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NACA 63-215 AIRFOIL (n63215-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 63-215 AIRFOIL (n63215-il)
Reynolds number: 200,000
Max Cl/Cd: 59.48 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63215-il-200000-n5.txt
Download as CSV file: xf-n63215-il-200000-n5.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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.8485   0.09431   0.08982  -0.0316   1.0000   0.0214
 -15.750  -0.8792   0.08454   0.07978  -0.0378   1.0000   0.0214
 -15.500  -0.8944   0.07830   0.07338  -0.0415   1.0000   0.0215
 -15.250  -0.9083   0.07262   0.06753  -0.0447   1.0000   0.0216
 -15.000  -0.9187   0.06780   0.06255  -0.0472   1.0000   0.0217
 -14.750  -0.9262   0.06370   0.05832  -0.0491   1.0000   0.0219
 -14.500  -0.9318   0.06002   0.05451  -0.0507   1.0000   0.0222
 -14.250  -0.9375   0.05637   0.05069  -0.0520   1.0000   0.0223
 -14.000  -0.9395   0.05346   0.04766  -0.0530   1.0000   0.0228
 -13.750  -0.9417   0.05045   0.04450  -0.0536   1.0000   0.0230
 -13.500  -0.9424   0.04778   0.04167  -0.0541   1.0000   0.0235
 -13.250  -0.9418   0.04523   0.03893  -0.0543   1.0000   0.0240
 -13.000  -0.9395   0.04290   0.03641  -0.0542   1.0000   0.0245
 -12.750  -0.9358   0.04071   0.03402  -0.0540   1.0000   0.0250
 -12.500  -0.9299   0.03874   0.03183  -0.0535   1.0000   0.0254
 -12.250  -0.9202   0.03704   0.03011  -0.0530   1.0000   0.0259
 -12.000  -0.9100   0.03555   0.02858  -0.0525   1.0000   0.0263
 -11.750  -0.8996   0.03416   0.02715  -0.0519   1.0000   0.0269
 -11.500  -0.8886   0.03281   0.02573  -0.0512   1.0000   0.0275
 -11.250  -0.8773   0.03156   0.02440  -0.0505   1.0000   0.0283
 -11.000  -0.8653   0.03037   0.02311  -0.0497   1.0000   0.0293
 -10.750  -0.8525   0.02924   0.02185  -0.0488   1.0000   0.0302
 -10.500  -0.8402   0.02806   0.02063  -0.0477   1.0000   0.0311
 -10.250  -0.8292   0.02699   0.01956  -0.0466   1.0000   0.0319
 -10.000  -0.8185   0.02605   0.01861  -0.0452   1.0000   0.0328
  -9.750  -0.8090   0.02518   0.01772  -0.0435   1.0000   0.0337
  -9.500  -0.7960   0.02432   0.01682  -0.0422   0.9938   0.0349
  -9.250  -0.7657   0.02335   0.01572  -0.0441   0.9680   0.0365
  -9.000  -0.7377   0.02225   0.01460  -0.0458   0.9496   0.0384
  -8.750  -0.7112   0.02145   0.01374  -0.0468   0.9334   0.0406
  -8.500  -0.6883   0.02075   0.01293  -0.0468   0.9179   0.0427
  -8.250  -0.6686   0.02005   0.01215  -0.0461   0.9034   0.0448
  -8.000  -0.6497   0.01939   0.01145  -0.0453   0.8907   0.0474
  -7.750  -0.6295   0.01884   0.01081  -0.0445   0.8794   0.0503
  -7.500  -0.6097   0.01827   0.01017  -0.0436   0.8683   0.0536
  -7.250  -0.5897   0.01771   0.00957  -0.0427   0.8583   0.0578
  -7.000  -0.5686   0.01722   0.00900  -0.0419   0.8493   0.0626
  -6.750  -0.5474   0.01667   0.00844  -0.0412   0.8399   0.0697
  -6.500  -0.5259   0.01614   0.00790  -0.0404   0.8319   0.0807
  -6.250  -0.5036   0.01560   0.00739  -0.0399   0.8231   0.0978
  -6.000  -0.4817   0.01501   0.00689  -0.0393   0.8156   0.1249
  -5.750  -0.4597   0.01434   0.00640  -0.0389   0.8073   0.1653
  -5.500  -0.4382   0.01362   0.00589  -0.0384   0.8000   0.2207
  -5.250  -0.4162   0.01288   0.00544  -0.0381   0.7924   0.2896
  -5.000  -0.3930   0.01232   0.00515  -0.0377   0.7850   0.3577
  -4.750  -0.3678   0.01202   0.00496  -0.0374   0.7783   0.4094
  -4.500  -0.3415   0.01183   0.00486  -0.0372   0.7708   0.4468
  -4.250  -0.3150   0.01172   0.00477  -0.0369   0.7648   0.4795
  -4.000  -0.2877   0.01165   0.00471  -0.0368   0.7574   0.5068
  -3.750  -0.2604   0.01161   0.00466  -0.0366   0.7507   0.5260
  -3.500  -0.2326   0.01159   0.00458  -0.0365   0.7444   0.5410
  -3.250  -0.2047   0.01156   0.00451  -0.0365   0.7374   0.5544
  -3.000  -0.1770   0.01155   0.00447  -0.0363   0.7316   0.5672
  -2.750  -0.1489   0.01153   0.00443  -0.0363   0.7245   0.5774
  -2.500  -0.1206   0.01150   0.00432  -0.0364   0.7181   0.5858
  -2.250  -0.0924   0.01148   0.00425  -0.0364   0.7124   0.5927
  -2.000  -0.0640   0.01145   0.00420  -0.0365   0.7054   0.6001
  -1.750  -0.0357   0.01143   0.00411  -0.0365   0.6995   0.6071
  -1.500  -0.0074   0.01142   0.00409  -0.0366   0.6933   0.6136
  -1.250   0.0213   0.01141   0.00403  -0.0367   0.6869   0.6208
  -1.000   0.0494   0.01140   0.00399  -0.0367   0.6814   0.6265
  -0.750   0.0779   0.01140   0.00399  -0.0368   0.6747   0.6330
  -0.500   0.1065   0.01140   0.00395  -0.0370   0.6688   0.6395
  -0.250   0.1347   0.01141   0.00396  -0.0370   0.6636   0.6451
   0.000   0.1632   0.01142   0.00398  -0.0371   0.6567   0.6519
   0.250   0.1916   0.01144   0.00398  -0.0372   0.6510   0.6578
   0.500   0.2198   0.01147   0.00401  -0.0372   0.6455   0.6638
   0.750   0.2485   0.01150   0.00405  -0.0374   0.6391   0.6710
   1.000   0.2765   0.01153   0.00409  -0.0374   0.6335   0.6766
   1.250   0.3048   0.01157   0.00416  -0.0375   0.6277   0.6830
   1.500   0.3333   0.01161   0.00423  -0.0376   0.6213   0.6899
   1.750   0.3612   0.01166   0.00429  -0.0375   0.6159   0.6959
   2.000   0.3895   0.01172   0.00439  -0.0377   0.6093   0.7030
   2.250   0.4174   0.01177   0.00448  -0.0377   0.6029   0.7091
   2.500   0.4453   0.01184   0.00458  -0.0376   0.5970   0.7159
   2.750   0.4735   0.01191   0.00470  -0.0377   0.5898   0.7233
   3.000   0.5010   0.01197   0.00481  -0.0376   0.5837   0.7293
   3.250   0.5289   0.01205   0.00495  -0.0376   0.5765   0.7368
   3.500   0.5563   0.01213   0.00507  -0.0375   0.5691   0.7435
   3.750   0.5835   0.01220   0.00522  -0.0373   0.5600   0.7506
   4.000   0.6107   0.01227   0.00529  -0.0371   0.5491   0.7580
   4.250   0.6370   0.01234   0.00543  -0.0368   0.5369   0.7649
   4.750   0.6898   0.01251   0.00572  -0.0362   0.5113   0.7797
   5.000   0.7157   0.01262   0.00585  -0.0358   0.4943   0.7880
   5.250   0.7398   0.01276   0.00598  -0.0351   0.4703   0.7953
   5.500   0.7636   0.01295   0.00614  -0.0344   0.4400   0.8038
   5.750   0.7860   0.01322   0.00634  -0.0334   0.4068   0.8117
   6.000   0.8077   0.01358   0.00662  -0.0325   0.3679   0.8208
   6.250   0.8257   0.01414   0.00699  -0.0310   0.3186   0.8293
   6.500   0.8421   0.01488   0.00750  -0.0295   0.2666   0.8396
   6.750   0.8560   0.01569   0.00811  -0.0276   0.2177   0.8496
   7.000   0.8697   0.01652   0.00876  -0.0258   0.1751   0.8607
   7.250   0.8833   0.01731   0.00941  -0.0239   0.1416   0.8733
   7.750   0.9087   0.01871   0.01067  -0.0197   0.0948   0.9047
   8.000   0.9207   0.01937   0.01132  -0.0175   0.0801   0.9281
   8.250   0.9388   0.02010   0.01206  -0.0168   0.0683   0.9702
   8.500   0.9530   0.02089   0.01284  -0.0156   0.0612   1.0000
   8.750   0.9657   0.02180   0.01372  -0.0142   0.0559   1.0000
   9.000   0.9791   0.02269   0.01464  -0.0130   0.0517   1.0000
   9.250   0.9911   0.02369   0.01564  -0.0119   0.0478   1.0000
   9.500   1.0025   0.02477   0.01674  -0.0107   0.0450   1.0000
   9.750   1.0148   0.02582   0.01785  -0.0097   0.0424   1.0000
  10.000   1.0254   0.02702   0.01906  -0.0087   0.0401   1.0000
  10.250   1.0342   0.02839   0.02046  -0.0077   0.0382   1.0000
  10.500   1.0456   0.02963   0.02179  -0.0069   0.0366   1.0000
  10.750   1.0557   0.03100   0.02322  -0.0061   0.0351   1.0000
  11.000   1.0649   0.03247   0.02474  -0.0054   0.0338   1.0000
  11.250   1.0722   0.03415   0.02644  -0.0047   0.0327   1.0000
  11.500   1.0798   0.03584   0.02819  -0.0040   0.0316   1.0000
  11.750   1.0892   0.03743   0.02988  -0.0034   0.0305   1.0000
  12.000   1.0981   0.03909   0.03162  -0.0029   0.0293   1.0000
  12.250   1.1064   0.04082   0.03342  -0.0025   0.0284   1.0000
  12.500   1.1136   0.04268   0.03531  -0.0022   0.0274   1.0000
  12.750   1.1191   0.04476   0.03741  -0.0019   0.0267   1.0000
  13.000   1.1272   0.04666   0.03943  -0.0016   0.0260   1.0000
  13.250   1.1348   0.04865   0.04155  -0.0014   0.0252   1.0000
  13.500   1.1417   0.05074   0.04375  -0.0013   0.0246   1.0000
  13.750   1.1479   0.05293   0.04603  -0.0012   0.0239   1.0000
  14.000   1.1538   0.05520   0.04839  -0.0013   0.0234   1.0000
  14.250   1.1591   0.05758   0.05085  -0.0015   0.0230   1.0000
  14.500   1.1640   0.06005   0.05339  -0.0018   0.0226   1.0000
  14.750   1.1685   0.06262   0.05601  -0.0021   0.0222   1.0000
  15.000   1.1726   0.06534   0.05881  -0.0024   0.0219   1.0000
  15.250   1.1750   0.06838   0.06203  -0.0030   0.0216   1.0000
  15.500   1.1753   0.07177   0.06561  -0.0038   0.0212   1.0000
  15.750   1.1748   0.07535   0.06938  -0.0048   0.0209   1.0000
  16.000   1.1720   0.07936   0.07357  -0.0062   0.0206   1.0000
  16.250   1.1680   0.08364   0.07804  -0.0078   0.0203   1.0000
  16.500   1.1627   0.08826   0.08284  -0.0098   0.0200   1.0000
  16.750   1.1561   0.09323   0.08798  -0.0121   0.0198   1.0000
  17.000   1.1484   0.09853   0.09345  -0.0148   0.0195   1.0000
  17.250   1.1394   0.10423   0.09932  -0.0178   0.0193   1.0000
  17.500   1.1291   0.11037   0.10563  -0.0212   0.0191   1.0000
  17.750   1.1157   0.11734   0.11278  -0.0253   0.0190   1.0000
  18.000   1.1004   0.12503   0.12067  -0.0300   0.0189   1.0000
  18.250   1.0767   0.13499   0.13086  -0.0364   0.0189   1.0000
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