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RAF 34 AIRFOIL (raf34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAF 34 AIRFOIL (raf34-il)
Reynolds number: 1,000,000
Max Cl/Cd: 84.75 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-raf34-il-1000000-n5.txt
Download as CSV file: xf-raf34-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAF 34 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.1254   0.08832   0.08581  -0.0272   1.0000   0.0107
 -18.000  -1.2447   0.06286   0.05990  -0.0436   1.0000   0.0101
 -17.750  -1.2811   0.05257   0.04938  -0.0511   1.0000   0.0100
 -17.500  -1.2994   0.04640   0.04304  -0.0552   1.0000   0.0101
 -17.250  -1.3101   0.04196   0.03845  -0.0574   1.0000   0.0103
 -17.000  -1.3168   0.03848   0.03485  -0.0585   1.0000   0.0104
 -16.750  -1.3199   0.03574   0.03199  -0.0588   1.0000   0.0105
 -16.500  -1.3199   0.03353   0.02968  -0.0584   1.0000   0.0108
 -16.250  -1.3186   0.03163   0.02768  -0.0576   1.0000   0.0110
 -16.000  -1.3155   0.03002   0.02596  -0.0564   1.0000   0.0113
 -15.750  -1.3110   0.02862   0.02446  -0.0549   1.0000   0.0116
 -15.500  -1.3045   0.02742   0.02320  -0.0532   1.0000   0.0120
 -15.250  -1.2973   0.02634   0.02204  -0.0514   1.0000   0.0123
 -15.000  -1.2875   0.02546   0.02111  -0.0496   1.0000   0.0126
 -14.750  -1.2752   0.02477   0.02038  -0.0479   1.0000   0.0132
 -14.500  -1.2640   0.02403   0.01958  -0.0459   1.0000   0.0136
 -14.250  -1.2537   0.02328   0.01876  -0.0437   1.0000   0.0138
 -14.000  -1.2415   0.02267   0.01808  -0.0415   1.0000   0.0142
 -13.750  -1.2299   0.02205   0.01739  -0.0392   1.0000   0.0146
 -13.500  -1.2183   0.02147   0.01674  -0.0367   1.0000   0.0149
 -13.250  -1.2044   0.02093   0.01616  -0.0346   1.0000   0.0152
 -13.000  -1.1864   0.02052   0.01573  -0.0331   1.0000   0.0157
 -12.750  -1.1676   0.02015   0.01534  -0.0317   1.0000   0.0161
 -12.500  -1.1492   0.01974   0.01490  -0.0303   1.0000   0.0165
 -12.250  -1.1305   0.01933   0.01444  -0.0289   1.0000   0.0169
 -12.000  -1.1111   0.01895   0.01402  -0.0275   1.0000   0.0174
 -11.750  -1.0915   0.01858   0.01360  -0.0262   1.0000   0.0178
 -11.500  -1.0720   0.01818   0.01315  -0.0248   1.0000   0.0182
 -11.250  -1.0524   0.01779   0.01270  -0.0234   1.0000   0.0184
 -10.750  -0.9733   0.01658   0.01141  -0.0294   0.9477   0.0195
 -10.500  -0.9271   0.01620   0.01087  -0.0337   0.8979   0.0200
 -10.250  -0.9059   0.01601   0.01053  -0.0324   0.8640   0.0204
 -10.000  -0.8846   0.01578   0.01019  -0.0312   0.8426   0.0208
  -9.750  -0.8632   0.01550   0.00981  -0.0300   0.8254   0.0212
  -9.500  -0.8409   0.01526   0.00949  -0.0290   0.8104   0.0216
  -9.250  -0.8186   0.01496   0.00910  -0.0280   0.7970   0.0220
  -9.000  -0.7959   0.01469   0.00873  -0.0271   0.7847   0.0223
  -8.750  -0.7724   0.01445   0.00842  -0.0262   0.7731   0.0226
  -8.500  -0.7489   0.01420   0.00808  -0.0254   0.7617   0.0228
  -8.250  -0.7252   0.01395   0.00776  -0.0246   0.7514   0.0230
  -8.000  -0.7046   0.01337   0.00710  -0.0234   0.7407   0.0237
  -7.750  -0.6817   0.01299   0.00667  -0.0225   0.7308   0.0241
  -7.500  -0.6582   0.01268   0.00630  -0.0216   0.7214   0.0245
  -7.250  -0.6340   0.01241   0.00597  -0.0209   0.7116   0.0248
  -7.000  -0.6097   0.01217   0.00567  -0.0202   0.7026   0.0252
  -6.750  -0.5849   0.01194   0.00539  -0.0196   0.6936   0.0257
  -6.500  -0.5603   0.01169   0.00509  -0.0189   0.6856   0.0260
  -6.250  -0.5355   0.01146   0.00480  -0.0182   0.6770   0.0264
  -6.000  -0.5105   0.01123   0.00453  -0.0176   0.6693   0.0268
  -5.750  -0.4853   0.01102   0.00426  -0.0171   0.6616   0.0271
  -5.500  -0.4599   0.01083   0.00403  -0.0165   0.6544   0.0275
  -5.250  -0.4343   0.01064   0.00380  -0.0160   0.6470   0.0278
  -5.000  -0.4087   0.01047   0.00357  -0.0155   0.6403   0.0281
  -4.750  -0.3827   0.01032   0.00339  -0.0151   0.6335   0.0283
  -4.500  -0.3573   0.01012   0.00314  -0.0145   0.6268   0.0290
  -4.250  -0.3315   0.00992   0.00291  -0.0140   0.6207   0.0299
  -4.000  -0.3056   0.00976   0.00273  -0.0135   0.6139   0.0307
  -3.750  -0.2795   0.00962   0.00257  -0.0131   0.6080   0.0314
  -3.500  -0.2532   0.00949   0.00241  -0.0127   0.6014   0.0323
  -3.250  -0.2269   0.00938   0.00227  -0.0123   0.5950   0.0332
  -3.000  -0.2003   0.00927   0.00215  -0.0120   0.5891   0.0342
  -2.750  -0.1737   0.00917   0.00202  -0.0116   0.5826   0.0360
  -2.500  -0.1475   0.00905   0.00191  -0.0112   0.5762   0.0399
  -2.250  -0.1218   0.00886   0.00178  -0.0107   0.5699   0.0560
  -2.000  -0.0967   0.00865   0.00167  -0.0102   0.5633   0.0873
  -1.750  -0.0706   0.00850   0.00159  -0.0098   0.5574   0.1065
  -1.500  -0.0445   0.00837   0.00152  -0.0094   0.5506   0.1265
  -1.000   0.0074   0.00810   0.00138  -0.0085   0.5375   0.1752
  -0.750   0.0322   0.00791   0.00132  -0.0079   0.5304   0.2237
  -0.500   0.0571   0.00770   0.00127  -0.0073   0.5218   0.2761
  -0.250   0.0823   0.00756   0.00123  -0.0068   0.5126   0.3176
   0.000   0.1066   0.00739   0.00118  -0.0061   0.5004   0.3698
   0.250   0.1295   0.00709   0.00114  -0.0051   0.4909   0.4541
   0.500   0.1505   0.00676   0.00111  -0.0038   0.4805   0.5581
   0.750   0.1692   0.00640   0.00110  -0.0019   0.4703   0.6685
   1.000   0.1890   0.00616   0.00112   0.0000   0.4618   0.7494
   1.250   0.2114   0.00606   0.00116   0.0013   0.4527   0.8005
   1.500   0.2358   0.00599   0.00120   0.0022   0.4431   0.8406
   1.750   0.2627   0.00598   0.00126   0.0026   0.4334   0.8754
   2.000   0.2949   0.00602   0.00135   0.0017   0.4233   0.9044
   2.250   0.3313   0.00611   0.00145  -0.0001   0.4120   0.9217
   2.500   0.3651   0.00623   0.00154  -0.0014   0.4014   0.9320
   2.750   0.4024   0.00638   0.00164  -0.0035   0.3903   0.9388
   3.000   0.4344   0.00651   0.00174  -0.0044   0.3792   0.9470
   3.250   0.4721   0.00667   0.00185  -0.0066   0.3661   0.9510
   3.500   0.5015   0.00683   0.00197  -0.0069   0.3552   0.9575
   3.750   0.5311   0.00700   0.00209  -0.0073   0.3435   0.9616
   4.000   0.5634   0.00716   0.00221  -0.0083   0.3319   0.9636
   4.250   0.5945   0.00732   0.00234  -0.0091   0.3215   0.9661
   4.500   0.6223   0.00753   0.00249  -0.0092   0.3056   0.9699
   4.750   0.6492   0.00778   0.00265  -0.0091   0.2862   0.9735
   5.000   0.6813   0.00806   0.00283  -0.0102   0.2648   0.9750
   5.250   0.7119   0.00840   0.00305  -0.0111   0.2381   0.9769
   5.500   0.7407   0.00876   0.00329  -0.0116   0.2105   0.9793
   5.750   0.7653   0.00921   0.00357  -0.0112   0.1793   0.9828
   6.000   0.7924   0.00971   0.00391  -0.0115   0.1441   0.9848
   6.250   0.8229   0.01006   0.00418  -0.0125   0.1285   0.9860
   6.500   0.8531   0.01036   0.00443  -0.0133   0.1183   0.9873
   6.750   0.8829   0.01063   0.00468  -0.0140   0.1116   0.9889
   7.000   0.9121   0.01088   0.00492  -0.0146   0.1050   0.9906
   7.250   0.9403   0.01116   0.00518  -0.0149   0.0979   0.9923
   7.500   0.9675   0.01145   0.00546  -0.0151   0.0900   0.9939
   7.750   0.9935   0.01229   0.00602  -0.0156   0.0500   0.9954
   8.000   1.0217   0.01274   0.00643  -0.0163   0.0409   0.9968
   8.250   1.0503   0.01311   0.00679  -0.0169   0.0367   0.9981
   8.500   1.0787   0.01350   0.00718  -0.0175   0.0329   0.9992
   8.750   1.1062   0.01385   0.00754  -0.0179   0.0306   1.0000
   9.000   1.1230   0.01423   0.00792  -0.0161   0.0285   1.0000
   9.250   1.1400   0.01458   0.00828  -0.0143   0.0269   1.0000
   9.500   1.1567   0.01492   0.00865  -0.0125   0.0252   1.0000
   9.750   1.1722   0.01532   0.00906  -0.0105   0.0237   1.0000
  10.000   1.1866   0.01574   0.00948  -0.0083   0.0219   1.0000
  10.250   1.2013   0.01612   0.00990  -0.0062   0.0207   1.0000
  10.500   1.2143   0.01657   0.01035  -0.0038   0.0191   1.0000
  10.750   1.2254   0.01706   0.01086  -0.0012   0.0177   1.0000
  11.000   1.2320   0.01749   0.01131   0.0023   0.0168   1.0000
  11.250   1.2372   0.01794   0.01180   0.0060   0.0161   1.0000
  11.500   1.2433   0.01852   0.01240   0.0092   0.0151   1.0000
  11.750   1.2498   0.01922   0.01313   0.0119   0.0141   1.0000
  12.000   1.2582   0.01997   0.01393   0.0141   0.0135   1.0000
  12.250   1.2673   0.02081   0.01481   0.0159   0.0129   1.0000
  12.500   1.2760   0.02177   0.01582   0.0175   0.0123   1.0000
  12.750   1.2846   0.02285   0.01694   0.0189   0.0119   1.0000
  13.000   1.2920   0.02410   0.01823   0.0201   0.0113   1.0000
  13.250   1.3000   0.02538   0.01957   0.0211   0.0110   1.0000
  13.500   1.3078   0.02677   0.02101   0.0220   0.0106   1.0000
  13.750   1.3158   0.02819   0.02249   0.0228   0.0102   1.0000
  14.000   1.3224   0.02978   0.02415   0.0234   0.0100   1.0000
  14.250   1.3289   0.03144   0.02586   0.0239   0.0096   1.0000
  14.500   1.3343   0.03324   0.02772   0.0244   0.0092   1.0000
  14.750   1.3381   0.03524   0.02979   0.0247   0.0090   1.0000
  15.000   1.3415   0.03733   0.03193   0.0250   0.0088   1.0000
  15.250   1.3435   0.03960   0.03427   0.0252   0.0086   1.0000
  15.500   1.3428   0.04220   0.03694   0.0252   0.0082   1.0000
  15.750   1.3441   0.04464   0.03945   0.0252   0.0081   1.0000
  16.000   1.3452   0.04718   0.04207   0.0250   0.0080   1.0000
  16.250   1.3453   0.04991   0.04489   0.0247   0.0079   1.0000
  16.500   1.3448   0.05279   0.04785   0.0243   0.0077   1.0000
  16.750   1.3432   0.05590   0.05104   0.0237   0.0076   1.0000
  17.000   1.3419   0.05903   0.05425   0.0230   0.0074   1.0000
  17.250   1.3379   0.06255   0.05785   0.0222   0.0073   1.0000
  17.500   1.3333   0.06625   0.06164   0.0212   0.0071   1.0000
  17.750   1.3279   0.07014   0.06562   0.0201   0.0072   1.0000
  18.000   1.3227   0.07404   0.06960   0.0189   0.0070   1.0000
  18.250   1.3168   0.07812   0.07376   0.0175   0.0068   1.0000
  18.500   1.3082   0.08267   0.07840   0.0160   0.0067   1.0000
  18.750   1.3002   0.08720   0.08301   0.0143   0.0067   1.0000
  19.000   1.2908   0.09199   0.08789   0.0126   0.0066   1.0000
  19.250   1.2796   0.09714   0.09313   0.0106   0.0065   1.0000
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