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NACA 63-015A AIRFOIL (n63015a-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 63-015A AIRFOIL (n63015a-il)
Reynolds number: 500,000
Max Cl/Cd: 55.25 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n63015a-il-500000-n5.txt
Download as CSV file: xf-n63015a-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 63-015A AIRFOIL                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0441   0.13855   0.13524   0.0097   1.0000   0.0118
 -19.500  -1.0606   0.13090   0.12746   0.0053   1.0000   0.0118
 -19.250  -1.0755   0.12380   0.12023   0.0014   1.0000   0.0119
 -19.000  -1.0898   0.11700   0.11331  -0.0022   1.0000   0.0119
 -18.750  -1.1029   0.11063   0.10682  -0.0055   1.0000   0.0120
 -18.500  -1.1150   0.10452   0.10059  -0.0086   1.0000   0.0120
 -18.250  -1.1261   0.09875   0.09470  -0.0114   1.0000   0.0121
 -18.000  -1.1364   0.09326   0.08910  -0.0140   1.0000   0.0121
 -17.750  -1.1454   0.08808   0.08381  -0.0163   1.0000   0.0122
 -17.500  -1.1534   0.08318   0.07879  -0.0184   1.0000   0.0122
 -17.250  -1.1602   0.07856   0.07406  -0.0204   1.0000   0.0123
 -17.000  -1.1662   0.07420   0.06959  -0.0221   1.0000   0.0124
 -16.750  -1.1710   0.07010   0.06539  -0.0236   1.0000   0.0124
 -16.500  -1.1745   0.06627   0.06145  -0.0249   1.0000   0.0125
 -16.250  -1.1773   0.06266   0.05774  -0.0260   1.0000   0.0126
 -16.000  -1.1791   0.05928   0.05426  -0.0270   1.0000   0.0127
 -15.750  -1.1798   0.05610   0.05098  -0.0277   1.0000   0.0128
 -15.500  -1.1795   0.05316   0.04794  -0.0284   1.0000   0.0129
 -15.250  -1.1786   0.05038   0.04507  -0.0288   1.0000   0.0131
 -15.000  -1.1765   0.04781   0.04240  -0.0291   1.0000   0.0132
 -14.750  -1.1737   0.04536   0.03986  -0.0292   1.0000   0.0134
 -14.500  -1.1702   0.04306   0.03745  -0.0293   1.0000   0.0136
 -14.250  -1.1658   0.04087   0.03517  -0.0292   1.0000   0.0137
 -14.000  -1.1607   0.03879   0.03301  -0.0290   1.0000   0.0139
 -13.750  -1.1550   0.03682   0.03094  -0.0287   1.0000   0.0140
 -13.500  -1.1484   0.03498   0.02900  -0.0284   1.0000   0.0141
 -13.250  -1.1410   0.03324   0.02718  -0.0279   1.0000   0.0143
 -13.000  -1.1327   0.03162   0.02548  -0.0274   1.0000   0.0144
 -12.750  -1.1235   0.03012   0.02389  -0.0268   1.0000   0.0146
 -12.500  -1.1151   0.02860   0.02229  -0.0260   1.0000   0.0147
 -12.250  -1.1075   0.02706   0.02069  -0.0251   1.0000   0.0150
 -12.000  -1.0979   0.02574   0.01931  -0.0242   1.0000   0.0152
 -11.750  -1.0869   0.02458   0.01810  -0.0232   1.0000   0.0155
 -11.500  -1.0749   0.02355   0.01702  -0.0221   1.0000   0.0158
 -11.250  -1.0622   0.02261   0.01603  -0.0209   1.0000   0.0161
 -11.000  -1.0488   0.02176   0.01512  -0.0196   1.0000   0.0164
 -10.750  -1.0350   0.02099   0.01430  -0.0183   1.0000   0.0169
 -10.500  -1.0209   0.02029   0.01355  -0.0168   1.0000   0.0173
 -10.250  -1.0066   0.01966   0.01287  -0.0151   1.0000   0.0178
 -10.000  -0.9934   0.01904   0.01221  -0.0132   1.0000   0.0183
  -9.750  -0.9805   0.01841   0.01155  -0.0111   1.0000   0.0189
  -9.500  -0.9649   0.01787   0.01099  -0.0095   1.0000   0.0196
  -9.250  -0.9490   0.01738   0.01048  -0.0077   1.0000   0.0205
  -9.000  -0.9322   0.01693   0.00999  -0.0061   0.9992   0.0214
  -8.750  -0.9024   0.01636   0.00939  -0.0073   0.9891   0.0228
  -8.500  -0.8728   0.01580   0.00883  -0.0084   0.9773   0.0248
  -8.250  -0.8425   0.01534   0.00832  -0.0094   0.9638   0.0269
  -8.000  -0.8140   0.01483   0.00781  -0.0101   0.9480   0.0300
  -7.750  -0.7874   0.01444   0.00737  -0.0102   0.9296   0.0332
  -7.500  -0.7641   0.01404   0.00694  -0.0096   0.9100   0.0376
  -7.250  -0.7415   0.01369   0.00656  -0.0088   0.8910   0.0428
  -7.000  -0.7189   0.01335   0.00618  -0.0080   0.8735   0.0500
  -6.750  -0.6962   0.01301   0.00583  -0.0073   0.8578   0.0593
  -6.500  -0.6731   0.01267   0.00548  -0.0066   0.8434   0.0706
  -6.000  -0.6261   0.01199   0.00483  -0.0054   0.8181   0.1009
  -5.750  -0.6033   0.01156   0.00449  -0.0048   0.8071   0.1278
  -5.500  -0.5809   0.01109   0.00414  -0.0041   0.7968   0.1642
  -5.000  -0.5357   0.01009   0.00347  -0.0028   0.7779   0.2535
  -4.750  -0.5134   0.00957   0.00315  -0.0021   0.7689   0.3079
  -4.500  -0.4907   0.00911   0.00289  -0.0014   0.7608   0.3655
  -4.250  -0.4668   0.00876   0.00271  -0.0009   0.7523   0.4140
  -4.000  -0.4412   0.00857   0.00258  -0.0005   0.7448   0.4444
  -3.750  -0.4147   0.00843   0.00247  -0.0003   0.7369   0.4653
  -3.500  -0.3879   0.00833   0.00237  -0.0002   0.7296   0.4822
  -3.250  -0.3607   0.00823   0.00228  -0.0001   0.7219   0.4977
  -3.000  -0.3338   0.00815   0.00220   0.0001   0.7147   0.5168
  -2.750  -0.3066   0.00807   0.00214   0.0002   0.7074   0.5337
  -2.500  -0.2794   0.00801   0.00208   0.0003   0.7000   0.5469
  -2.250  -0.2519   0.00795   0.00202   0.0003   0.6932   0.5591
  -2.000  -0.2241   0.00791   0.00197   0.0003   0.6857   0.5702
  -1.750  -0.1964   0.00788   0.00193   0.0004   0.6789   0.5799
  -1.500  -0.1684   0.00785   0.00189   0.0003   0.6716   0.5873
  -1.000  -0.1122   0.00782   0.00182   0.0002   0.6575   0.6015
  -0.750  -0.0844   0.00780   0.00180   0.0002   0.6505   0.6086
  -0.500  -0.0560   0.00780   0.00178   0.0001   0.6436   0.6157
  -0.250  -0.0281   0.00778   0.00177   0.0001   0.6363   0.6224
   0.000   0.0000   0.00779   0.00177   0.0000   0.6297   0.6297
   0.250   0.0281   0.00778   0.00177  -0.0001   0.6224   0.6363
   0.500   0.0560   0.00780   0.00178  -0.0001   0.6157   0.6436
   0.750   0.0844   0.00780   0.00180  -0.0002   0.6086   0.6504
   1.000   0.1122   0.00782   0.00182  -0.0002   0.6015   0.6575
   1.500   0.1684   0.00785   0.00189  -0.0003   0.5872   0.6715
   1.750   0.1964   0.00788   0.00193  -0.0004   0.5799   0.6788
   2.000   0.2241   0.00791   0.00197  -0.0003   0.5702   0.6857
   2.250   0.2519   0.00795   0.00202  -0.0003   0.5591   0.6932
   2.500   0.2794   0.00801   0.00208  -0.0003   0.5469   0.7000
   2.750   0.3066   0.00807   0.00214  -0.0002   0.5338   0.7074
   3.000   0.3338   0.00815   0.00220  -0.0001   0.5169   0.7147
   3.250   0.3607   0.00823   0.00228   0.0001   0.4977   0.7219
   3.500   0.3879   0.00833   0.00237   0.0002   0.4822   0.7296
   3.750   0.4147   0.00843   0.00247   0.0003   0.4654   0.7370
   4.000   0.4412   0.00856   0.00258   0.0005   0.4445   0.7448
   4.250   0.4668   0.00876   0.00271   0.0009   0.4138   0.7524
   4.500   0.4907   0.00911   0.00289   0.0014   0.3656   0.7609
   4.750   0.5134   0.00957   0.00315   0.0021   0.3082   0.7690
   5.000   0.5357   0.01009   0.00346   0.0028   0.2535   0.7779
   5.250   0.5583   0.01058   0.00379   0.0035   0.2075   0.7869
   5.750   0.6033   0.01156   0.00449   0.0048   0.1278   0.8072
   6.000   0.6261   0.01199   0.00483   0.0054   0.1009   0.8181
   6.500   0.6731   0.01267   0.00548   0.0066   0.0706   0.8434
   6.750   0.6961   0.01301   0.00583   0.0073   0.0594   0.8578
   7.000   0.7189   0.01335   0.00618   0.0080   0.0500   0.8735
   7.250   0.7415   0.01369   0.00656   0.0088   0.0428   0.8911
   7.500   0.7640   0.01404   0.00694   0.0096   0.0375   0.9101
   7.750   0.7874   0.01444   0.00737   0.0102   0.0332   0.9297
   8.000   0.8141   0.01483   0.00781   0.0101   0.0300   0.9480
   8.250   0.8425   0.01534   0.00832   0.0094   0.0269   0.9638
   8.500   0.8729   0.01580   0.00883   0.0083   0.0248   0.9774
   8.750   0.9025   0.01636   0.00939   0.0073   0.0228   0.9892
   9.000   0.9323   0.01693   0.00999   0.0061   0.0214   0.9993
   9.250   0.9491   0.01738   0.01047   0.0077   0.0205   1.0000
   9.500   0.9650   0.01786   0.01099   0.0094   0.0196   1.0000
   9.750   0.9806   0.01841   0.01155   0.0111   0.0189   1.0000
  10.000   0.9936   0.01904   0.01220   0.0132   0.0183   1.0000
  10.250   1.0069   0.01966   0.01286   0.0151   0.0178   1.0000
  10.500   1.0212   0.02029   0.01355   0.0167   0.0173   1.0000
  10.750   1.0354   0.02099   0.01430   0.0182   0.0169   1.0000
  11.000   1.0492   0.02176   0.01512   0.0196   0.0164   1.0000
  11.250   1.0626   0.02261   0.01603   0.0208   0.0161   1.0000
  11.500   1.0754   0.02354   0.01701   0.0220   0.0158   1.0000
  11.750   1.0875   0.02457   0.01809   0.0231   0.0155   1.0000
  12.000   1.0986   0.02573   0.01930   0.0241   0.0152   1.0000
  12.250   1.1082   0.02704   0.02067   0.0250   0.0150   1.0000
  12.500   1.1159   0.02859   0.02227   0.0259   0.0147   1.0000
  12.750   1.1244   0.03010   0.02386   0.0267   0.0146   1.0000
  13.000   1.1337   0.03160   0.02545   0.0272   0.0144   1.0000
  13.250   1.1420   0.03322   0.02716   0.0278   0.0143   1.0000
  13.500   1.1495   0.03495   0.02897   0.0282   0.0141   1.0000
  13.750   1.1563   0.03679   0.03091   0.0285   0.0140   1.0000
  14.000   1.1620   0.03876   0.03297   0.0288   0.0139   1.0000
  14.250   1.1672   0.04083   0.03513   0.0290   0.0137   1.0000
  14.500   1.1716   0.04302   0.03741   0.0291   0.0136   1.0000
  14.750   1.1753   0.04532   0.03982   0.0290   0.0134   1.0000
  15.000   1.1783   0.04774   0.04233   0.0289   0.0132   1.0000
  15.250   1.1803   0.05033   0.04502   0.0286   0.0131   1.0000
  15.500   1.1813   0.05310   0.04788   0.0281   0.0129   1.0000
  15.750   1.1818   0.05603   0.05091   0.0275   0.0128   1.0000
  16.000   1.1811   0.05920   0.05418   0.0267   0.0127   1.0000
  16.250   1.1794   0.06258   0.05766   0.0258   0.0126   1.0000
  16.500   1.1767   0.06619   0.06137   0.0246   0.0125   1.0000
  16.750   1.1732   0.07002   0.06531   0.0233   0.0124   1.0000
  17.000   1.1685   0.07412   0.06951   0.0218   0.0124   1.0000
  17.250   1.1626   0.07847   0.07397   0.0201   0.0123   1.0000
  17.500   1.1558   0.08309   0.07871   0.0181   0.0122   1.0000
  17.750   1.1479   0.08799   0.08371   0.0160   0.0122   1.0000
  18.000   1.1388   0.09319   0.08903   0.0136   0.0121   1.0000
  18.250   1.1285   0.09868   0.09463   0.0111   0.0120   1.0000
  18.500   1.1175   0.10446   0.10053   0.0083   0.0120   1.0000
  18.750   1.1053   0.11060   0.10678   0.0052   0.0119   1.0000
  19.000   1.0921   0.11699   0.11329   0.0019   0.0119   1.0000
  19.250   1.0778   0.12380   0.12024  -0.0018   0.0119   1.0000
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