0.8901   0.07844   0.07303  -0.0405   1.0000   0.0206
 -15.500  -0.9066   0.07231   0.06668  -0.0439   1.0000   0.0207
 -15.250  -0.9209   0.06688   0.06101  -0.0467   1.0000   0.0209
 -15.000  -0.9327   0.06212   0.05601  -0.0488   1.0000   0.0211
 -14.750  -0.9392   0.05828   0.05199  -0.0502   1.0000   0.0213
 -14.500  -0.9382   0.05554   0.04921  -0.0509   1.0000   0.0216
 -14.250  -0.9371   0.05287   0.04646  -0.0516   1.0000   0.0218
 -14.000  -0.9354   0.05032   0.04382  -0.0520   1.0000   0.0220
 -13.750  -0.9325   0.04800   0.04142  -0.0523   1.0000   0.0223
 -13.500  -0.9288   0.04581   0.03914  -0.0525   1.0000   0.0227
 -13.250  -0.9244   0.04369   0.03693  -0.0524   1.0000   0.0231
 -13.000  -0.9193   0.04170   0.03482  -0.0522   1.0000   0.0236
 -12.750  -0.9131   0.03984   0.03283  -0.0519   1.0000   0.0242
 -12.500  -0.9064   0.03803   0.03085  -0.0514   1.0000   0.0250
 -12.250  -0.8980   0.03642   0.02912  -0.0509   1.0000   0.0257
 -12.000  -0.8881   0.03501   0.02772  -0.0502   1.0000   0.0262
 -11.750  -0.8779   0.03372   0.02641  -0.0496   1.0000   0.0268
 -11.500  -0.8671   0.03247   0.02512  -0.0488   1.0000   0.0275
 -11.250  -0.8557   0.03127   0.02387  -0.0479   1.0000   0.0283
 -11.000  -0.8437   0.03013   0.02264  -0.0470   1.0000   0.0292
 -10.750  -0.8311   0.02905   0.02146  -0.0459   1.0000   0.0300
 -10.500  -0.8191   0.02796   0.02032  -0.0447   1.0000   0.0307
 -10.250  -0.8085   0.02691   0.01931  -0.0434   1.0000   0.0315
 -10.000  -0.7980   0.02601   0.01840  -0.0419   1.0000   0.0322
  -9.750  -0.7885   0.02521   0.01759  -0.0400   1.0000   0.0332
  -9.500  -0.7814   0.02449   0.01686  -0.0376   1.0000   0.0341
  -9.250  -0.7585   0.02373   0.01602  -0.0379   0.9842   0.0357
  -9.000  -0.7287   0.02269   0.01498  -0.0397   0.9648   0.0375
  -8.750  -0.6983   0.02188   0.01415  -0.0413   0.9499   0.0396
  -8.500  -0.6705   0.02115   0.01335  -0.0422   0.9351   0.0416
  -8.000  -0.6264   0.01970   0.01181  -0.0416   0.9082   0.0452
  -7.750  -0.6059   0.01912   0.01119  -0.0407   0.8960   0.0470
  -7.500  -0.5852   0.01860   0.01059  -0.0398   0.8851   0.0490
  -7.250  -0.5652   0.01806   0.01001  -0.0387   0.8750   0.0518
  -7.000  -0.5445   0.01755   0.00947  -0.0377   0.8655   0.0553
  -6.750  -0.5226   0.01712   0.00897  -0.0368   0.8577   0.0597
  -6.500  -0.5014   0.01658   0.00845  -0.0359   0.8490   0.0657
  -6.250  -0.4793   0.01610   0.00797  -0.0351   0.8417   0.0749
  -6.000  -0.4567   0.01560   0.00753  -0.0344   0.8337   0.0910
  -5.750  -0.4343   0.01507   0.00709  -0.0337   0.8267   0.1157
  -5.500  -0.4117   0.01450   0.00667  -0.0331   0.8200   0.1494
  -5.250  -0.3892   0.01386   0.00624  -0.0326   0.8133   0.1952
  -5.000  -0.3671   0.01316   0.00580  -0.0320   0.8078   0.2604
  -4.750  -0.3443   0.01249   0.00550  -0.0316   0.8007   0.3367
  -4.500  -0.3196   0.01211   0.00534  -0.0311   0.7947   0.3981
  -4.000  -0.2661   0.01180   0.00522  -0.0305   0.7827   0.4760
  -3.750  -0.2390   0.01173   0.00517  -0.0301   0.7767   0.5016
  -3.500  -0.2116   0.01168   0.00512  -0.0297   0.7679   0.5225
  -3.250  -0.1842   0.01164   0.00503  -0.0292   0.7589   0.5387
  -3.000  -0.1567   0.01161   0.00499  -0.0288   0.7478   0.5558
  -2.750  -0.1293   0.01160   0.00495  -0.0284   0.7383   0.5715
  -2.500  -0.1014   0.01156   0.00488  -0.0280   0.7285   0.5809
  -2.250  -0.0729   0.01154   0.00480  -0.0279   0.7204   0.5898
  -2.000  -0.0448   0.01150   0.00476  -0.0276   0.7125   0.5972
  -1.750  -0.0163   0.01148   0.00468  -0.0275   0.7044   0.6043
  -1.500   0.0121   0.01144   0.00460  -0.0274   0.6955   0.6105
  -1.250   0.0404   0.01141   0.00457  -0.0272   0.6858   0.6165
  -1.000   0.0689   0.01140   0.00446  -0.0270   0.6752   0.6237
  -0.750   0.0968   0.01137   0.00444  -0.0267   0.6625   0.6297
  -0.500   0.1251   0.01135   0.00439  -0.0266   0.6492   0.6364
  -0.250   0.1533   0.01134   0.00432  -0.0264   0.6348   0.6426
   0.000   0.1810   0.01134   0.00429  -0.0261   0.6184   0.6479
   0.250   0.2090   0.01136   0.00425  -0.0259   0.5996   0.6546
   0.500   0.2363   0.01140   0.00421  -0.0255   0.5735   0.6606
   0.750   0.2628   0.01149   0.00419  -0.0250   0.5367   0.6667
   1.000   0.2878   0.01174   0.00413  -0.0243   0.4675   0.6735
   1.250   0.3081   0.01239   0.00427  -0.0231   0.3651   0.6791
   1.500   0.3327   0.01279   0.00448  -0.0226   0.3370   0.6864
   1.750   0.3585   0.01306   0.00468  -0.0222   0.3161   0.6932
   2.000   0.3843   0.01332   0.00487  -0.0219   0.2976   0.6996
   2.500   0.4361   0.01381   0.00523  -0.0212   0.2677   0.7128
   2.750   0.4622   0.01405   0.00542  -0.0209   0.2549   0.7200
   3.000   0.4883   0.01427   0.00560  -0.0206   0.2433   0.7265
   3.250   0.5138   0.01451   0.00581  -0.0201   0.2330   0.7329
   3.500   0.5399   0.01477   0.00601  -0.0199   0.2229   0.7404
   3.750   0.5651   0.01499   0.00624  -0.0194   0.2146   0.7467
   4.000   0.5905   0.01526   0.00648  -0.0190   0.2072   0.7547
   4.250   0.6155   0.01550   0.00674  -0.0185   0.2009   0.7618
   4.500   0.6408   0.01575   0.00699  -0.0181   0.1945   0.7699
   4.750   0.6649   0.01606   0.00728  -0.0175   0.1889   0.7771
   5.000   0.6900   0.01629   0.00756  -0.0170   0.1836   0.7849
   5.250   0.7145   0.01655   0.00784  -0.0164   0.1781   0.7928
   5.750   0.7621   0.01713   0.00845  -0.0152   0.1680   0.8089
   6.000   0.7852   0.01741   0.00876  -0.0144   0.1631   0.8171
   6.250   0.8075   0.01775   0.00910  -0.0135   0.1589   0.8258
   6.500   0.8299   0.01807   0.00946  -0.0126   0.1553   0.8354
   6.750   0.8521   0.01836   0.00982  -0.0117   0.1514   0.8450
   7.250   0.8932   0.01906   0.01056  -0.0094   0.1440   0.8668
   7.500   0.9129   0.01941   0.01095  -0.0081   0.1404   0.8795
   7.750   0.9326   0.01969   0.01132  -0.0067   0.1366   0.8945
   8.000   0.9504   0.01998   0.01168  -0.0051   0.1329   0.9137
   8.250   0.9688   0.02034   0.01206  -0.0037   0.1296   0.9414
   8.500   0.9950   0.02081   0.01254  -0.0041   0.1264   1.0000
   8.750   1.0183   0.02128   0.01308  -0.0039   0.1234   1.0000
   9.000   1.0397   0.02177   0.01360  -0.0034   0.1205   1.0000
   9.250   1.0593   0.02230   0.01414  -0.0026   0.1179   1.0000
   9.500   1.0773   0.02291   0.01473  -0.0017   0.1155   1.0000
   9.750   1.0941   0.02364   0.01542  -0.0007   0.1132   1.0000
  10.000   1.1135   0.02422   0.01609   0.0000   0.1113   1.0000
  10.250   1.1319   0.02485   0.01679   0.0008   0.1089   1.0000
  10.500   1.1492   0.02551   0.01751   0.0017   0.1066   1.0000
  10.750   1.1654   0.02622   0.01826   0.0026   0.1044   1.0000
  11.000   1.1802   0.02701   0.01907   0.0035   0.1024   1.0000
  11.250   1.1938   0.02793   0.01997   0.0045   0.1005   1.0000
  11.500   1.2086   0.02886   0.02095   0.0053   0.0989   1.0000
  11.750   1.2239   0.02975   0.02195   0.0061   0.0974   1.0000
  12.000   1.2381   0.03071   0.02301   0.0068   0.0957   1.0000
  12.250   1.2514   0.03174   0.02413   0.0076   0.0941   1.0000
  12.500   1.2638   0.03284   0.02529   0.0083   0.0926   1.0000
  12.750   1.2752   0.03400   0.02653   0.0090   0.0912   1.0000
  13.000   1.2855   0.03527   0.02785   0.0097   0.0898   1.0000
  13.250   1.2949   0.03666   0.02927   0.0103   0.0886   1.0000
  13.500   1.3037   0.03819   0.03081   0.0108   0.0873   1.0000
  13.750   1.3125   0.03975   0.03247   0.0113   0.0862   1.0000
  14.000   1.3203   0.04141   0.03428   0.0117   0.0851   1.0000
  14.250   1.3267   0.04321   0.03622   0.0119   0.0839   1.0000
  14.500   1.3321   0.04515   0.03829   0.0121   0.0826   1.0000
  14.750   1.3365   0.04724   0.04049   0.0121   0.0815   1.0000
  15.000   1.3400   0.04946   0.04282   0.0120   0.0804   1.0000
  15.250   1.3424   0.05186   0.04533   0.0117   0.0795   1.0000
  15.500   1.3438   0.05443   0.04800   0.0113   0.0787   1.0000
  15.750   1.3443   0.05719   0.05085   0.0107   0.0778   1.0000
  16.000   1.3441   0.06013   0.05386   0.0099   0.0770   1.0000
  16.250   1.3436   0.06322   0.05703   0.0090   0.0762   1.0000
  16.500   1.3438   0.06634   0.06021   0.0082   0.0753   1.0000
  16.750   1.3365   0.07059   0.06463   0.0064   0.0746   1.0000
  17.000   1.3240   0.07585   0.07010   0.0039   0.0741   1.0000
  17.250   1.3063   0.08222   0.07671   0.0004   0.0734   1.0000
  17.500   1.2815   0.09020   0.08493  -0.0042   0.0727   1.0000
  17.750   1.2368   0.10251   0.09756  -0.0120   0.0720   1.0000
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