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FX 63-158 AIRFOIL (fx63158-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX 63-158 AIRFOIL (fx63158-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx63158-il-1000000.txt
Download as CSV file: xf-fx63158-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 63-158 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.0570   0.08436   0.08153  -0.1060   0.7212   0.0110
 -11.250  -0.0635   0.07711   0.07423  -0.1091   0.7056   0.0115
 -11.000  -0.0696   0.07008   0.06720  -0.1121   0.7014   0.0115
 -10.750  -0.0766   0.06198   0.05908  -0.1158   0.6941   0.0115
 -10.500  -0.0927   0.05345   0.05043  -0.1208   0.6798   0.0115
 -10.250  -0.1158   0.04609   0.04299  -0.1255   0.6786   0.0115
 -10.000  -0.1292   0.04156   0.03839  -0.1279   0.6741   0.0115
  -9.750  -0.1453   0.03759   0.03428  -0.1294   0.6593   0.0115
  -9.500  -0.1669   0.03402   0.03056  -0.1302   0.6528   0.0115
  -9.250  -0.1803   0.03142   0.02785  -0.1298   0.6461   0.0115
  -9.000  -0.2001   0.02943   0.02572  -0.1278   0.6373   0.0115
  -8.750  -0.2131   0.02767   0.02380  -0.1261   0.6274   0.0115
  -8.500  -0.2182   0.02551   0.02142  -0.1247   0.6204   0.0116
  -8.250  -0.2276   0.02087   0.01653  -0.1235   0.6118   0.0118
  -8.000  -0.2163   0.01888   0.01444  -0.1229   0.6021   0.0119
  -7.750  -0.2032   0.01718   0.01264  -0.1225   0.5961   0.0121
  -7.500  -0.1878   0.01569   0.01105  -0.1221   0.5879   0.0123
  -7.250  -0.1714   0.01427   0.00946  -0.1218   0.5783   0.0126
  -7.000  -0.1529   0.01292   0.00794  -0.1215   0.5695   0.0131
  -6.750  -0.1303   0.01264   0.00716  -0.1208   0.5605   0.0146
  -6.500  -0.1119   0.01000   0.00423  -0.1209   0.5537   0.0150
  -6.250  -0.0890   0.00892   0.00311  -0.1209   0.5463   0.0153
  -6.000  -0.0648   0.00809   0.00218  -0.1209   0.5396   0.0156
  -5.750  -0.0404   0.00739   0.00133  -0.1208   0.5295   0.0162
  -5.500  -0.0203   0.01451   0.00784  -0.1221   0.5254   0.0093
  -5.250   0.0047   0.01396   0.00720  -0.1215   0.5083   0.0088
  -5.000   0.0284   0.01303   0.00618  -0.1210   0.4944   0.0085
  -4.750   0.0544   0.01237   0.00540  -0.1211   0.4804   0.0084
  -4.500   0.0828   0.01181   0.00474  -0.1217   0.4698   0.0085
  -4.250   0.1119   0.01142   0.00425  -0.1224   0.4580   0.0088
  -4.000   0.1413   0.01107   0.00373  -0.1232   0.4286   0.0094
  -3.750   0.1692   0.01102   0.00355  -0.1235   0.4042   0.0100
  -3.500   0.1960   0.01110   0.00342  -0.1236   0.3586   0.0106
  -3.250   0.2233   0.01119   0.00332  -0.1238   0.3201   0.0110
  -3.000   0.2494   0.01139   0.00328  -0.1238   0.2700   0.0115
  -2.750   0.2762   0.01156   0.00329  -0.1239   0.2277   0.0129
  -2.500   0.3050   0.01158   0.00324  -0.1243   0.2116   0.0145
  -2.250   0.3333   0.01165   0.00315  -0.1246   0.1802   0.0177
  -2.000   0.3627   0.01163   0.00307  -0.1251   0.1720   0.0218
  -1.750   0.3918   0.01163   0.00308  -0.1255   0.1682   0.0345
  -1.500   0.4204   0.01168   0.00308  -0.1259   0.1581   0.0370
  -1.250   0.4482   0.01181   0.00310  -0.1260   0.1347   0.0397
  -1.000   0.4769   0.01185   0.00310  -0.1264   0.1302   0.0439
  -0.750   0.5061   0.01186   0.00310  -0.1269   0.1267   0.0504
  -0.500   0.5362   0.01181   0.00313  -0.1276   0.1254   0.0911
  -0.250   0.5652   0.01183   0.00315  -0.1281   0.1235   0.1056
   0.000   0.5952   0.01180   0.00319  -0.1288   0.1213   0.1431
   0.250   0.6239   0.01185   0.00324  -0.1291   0.1185   0.1545
   0.500   0.6533   0.01187   0.00331  -0.1298   0.1158   0.1899
   0.750   0.6842   0.01180   0.00336  -0.1307   0.1144   0.2397
   1.000   0.7190   0.01153   0.00338  -0.1329   0.1121   0.3627
   1.250   0.7554   0.01123   0.00343  -0.1356   0.0964   0.5167
   1.500   0.7859   0.01124   0.00360  -0.1365   0.0952   0.5866
   1.750   0.8135   0.01139   0.00378  -0.1366   0.0939   0.6133
   2.000   0.8408   0.01155   0.00393  -0.1366   0.0926   0.6241
   2.250   0.8679   0.01172   0.00408  -0.1366   0.0912   0.6328
   2.500   0.8948   0.01189   0.00425  -0.1365   0.0894   0.6382
   2.750   0.9217   0.01205   0.00443  -0.1365   0.0883   0.6435
   3.000   0.9484   0.01222   0.00460  -0.1364   0.0877   0.6486
   3.250   0.9750   0.01241   0.00478  -0.1363   0.0870   0.6536
   3.500   1.0014   0.01258   0.00499  -0.1362   0.0863   0.6583
   3.750   1.0275   0.01278   0.00519  -0.1360   0.0854   0.6613
   4.000   1.0533   0.01299   0.00541  -0.1357   0.0844   0.6657
   4.250   1.0788   0.01324   0.00564  -0.1354   0.0833   0.6704
   4.500   1.1041   0.01345   0.00587  -0.1352   0.0821   0.6734
   4.750   1.1293   0.01367   0.00611  -0.1348   0.0809   0.6753
   5.000   1.1543   0.01389   0.00634  -0.1345   0.0799   0.6779
   5.250   1.1796   0.01408   0.00656  -0.1342   0.0795   0.6810
   5.500   1.2048   0.01427   0.00677  -0.1339   0.0787   0.6837
   5.750   1.2299   0.01447   0.00698  -0.1336   0.0765   0.6858
   6.000   1.2531   0.01478   0.00725  -0.1330   0.0641   0.6871
   6.250   1.2758   0.01510   0.00753  -0.1323   0.0630   0.6880
   6.500   1.2983   0.01540   0.00782  -0.1316   0.0614   0.6894
   6.750   1.3200   0.01573   0.00816  -0.1307   0.0593   0.6908
   7.000   1.3414   0.01606   0.00852  -0.1298   0.0577   0.6922
   7.250   1.3615   0.01642   0.00894  -0.1286   0.0567   0.6936
   7.500   1.3786   0.01681   0.00939  -0.1269   0.0557   0.6949
   7.750   1.3943   0.01726   0.00989  -0.1250   0.0545   0.6963
   8.000   1.4093   0.01776   0.01043  -0.1230   0.0533   0.6977
   8.250   1.4236   0.01829   0.01101  -0.1209   0.0520   0.6991
   8.500   1.4391   0.01878   0.01154  -0.1191   0.0508   0.7006
   8.750   1.4590   0.01906   0.01186  -0.1180   0.0494   0.7021
   9.000   1.4769   0.01945   0.01229  -0.1167   0.0474   0.7034
   9.250   1.4923   0.01996   0.01282  -0.1150   0.0450   0.7046
   9.500   1.5088   0.02042   0.01332  -0.1136   0.0431   0.7065
   9.750   1.5270   0.02079   0.01374  -0.1125   0.0365   0.7089
  10.000   1.5360   0.02166   0.01454  -0.1101   0.0309   0.7110
  10.250   1.5459   0.02253   0.01545  -0.1080   0.0284   0.7131
  10.500   1.5526   0.02362   0.01657  -0.1056   0.0258   0.7154
  10.750   1.5604   0.02472   0.01772  -0.1035   0.0236   0.7175
  11.000   1.5704   0.02574   0.01880  -0.1019   0.0225   0.7197
  11.250   1.5764   0.02711   0.02020  -0.1000   0.0190   0.7214
  11.500   1.5773   0.02895   0.02205  -0.0979   0.0151   0.7234
  11.750   1.5796   0.03083   0.02396  -0.0963   0.0124   0.7256
  12.000   1.5821   0.03283   0.02601  -0.0949   0.0105   0.7278
  12.250   1.5870   0.03475   0.02799  -0.0939   0.0092   0.7297
  12.500   1.5889   0.03704   0.03035  -0.0929   0.0070   0.7315
  12.750   1.5819   0.04036   0.03371  -0.0918   0.0033   0.7330
  13.000   1.5815   0.04314   0.03657  -0.0911   0.0030   0.7348
  13.250   1.5825   0.04587   0.03939  -0.0907   0.0028   0.7362
  13.500   1.5838   0.04865   0.04225  -0.0903   0.0026   0.7376
  13.750   1.5848   0.05152   0.04520  -0.0901   0.0024   0.7387
  14.000   1.5858   0.05446   0.04824  -0.0900   0.0024   0.7399
  14.250   1.5866   0.05752   0.05141  -0.0901   0.0023   0.7416
  14.500   1.5866   0.06074   0.05473  -0.0902   0.0023   0.7433
  14.750   1.5861   0.06412   0.05821  -0.0905   0.0022   0.7449
  15.000   1.5855   0.06759   0.06179  -0.0909   0.0022   0.7465
  15.250   1.5851   0.07110   0.06539  -0.0913   0.0021   0.7480
  15.500   1.5839   0.07479   0.06919  -0.0919   0.0021   0.7494
  15.750   1.5822   0.07865   0.07315  -0.0927   0.0020   0.7508
  16.000   1.5803   0.08262   0.07722  -0.0935   0.0020   0.7522
  16.250   1.5787   0.08660   0.08130  -0.0944   0.0020   0.7536
  16.500   1.5755   0.09090   0.08570  -0.0955   0.0019   0.7548
  16.750   1.5725   0.09522   0.09012  -0.0967   0.0019   0.7559
  17.000   1.5696   0.09961   0.09461  -0.0980   0.0019   0.7575
  17.250   1.5653   0.10433   0.09945  -0.0996   0.0019   0.7593
  17.500   1.5608   0.10911   0.10435  -0.1013   0.0018   0.7610
  17.750   1.5568   0.11384   0.10919  -0.1030   0.0018   0.7626
  18.000   1.5512   0.11892   0.11438  -0.1051   0.0018   0.7642
  18.250   1.5456   0.12404   0.11961  -0.1072   0.0018   0.7659
  18.500   1.5400   0.12919   0.12488  -0.1095   0.0017   0.7676
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