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RAF 32 AIRFOIL (raf32-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAF 32 AIRFOIL (raf32-il)
Reynolds number: 1,000,000
Max Cl/Cd: 134.8 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-raf32-il-1000000-n5.txt
Download as CSV file: xf-raf32-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7122   0.06428   0.06162  -0.0995   0.9910   0.0080
 -14.500  -0.7959   0.04412   0.04114  -0.1186   0.9847   0.0077
 -14.250  -0.8236   0.03026   0.02693  -0.1374   0.9761   0.0077
 -13.750  -0.7916   0.02371   0.01998  -0.1491   0.9642   0.0080
 -13.500  -0.7720   0.02200   0.01814  -0.1510   0.9584   0.0082
 -13.250  -0.7458   0.02064   0.01666  -0.1532   0.9546   0.0084
 -13.000  -0.7253   0.01963   0.01554  -0.1536   0.9473   0.0087
 -12.750  -0.7005   0.01867   0.01448  -0.1545   0.9412   0.0089
 -12.500  -0.6776   0.01789   0.01359  -0.1548   0.9323   0.0092
 -12.250  -0.6552   0.01718   0.01277  -0.1547   0.9228   0.0095
 -12.000  -0.6320   0.01655   0.01201  -0.1547   0.9142   0.0098
 -11.750  -0.6097   0.01600   0.01136  -0.1543   0.9058   0.0100
 -11.500  -0.5881   0.01533   0.01059  -0.1539   0.8985   0.0105
 -11.250  -0.5659   0.01478   0.00996  -0.1534   0.8907   0.0110
 -11.000  -0.5426   0.01430   0.00940  -0.1530   0.8838   0.0115
 -10.750  -0.5193   0.01386   0.00888  -0.1526   0.8767   0.0120
 -10.500  -0.4952   0.01347   0.00838  -0.1522   0.8702   0.0125
 -10.250  -0.4717   0.01300   0.00785  -0.1518   0.8640   0.0131
 -10.000  -0.4479   0.01259   0.00737  -0.1513   0.8574   0.0139
  -9.750  -0.4233   0.01224   0.00694  -0.1510   0.8516   0.0147
  -9.500  -0.3983   0.01192   0.00656  -0.1506   0.8460   0.0155
  -9.250  -0.3738   0.01154   0.00612  -0.1503   0.8405   0.0168
  -9.000  -0.3487   0.01123   0.00574  -0.1499   0.8356   0.0183
  -8.750  -0.3231   0.01094   0.00541  -0.1497   0.8305   0.0196
  -8.500  -0.2980   0.01062   0.00505  -0.1493   0.8250   0.0219
  -8.250  -0.2723   0.01038   0.00475  -0.1490   0.8199   0.0239
  -8.000  -0.2464   0.01009   0.00446  -0.1488   0.8153   0.0277
  -7.750  -0.2203   0.00986   0.00423  -0.1486   0.8105   0.0317
  -7.500  -0.1940   0.00969   0.00405  -0.1484   0.8059   0.0361
  -7.250  -0.1673   0.00953   0.00385  -0.1482   0.8017   0.0388
  -7.000  -0.1404   0.00938   0.00371  -0.1481   0.7969   0.0422
  -6.750  -0.1136   0.00927   0.00356  -0.1479   0.7917   0.0446
  -6.500  -0.0867   0.00918   0.00342  -0.1477   0.7870   0.0462
  -6.250  -0.0593   0.00909   0.00329  -0.1476   0.7823   0.0471
  -6.000  -0.0326   0.00893   0.00310  -0.1475   0.7774   0.0487
  -5.500   0.0211   0.00866   0.00277  -0.1471   0.7678   0.0528
  -5.250   0.0481   0.00856   0.00265  -0.1469   0.7621   0.0546
  -5.000   0.0747   0.00849   0.00252  -0.1467   0.7565   0.0561
  -4.750   0.1021   0.00839   0.00240  -0.1466   0.7512   0.0571
  -4.500   0.1291   0.00831   0.00227  -0.1464   0.7454   0.0577
  -4.250   0.1558   0.00823   0.00215  -0.1461   0.7397   0.0585
  -4.000   0.1827   0.00811   0.00200  -0.1459   0.7334   0.0606
  -3.750   0.2091   0.00802   0.00188  -0.1456   0.7266   0.0628
  -3.500   0.2361   0.00794   0.00178  -0.1455   0.7205   0.0649
  -3.250   0.2627   0.00788   0.00170  -0.1452   0.7128   0.0672
  -3.000   0.2892   0.00784   0.00162  -0.1449   0.7047   0.0694
  -2.750   0.3150   0.00780   0.00154  -0.1444   0.6949   0.0748
  -2.500   0.3412   0.00774   0.00148  -0.1441   0.6856   0.0819
  -2.250   0.3668   0.00766   0.00142  -0.1436   0.6773   0.0982
  -2.000   0.3931   0.00752   0.00136  -0.1434   0.6703   0.1276
  -1.750   0.4187   0.00742   0.00132  -0.1430   0.6636   0.1590
  -1.500   0.4451   0.00733   0.00130  -0.1427   0.6576   0.1860
  -1.250   0.4715   0.00729   0.00129  -0.1425   0.6514   0.2087
  -1.000   0.4976   0.00728   0.00129  -0.1421   0.6455   0.2260
  -0.750   0.5245   0.00725   0.00130  -0.1419   0.6403   0.2426
  -0.500   0.5511   0.00723   0.00131  -0.1417   0.6349   0.2580
  -0.250   0.5769   0.00722   0.00134  -0.1413   0.6297   0.2803
   0.000   0.6038   0.00719   0.00136  -0.1411   0.6250   0.3016
   0.250   0.6302   0.00718   0.00139  -0.1408   0.6198   0.3202
   0.500   0.6562   0.00719   0.00143  -0.1405   0.6150   0.3368
   0.750   0.6827   0.00716   0.00147  -0.1402   0.6107   0.3636
   1.000   0.7088   0.00710   0.00152  -0.1399   0.6058   0.4055
   1.250   0.7343   0.00708   0.00158  -0.1395   0.6007   0.4425
   1.500   0.7599   0.00708   0.00165  -0.1391   0.5950   0.4739
   1.750   0.7856   0.00708   0.00172  -0.1387   0.5883   0.5035
   2.000   0.8101   0.00712   0.00181  -0.1380   0.5812   0.5355
   2.250   0.8360   0.00714   0.00188  -0.1376   0.5742   0.5615
   2.500   0.8597   0.00721   0.00197  -0.1368   0.5641   0.5837
   2.750   0.8837   0.00727   0.00206  -0.1360   0.5524   0.6087
   3.000   0.9075   0.00734   0.00216  -0.1352   0.5409   0.6313
   3.250   0.9301   0.00743   0.00227  -0.1341   0.5274   0.6562
   3.500   0.9518   0.00751   0.00240  -0.1329   0.5129   0.6910
   3.750   0.9729   0.00758   0.00254  -0.1316   0.4999   0.7354
   4.000   0.9917   0.00764   0.00270  -0.1297   0.4832   0.7934
   4.250   1.0326   0.00766   0.00297  -0.1328   0.4592   1.0000
   4.500   1.0536   0.00787   0.00313  -0.1315   0.4454   1.0000
   4.750   1.0725   0.00811   0.00330  -0.1298   0.4294   1.0000
   5.000   1.0893   0.00842   0.00352  -0.1276   0.4094   1.0000
   5.250   1.1061   0.00874   0.00374  -0.1254   0.3881   1.0000
   5.500   1.1240   0.00903   0.00397  -0.1236   0.3702   1.0000
   5.750   1.1411   0.00937   0.00422  -0.1215   0.3493   1.0000
   6.000   1.1541   0.00986   0.00456  -0.1188   0.3169   1.0000
   6.250   1.1639   0.01051   0.00500  -0.1156   0.2771   1.0000
   6.500   1.1702   0.01131   0.00555  -0.1118   0.2323   1.0000
   6.750   1.1811   0.01195   0.00604  -0.1089   0.2031   1.0000
   7.000   1.1918   0.01261   0.00654  -0.1060   0.1732   1.0000
   7.250   1.2046   0.01320   0.00702  -0.1036   0.1490   1.0000
   7.500   1.2110   0.01410   0.00771  -0.1002   0.1125   1.0000
   7.750   1.2205   0.01489   0.00837  -0.0974   0.0881   1.0000
   8.000   1.2323   0.01559   0.00900  -0.0950   0.0733   1.0000
   8.250   1.2472   0.01616   0.00954  -0.0932   0.0660   1.0000
   8.500   1.2629   0.01670   0.01007  -0.0915   0.0608   1.0000
   8.750   1.2781   0.01727   0.01064  -0.0898   0.0561   1.0000
   9.000   1.2937   0.01785   0.01122  -0.0882   0.0519   1.0000
   9.250   1.3094   0.01842   0.01181  -0.0866   0.0476   1.0000
   9.500   1.3226   0.01916   0.01251  -0.0848   0.0408   1.0000
   9.750   1.3343   0.02000   0.01331  -0.0829   0.0324   1.0000
  10.000   1.3464   0.02085   0.01414  -0.0811   0.0271   1.0000
  10.250   1.3591   0.02168   0.01497  -0.0794   0.0235   1.0000
  10.500   1.3701   0.02263   0.01592  -0.0776   0.0202   1.0000
  10.750   1.3835   0.02346   0.01678  -0.0761   0.0186   1.0000
  11.000   1.3950   0.02443   0.01777  -0.0744   0.0170   1.0000
  11.250   1.4070   0.02540   0.01876  -0.0729   0.0158   1.0000
  11.500   1.4186   0.02641   0.01980  -0.0714   0.0145   1.0000
  11.750   1.4289   0.02753   0.02095  -0.0699   0.0133   1.0000
  12.000   1.4404   0.02859   0.02205  -0.0685   0.0126   1.0000
  12.250   1.4512   0.02973   0.02323  -0.0671   0.0120   1.0000
  12.500   1.4613   0.03094   0.02447  -0.0657   0.0113   1.0000
  12.750   1.4704   0.03227   0.02584  -0.0643   0.0106   1.0000
  13.000   1.4797   0.03361   0.02723  -0.0630   0.0103   1.0000
  13.250   1.4893   0.03495   0.02862  -0.0618   0.0099   1.0000
  13.500   1.4981   0.03638   0.03010  -0.0606   0.0095   1.0000
  13.750   1.5059   0.03793   0.03171  -0.0595   0.0091   1.0000
  14.000   1.5131   0.03958   0.03339  -0.0583   0.0086   1.0000
  14.250   1.5191   0.04137   0.03524  -0.0572   0.0083   1.0000
  14.500   1.5268   0.04303   0.03696  -0.0562   0.0080   1.0000
  14.750   1.5335   0.04482   0.03881  -0.0553   0.0077   1.0000
  15.000   1.5395   0.04673   0.04079  -0.0545   0.0075   1.0000
  15.250   1.5448   0.04874   0.04287  -0.0536   0.0072   1.0000
  15.500   1.5500   0.05081   0.04499  -0.0529   0.0071   1.0000
  15.750   1.5535   0.05307   0.04731  -0.0522   0.0068   1.0000
  16.000   1.5558   0.05551   0.04981  -0.0515   0.0066   1.0000
  16.250   1.5580   0.05801   0.05239  -0.0510   0.0065   1.0000
  16.500   1.5614   0.06044   0.05489  -0.0505   0.0063   1.0000
  16.750   1.5639   0.06300   0.05753  -0.0502   0.0062   1.0000
  17.000   1.5659   0.06565   0.06026  -0.0499   0.0061   1.0000
  17.250   1.5672   0.06842   0.06311  -0.0497   0.0060   1.0000
  17.500   1.5671   0.07145   0.06622  -0.0496   0.0058   1.0000
  17.750   1.5675   0.07446   0.06931  -0.0497   0.0056   1.0000
  18.000   1.5671   0.07762   0.07255  -0.0498   0.0055   1.0000
  18.250   1.5658   0.08096   0.07598  -0.0501   0.0054   1.0000
  18.500   1.5632   0.08451   0.07961  -0.0505   0.0053   1.0000
  18.750   1.5598   0.08829   0.08348  -0.0511   0.0052   1.0000
  19.000   1.5552   0.09231   0.08759  -0.0519   0.0051   1.0000
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