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RAF 32 AIRFOIL (raf32-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: RAF 32 AIRFOIL (raf32-il)
Reynolds number: 500,000
Max Cl/Cd: 123.68 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-raf32-il-500000.txt
Download as CSV file: xf-raf32-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAF 32 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.2063   0.13069   0.12842  -0.0615   0.9907   0.0306
 -13.250  -0.1988   0.12729   0.12500  -0.0639   0.9893   0.0324
 -12.750  -0.7529   0.04104   0.03780  -0.1083   0.9881   0.0212
 -12.500  -0.7381   0.03527   0.03183  -0.1209   0.9833   0.0217
 -12.250  -0.7240   0.03265   0.02904  -0.1247   0.9757   0.0222
 -12.000  -0.6998   0.02990   0.02604  -0.1294   0.9725   0.0229
 -11.750  -0.6806   0.02777   0.02366  -0.1315   0.9672   0.0236
 -11.500  -0.6566   0.02599   0.02160  -0.1335   0.9626   0.0241
 -11.250  -0.6305   0.02375   0.01922  -0.1361   0.9601   0.0252
 -11.000  -0.5971   0.02283   0.01824  -0.1386   0.9588   0.0261
 -10.750  -0.5631   0.02185   0.01714  -0.1411   0.9578   0.0272
 -10.500  -0.5432   0.02104   0.01616  -0.1404   0.9514   0.0283
 -10.250  -0.5155   0.01978   0.01477  -0.1417   0.9482   0.0295
 -10.000  -0.4830   0.01919   0.01416  -0.1433   0.9461   0.0308
  -9.750  -0.4494   0.01860   0.01348  -0.1451   0.9442   0.0323
  -9.500  -0.4227   0.01802   0.01274  -0.1453   0.9401   0.0337
  -9.250  -0.3998   0.01716   0.01182  -0.1450   0.9345   0.0353
  -9.000  -0.3681   0.01691   0.01157  -0.1461   0.9314   0.0370
  -8.750  -0.3359   0.01652   0.01107  -0.1473   0.9286   0.0391
  -8.500  -0.3133   0.01598   0.01040  -0.1465   0.9225   0.0408
  -8.250  -0.2868   0.01545   0.00987  -0.1466   0.9177   0.0427
  -8.000  -0.2563   0.01521   0.00958  -0.1474   0.9142   0.0450
  -7.750  -0.2294   0.01503   0.00929  -0.1472   0.9092   0.0471
  -7.500  -0.2060   0.01426   0.00845  -0.1467   0.9033   0.0494
  -7.250  -0.1772   0.01393   0.00811  -0.1471   0.8990   0.0516
  -7.000  -0.1504   0.01372   0.00783  -0.1470   0.8940   0.0542
  -6.750  -0.1242   0.01356   0.00758  -0.1466   0.8884   0.0560
  -6.500  -0.0985   0.01275   0.00672  -0.1465   0.8837   0.0588
  -6.250  -0.0721   0.01247   0.00641  -0.1464   0.8786   0.0613
  -6.000  -0.0464   0.01222   0.00612  -0.1460   0.8726   0.0637
  -5.750  -0.0180   0.01200   0.00581  -0.1461   0.8679   0.0658
  -5.500   0.0072   0.01157   0.00532  -0.1456   0.8625   0.0681
  -5.250   0.0320   0.01116   0.00491  -0.1451   0.8567   0.0710
  -5.000   0.0600   0.01092   0.00462  -0.1452   0.8519   0.0737
  -4.750   0.0860   0.01073   0.00437  -0.1448   0.8463   0.0763
  -4.500   0.1124   0.01057   0.00415  -0.1445   0.8403   0.0782
  -4.250   0.1398   0.01019   0.00373  -0.1444   0.8353   0.0823
  -4.000   0.1650   0.00998   0.00352  -0.1439   0.8294   0.0864
  -3.750   0.1917   0.00983   0.00332  -0.1436   0.8235   0.0906
  -3.500   0.2198   0.00958   0.00307  -0.1436   0.8184   0.0991
  -3.250   0.2443   0.00934   0.00289  -0.1430   0.8118   0.1154
  -3.000   0.2698   0.00893   0.00272  -0.1427   0.8060   0.1820
  -2.750   0.2964   0.00873   0.00266  -0.1425   0.8002   0.2340
  -2.500   0.3223   0.00863   0.00261  -0.1420   0.7935   0.2623
  -2.250   0.3503   0.00856   0.00254  -0.1420   0.7877   0.2849
  -2.000   0.3757   0.00849   0.00251  -0.1415   0.7803   0.3040
  -1.750   0.4027   0.00842   0.00244  -0.1412   0.7735   0.3231
  -1.500   0.4290   0.00837   0.00241  -0.1408   0.7667   0.3434
  -1.250   0.4551   0.00828   0.00238  -0.1405   0.7598   0.3658
  -1.000   0.4823   0.00823   0.00235  -0.1403   0.7540   0.3922
  -0.750   0.5075   0.00813   0.00236  -0.1397   0.7469   0.4275
  -0.500   0.5340   0.00804   0.00237  -0.1394   0.7409   0.4737
  -0.250   0.5591   0.00795   0.00243  -0.1388   0.7343   0.5230
   0.000   0.5847   0.00789   0.00247  -0.1383   0.7279   0.5700
   0.250   0.6109   0.00786   0.00251  -0.1379   0.7221   0.6112
   0.750   0.6618   0.00778   0.00259  -0.1367   0.7095   0.6806
   1.000   0.6863   0.00773   0.00267  -0.1359   0.7033   0.7191
   1.250   0.7104   0.00767   0.00272  -0.1350   0.6971   0.7654
   1.500   0.7341   0.00754   0.00277  -0.1340   0.6916   0.8335
   1.750   0.7942   0.00740   0.00286  -0.1409   0.6853   1.0000
   2.000   0.8201   0.00751   0.00290  -0.1405   0.6794   1.0000
   2.250   0.8451   0.00761   0.00297  -0.1399   0.6725   1.0000
   2.500   0.8697   0.00771   0.00303  -0.1392   0.6648   1.0000
   2.750   0.8947   0.00782   0.00310  -0.1386   0.6575   1.0000
   3.000   0.9192   0.00792   0.00318  -0.1378   0.6500   1.0000
   3.250   0.9439   0.00805   0.00328  -0.1372   0.6423   1.0000
   3.500   0.9676   0.00816   0.00336  -0.1362   0.6332   1.0000
   3.750   0.9904   0.00827   0.00346  -0.1351   0.6227   1.0000
   4.000   1.0139   0.00843   0.00355  -0.1342   0.6132   1.0000
   4.250   1.0369   0.00853   0.00368  -0.1332   0.6039   1.0000
   4.500   1.0603   0.00868   0.00381  -0.1323   0.5953   1.0000
   4.750   1.0830   0.00881   0.00394  -0.1312   0.5856   1.0000
   5.000   1.1054   0.00895   0.00409  -0.1301   0.5755   1.0000
   5.250   1.1267   0.00911   0.00423  -0.1287   0.5641   1.0000
   5.500   1.1469   0.00928   0.00437  -0.1271   0.5511   1.0000
   5.750   1.1665   0.00945   0.00455  -0.1255   0.5368   1.0000
   6.000   1.1834   0.00968   0.00472  -0.1232   0.5177   1.0000
   6.250   1.1970   0.00995   0.00492  -0.1203   0.4935   1.0000
   6.500   1.2077   0.01030   0.00517  -0.1169   0.4692   1.0000
   6.750   1.2176   0.01073   0.00549  -0.1134   0.4432   1.0000
   7.000   1.2287   0.01120   0.00585  -0.1103   0.4168   1.0000
   7.250   1.2386   0.01174   0.00627  -0.1070   0.3886   1.0000
   7.500   1.2461   0.01240   0.00678  -0.1034   0.3531   1.0000
   7.750   1.2508   0.01323   0.00739  -0.0995   0.3103   1.0000
   8.000   1.2516   0.01431   0.00820  -0.0952   0.2618   1.0000
   8.250   1.2549   0.01537   0.00904  -0.0914   0.2249   1.0000
   8.500   1.2602   0.01638   0.00988  -0.0881   0.1925   1.0000
   8.750   1.2630   0.01759   0.01086  -0.0845   0.1525   1.0000
   9.000   1.2625   0.01903   0.01203  -0.0808   0.1083   1.0000
   9.250   1.2659   0.02033   0.01318  -0.0777   0.0848   1.0000
   9.500   1.2732   0.02146   0.01425  -0.0752   0.0737   1.0000
   9.750   1.2838   0.02241   0.01522  -0.0732   0.0673   1.0000
  10.000   1.2927   0.02351   0.01632  -0.0710   0.0613   1.0000
  10.250   1.3029   0.02455   0.01737  -0.0691   0.0563   1.0000
  10.500   1.3105   0.02581   0.01865  -0.0671   0.0516   1.0000
  10.750   1.3217   0.02684   0.01973  -0.0654   0.0478   1.0000
  11.000   1.3262   0.02838   0.02126  -0.0633   0.0439   1.0000
  11.250   1.3390   0.02936   0.02230  -0.0619   0.0410   1.0000
  11.500   1.3474   0.03068   0.02363  -0.0603   0.0382   1.0000
  11.750   1.3526   0.03229   0.02528  -0.0585   0.0359   1.0000
  12.000   1.3624   0.03359   0.02664  -0.0572   0.0339   1.0000
  12.250   1.3701   0.03509   0.02818  -0.0558   0.0323   1.0000
  12.500   1.3720   0.03712   0.03024  -0.0541   0.0307   1.0000
  12.750   1.3794   0.03873   0.03193  -0.0528   0.0294   1.0000
  13.000   1.3868   0.04038   0.03365  -0.0517   0.0281   1.0000
  13.250   1.3926   0.04222   0.03555  -0.0505   0.0271   1.0000
  13.500   1.3966   0.04428   0.03765  -0.0494   0.0262   1.0000
  13.750   1.3922   0.04720   0.04062  -0.0480   0.0251   1.0000
  14.000   1.3989   0.04912   0.04264  -0.0472   0.0246   1.0000
  14.250   1.4041   0.05123   0.04484  -0.0464   0.0239   1.0000
  14.500   1.4086   0.05344   0.04713  -0.0457   0.0231   1.0000
  14.750   1.4126   0.05575   0.04950  -0.0451   0.0225   1.0000
  15.000   1.4157   0.05819   0.05200  -0.0446   0.0219   1.0000
  15.250   1.4153   0.06106   0.05492  -0.0440   0.0212   1.0000
  15.500   1.4122   0.06424   0.05816  -0.0434   0.0206   1.0000
  15.750   1.4172   0.06663   0.06066  -0.0432   0.0202   1.0000
  16.000   1.4205   0.06926   0.06340  -0.0430   0.0197   1.0000
  16.250   1.4232   0.07200   0.06624  -0.0429   0.0193   1.0000
  16.500   1.4257   0.07480   0.06913  -0.0429   0.0188   1.0000
  16.750   1.4275   0.07775   0.07215  -0.0430   0.0184   1.0000
  17.000   1.4287   0.08076   0.07524  -0.0432   0.0181   1.0000
  17.250   1.4295   0.08388   0.07842  -0.0435   0.0177   1.0000
  17.500   1.4295   0.08710   0.08170  -0.0438   0.0174   1.0000
  17.750   1.4286   0.09023   0.08489  -0.0436   0.0169   1.0000
  18.000   1.4283   0.09375   0.08855  -0.0443   0.0167   1.0000
  18.250   1.4276   0.09735   0.09228  -0.0452   0.0164   1.0000
  18.500   1.4266   0.10103   0.09610  -0.0462   0.0162   1.0000
  18.750   1.4252   0.10482   0.10001  -0.0472   0.0159   1.0000
  19.000   1.4231   0.10878   0.10409  -0.0486   0.0156   1.0000
  19.250   1.4207   0.11284   0.10826  -0.0501   0.0153   1.0000
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