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NACA 63-415 AIRFOIL (n63415-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NACA 63-415 AIRFOIL (n63415-il)
Reynolds number: 200,000
Max Cl/Cd: 70.01 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63415-il-200000-n5.txt
Download as CSV file: xf-n63415-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-415 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7116   0.07866   0.07427  -0.0592   1.0000   0.0221
 -14.250  -0.7467   0.06920   0.06456  -0.0655   1.0000   0.0220
 -14.000  -0.7709   0.06247   0.05760  -0.0695   1.0000   0.0220
 -13.750  -0.7875   0.05734   0.05227  -0.0722   1.0000   0.0222
 -13.500  -0.8014   0.05289   0.04762  -0.0742   1.0000   0.0224
 -13.250  -0.8121   0.04910   0.04361  -0.0755   1.0000   0.0227
 -13.000  -0.8204   0.04579   0.04008  -0.0762   1.0000   0.0231
 -12.750  -0.8276   0.04277   0.03681  -0.0764   1.0000   0.0235
 -12.500  -0.8329   0.04014   0.03393  -0.0761   1.0000   0.0240
 -12.250  -0.8283   0.03842   0.03217  -0.0755   1.0000   0.0243
 -12.000  -0.8237   0.03689   0.03060  -0.0747   1.0000   0.0247
 -11.750  -0.8196   0.03555   0.02921  -0.0735   1.0000   0.0251
 -11.500  -0.8171   0.03421   0.02779  -0.0719   1.0000   0.0255
 -11.250  -0.8172   0.03301   0.02651  -0.0695   1.0000   0.0260
 -11.000  -0.8204   0.03199   0.02541  -0.0662   1.0000   0.0264
 -10.750  -0.8044   0.03056   0.02381  -0.0663   0.9913   0.0273
 -10.500  -0.7763   0.02904   0.02202  -0.0683   0.9811   0.0285
 -10.250  -0.7472   0.02768   0.02063  -0.0704   0.9718   0.0295
 -10.000  -0.7183   0.02657   0.01947  -0.0721   0.9612   0.0306
  -9.750  -0.6894   0.02545   0.01824  -0.0737   0.9510   0.0318
  -9.500  -0.6597   0.02435   0.01698  -0.0752   0.9414   0.0332
  -9.250  -0.6322   0.02331   0.01584  -0.0762   0.9306   0.0346
  -9.000  -0.6068   0.02245   0.01495  -0.0769   0.9195   0.0361
  -8.750  -0.5812   0.02168   0.01410  -0.0774   0.9092   0.0378
  -8.500  -0.5582   0.02096   0.01328  -0.0772   0.8981   0.0394
  -8.250  -0.5364   0.02024   0.01246  -0.0768   0.8877   0.0410
  -8.000  -0.5150   0.01954   0.01172  -0.0763   0.8781   0.0428
  -7.750  -0.4936   0.01898   0.01111  -0.0758   0.8680   0.0451
  -7.500  -0.4709   0.01846   0.01047  -0.0753   0.8596   0.0474
  -7.250  -0.4498   0.01783   0.00981  -0.0747   0.8502   0.0500
  -7.000  -0.4267   0.01732   0.00924  -0.0743   0.8426   0.0530
  -6.750  -0.4033   0.01688   0.00870  -0.0739   0.8339   0.0564
  -6.500  -0.3800   0.01633   0.00812  -0.0735   0.8268   0.0608
  -6.250  -0.3557   0.01591   0.00764  -0.0732   0.8186   0.0663
  -6.000  -0.3314   0.01541   0.00713  -0.0730   0.8115   0.0743
  -5.750  -0.3067   0.01494   0.00668  -0.0729   0.8042   0.0873
  -5.500  -0.2820   0.01442   0.00623  -0.0728   0.7969   0.1103
  -5.250  -0.2570   0.01388   0.00580  -0.0728   0.7905   0.1478
  -5.000  -0.2323   0.01323   0.00538  -0.0729   0.7830   0.2017
  -4.750  -0.2076   0.01251   0.00496  -0.0731   0.7767   0.2812
  -4.500  -0.1820   0.01196   0.00473  -0.0732   0.7698   0.3617
  -4.250  -0.1550   0.01171   0.00461  -0.0733   0.7631   0.4161
  -4.000  -0.1273   0.01158   0.00451  -0.0733   0.7572   0.4540
  -3.750  -0.0996   0.01151   0.00449  -0.0733   0.7501   0.4885
  -3.500  -0.0718   0.01148   0.00447  -0.0732   0.7441   0.5164
  -3.250  -0.0436   0.01148   0.00444  -0.0732   0.7379   0.5362
  -3.000  -0.0155   0.01147   0.00441  -0.0732   0.7311   0.5508
  -2.750   0.0127   0.01149   0.00437  -0.0731   0.7256   0.5651
  -2.500   0.0409   0.01150   0.00437  -0.0731   0.7190   0.5776
  -2.250   0.0695   0.01149   0.00429  -0.0732   0.7126   0.5871
  -2.000   0.0978   0.01149   0.00424  -0.0732   0.7072   0.5942
  -1.750   0.1263   0.01149   0.00421  -0.0734   0.7006   0.6021
  -1.500   0.1547   0.01149   0.00417  -0.0734   0.6947   0.6092
  -1.250   0.1831   0.01150   0.00414  -0.0735   0.6890   0.6162
  -1.000   0.2118   0.01151   0.00411  -0.0737   0.6825   0.6235
  -0.750   0.2400   0.01152   0.00411  -0.0736   0.6771   0.6293
  -0.500   0.2686   0.01154   0.00410  -0.0738   0.6713   0.6361
  -0.250   0.2970   0.01156   0.00412  -0.0739   0.6649   0.6425
   0.000   0.3253   0.01159   0.00413  -0.0739   0.6596   0.6485
   0.250   0.3539   0.01163   0.00415  -0.0741   0.6539   0.6554
   0.500   0.3820   0.01167   0.00421  -0.0742   0.6478   0.6612
   0.750   0.4103   0.01172   0.00424  -0.0742   0.6426   0.6678
   1.000   0.4389   0.01177   0.00430  -0.0744   0.6367   0.6749
   1.250   0.4666   0.01182   0.00440  -0.0743   0.6308   0.6804
   1.500   0.4950   0.01189   0.00444  -0.0744   0.6257   0.6875
   1.750   0.5230   0.01195   0.00456  -0.0745   0.6194   0.6942
   2.000   0.5507   0.01202   0.00467  -0.0745   0.6134   0.7005
   2.250   0.5793   0.01211   0.00472  -0.0746   0.6082   0.7080
   2.500   0.6065   0.01218   0.00489  -0.0745   0.6014   0.7142
   2.750   0.6343   0.01226   0.00500  -0.0745   0.5953   0.7215
   3.000   0.6621   0.01236   0.00512  -0.0745   0.5892   0.7284
   3.250   0.6892   0.01244   0.00529  -0.0743   0.5824   0.7353
   3.500   0.7172   0.01255   0.00540  -0.0744   0.5765   0.7433
   3.750   0.7437   0.01264   0.00560  -0.0741   0.5692   0.7497
   4.000   0.7710   0.01275   0.00574  -0.0740   0.5620   0.7577
   4.250   0.7971   0.01284   0.00592  -0.0737   0.5529   0.7647
   4.500   0.8233   0.01294   0.00603  -0.0733   0.5425   0.7727
   4.750   0.8488   0.01304   0.00621  -0.0729   0.5308   0.7802
   5.000   0.8742   0.01315   0.00640  -0.0724   0.5195   0.7883
   5.250   0.8992   0.01328   0.00657  -0.0718   0.5068   0.7965
   5.500   0.9233   0.01342   0.00674  -0.0711   0.4919   0.8050
   5.750   0.9463   0.01359   0.00693  -0.0702   0.4704   0.8137
   6.000   0.9675   0.01382   0.00712  -0.0690   0.4421   0.8232
   6.250   0.9873   0.01413   0.00736  -0.0677   0.4103   0.8325
   6.750   1.0225   0.01502   0.00807  -0.0644   0.3395   0.8540
   7.000   1.0350   0.01572   0.00859  -0.0620   0.2958   0.8661
   7.250   1.0445   0.01653   0.00922  -0.0593   0.2516   0.8802
   7.500   1.0515   0.01738   0.00990  -0.0561   0.2121   0.8980
   7.750   1.0577   0.01818   0.01058  -0.0529   0.1795   0.9226
   8.000   1.0654   0.01893   0.01124  -0.0502   0.1513   1.0000
   8.250   1.0759   0.01996   0.01212  -0.0484   0.1249   1.0000
   8.500   1.0858   0.02103   0.01308  -0.0467   0.1035   1.0000
   8.750   1.0953   0.02216   0.01413  -0.0450   0.0863   1.0000
   9.000   1.1049   0.02332   0.01523  -0.0435   0.0739   1.0000
   9.250   1.1149   0.02450   0.01639  -0.0421   0.0649   1.0000
   9.500   1.1246   0.02574   0.01763  -0.0408   0.0583   1.0000
   9.750   1.1333   0.02710   0.01897  -0.0395   0.0530   1.0000
  10.000   1.1435   0.02839   0.02032  -0.0384   0.0490   1.0000
  10.250   1.1520   0.02985   0.02179  -0.0373   0.0456   1.0000
  10.500   1.1607   0.03134   0.02332  -0.0364   0.0429   1.0000
  10.750   1.1699   0.03283   0.02488  -0.0355   0.0404   1.0000
  11.000   1.1771   0.03453   0.02661  -0.0347   0.0383   1.0000
  11.250   1.1837   0.03634   0.02848  -0.0339   0.0367   1.0000
  11.500   1.1919   0.03803   0.03027  -0.0333   0.0350   1.0000
  11.750   1.1993   0.03986   0.03216  -0.0327   0.0334   1.0000
  12.000   1.2048   0.04189   0.03424  -0.0322   0.0321   1.0000
  12.250   1.2087   0.04413   0.03653  -0.0317   0.0310   1.0000
  12.500   1.2157   0.04613   0.03864  -0.0313   0.0299   1.0000
  12.750   1.2215   0.04828   0.04089  -0.0310   0.0289   1.0000
  13.000   1.2267   0.05053   0.04322  -0.0308   0.0279   1.0000
  13.250   1.2314   0.05290   0.04565  -0.0307   0.0271   1.0000
  13.500   1.2346   0.05549   0.04828  -0.0307   0.0264   1.0000
  13.750   1.2387   0.05804   0.05091  -0.0306   0.0257   1.0000
  14.000   1.2444   0.06048   0.05348  -0.0307   0.0250   1.0000
  14.250   1.2497   0.06304   0.05615  -0.0308   0.0242   1.0000
  14.500   1.2544   0.06569   0.05891  -0.0311   0.0236   1.0000
  14.750   1.2585   0.06847   0.06178  -0.0315   0.0229   1.0000
  15.000   1.2619   0.07138   0.06476  -0.0321   0.0224   1.0000
  15.250   1.2649   0.07439   0.06782  -0.0327   0.0219   1.0000
  15.500   1.2678   0.07746   0.07097  -0.0333   0.0214   1.0000
  15.750   1.2705   0.08070   0.07439  -0.0340   0.0209   1.0000
  16.000   1.2727   0.08404   0.07788  -0.0348   0.0205   1.0000
  16.250   1.2740   0.08757   0.08156  -0.0358   0.0201   1.0000
  16.500   1.2745   0.09128   0.08542  -0.0370   0.0198   1.0000
  16.750   1.2741   0.09520   0.08949  -0.0384   0.0194   1.0000
  17.000   1.2731   0.09925   0.09368  -0.0399   0.0192   1.0000
  17.250   1.2714   0.10349   0.09805  -0.0417   0.0189   1.0000
  17.500   1.2692   0.10790   0.10259  -0.0436   0.0187   1.0000
  17.750   1.2666   0.11244   0.10725  -0.0458   0.0185   1.0000
  18.000   1.2634   0.11713   0.11207  -0.0481   0.0183   1.0000
  18.250   1.2598   0.12197   0.11703  -0.0507   0.0182   1.0000
  18.500   1.2559   0.12691   0.12209  -0.0533   0.0180   1.0000
  18.750   1.2515   0.13202   0.12731  -0.0562   0.0179   1.0000
  19.000   1.2429   0.13819   0.13364  -0.0600   0.0177   1.0000
  19.250   1.2289   0.14583   0.14150  -0.0649   0.0177   1.0000
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