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RAF 32 AIRFOIL (raf32-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RAF 32 AIRFOIL (raf32-il)
Reynolds number: 500,000
Max Cl/Cd: 116.56 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-raf32-il-500000-n5.txt
Download as CSV file: xf-raf32-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.3973   0.14415   0.14168  -0.0470   0.9998   0.0101
 -14.750  -0.3882   0.14020   0.13774  -0.0500   0.9990   0.0103
 -14.500  -0.5188   0.10459   0.10195  -0.0654   0.9982   0.0119
 -14.250  -0.5539   0.09216   0.08940  -0.0736   0.9966   0.0119
 -14.000  -0.5858   0.08082   0.07793  -0.0819   0.9944   0.0118
 -13.750  -0.6225   0.06934   0.06632  -0.0908   0.9909   0.0117
 -13.500  -0.6596   0.05723   0.05405  -0.1021   0.9865   0.0115
 -13.250  -0.6909   0.04604   0.04267  -0.1135   0.9790   0.0113
 -13.000  -0.7083   0.03525   0.03161  -0.1275   0.9701   0.0112
 -12.750  -0.7022   0.02878   0.02482  -0.1389   0.9613   0.0114
 -12.500  -0.6809   0.02650   0.02234  -0.1426   0.9570   0.0119
 -12.250  -0.6598   0.02465   0.02029  -0.1449   0.9523   0.0122
 -12.000  -0.6390   0.02323   0.01871  -0.1461   0.9465   0.0126
 -11.750  -0.6144   0.02168   0.01702  -0.1481   0.9418   0.0131
 -11.500  -0.5935   0.02058   0.01579  -0.1484   0.9340   0.0135
 -11.250  -0.5675   0.01958   0.01467  -0.1494   0.9283   0.0141
 -11.000  -0.5452   0.01875   0.01371  -0.1494   0.9211   0.0147
 -10.750  -0.5185   0.01796   0.01277  -0.1502   0.9164   0.0153
 -10.500  -0.4976   0.01718   0.01188  -0.1497   0.9093   0.0161
 -10.250  -0.4726   0.01648   0.01108  -0.1499   0.9037   0.0171
 -10.000  -0.4482   0.01589   0.01039  -0.1499   0.8980   0.0182
  -9.750  -0.4239   0.01536   0.00974  -0.1497   0.8916   0.0192
  -9.500  -0.3983   0.01475   0.00904  -0.1498   0.8863   0.0206
  -9.250  -0.3745   0.01426   0.00848  -0.1494   0.8804   0.0223
  -9.000  -0.3493   0.01383   0.00796  -0.1492   0.8746   0.0242
  -8.500  -0.2982   0.01306   0.00708  -0.1489   0.8636   0.0298
  -8.250  -0.2721   0.01278   0.00678  -0.1487   0.8581   0.0335
  -7.750  -0.2190   0.01235   0.00625  -0.1485   0.8483   0.0402
  -7.500  -0.1923   0.01219   0.00603  -0.1484   0.8428   0.0433
  -7.250  -0.1648   0.01205   0.00580  -0.1483   0.8379   0.0460
  -7.000  -0.1382   0.01192   0.00559  -0.1481   0.8328   0.0475
  -6.750  -0.1126   0.01162   0.00527  -0.1479   0.8274   0.0503
  -6.500  -0.0857   0.01144   0.00504  -0.1478   0.8227   0.0526
  -6.250  -0.0588   0.01129   0.00482  -0.1476   0.8181   0.0548
  -6.000  -0.0324   0.01115   0.00462  -0.1474   0.8129   0.0567
  -5.750  -0.0053   0.01104   0.00443  -0.1473   0.8076   0.0580
  -5.500   0.0207   0.01074   0.00409  -0.1470   0.8027   0.0606
  -5.250   0.0468   0.01053   0.00386  -0.1467   0.7974   0.0627
  -5.000   0.0734   0.01036   0.00364  -0.1465   0.7923   0.0645
  -4.750   0.1004   0.01022   0.00344  -0.1464   0.7877   0.0663
  -4.500   0.1268   0.01008   0.00325  -0.1461   0.7822   0.0679
  -4.250   0.1535   0.00995   0.00307  -0.1459   0.7765   0.0692
  -4.000   0.1803   0.00981   0.00287  -0.1457   0.7713   0.0713
  -3.750   0.2066   0.00965   0.00271  -0.1454   0.7657   0.0748
  -3.500   0.2333   0.00953   0.00256  -0.1451   0.7599   0.0784
  -3.250   0.2601   0.00944   0.00243  -0.1449   0.7545   0.0827
  -3.000   0.2864   0.00929   0.00231  -0.1446   0.7481   0.0935
  -2.750   0.3126   0.00915   0.00219  -0.1444   0.7421   0.1125
  -2.500   0.3386   0.00895   0.00210  -0.1441   0.7359   0.1461
  -2.250   0.3644   0.00880   0.00204  -0.1437   0.7289   0.1800
  -2.000   0.3905   0.00871   0.00199  -0.1434   0.7218   0.2085
  -1.750   0.4164   0.00864   0.00195  -0.1430   0.7133   0.2296
  -1.500   0.4425   0.00860   0.00192  -0.1426   0.7058   0.2486
  -1.250   0.4686   0.00857   0.00190  -0.1423   0.6984   0.2658
  -1.000   0.4949   0.00856   0.00189  -0.1420   0.6920   0.2812
  -0.750   0.5211   0.00852   0.00190  -0.1416   0.6852   0.3018
  -0.250   0.5731   0.00845   0.00193  -0.1409   0.6729   0.3534
   0.000   0.5988   0.00842   0.00196  -0.1405   0.6665   0.3822
   0.250   0.6244   0.00838   0.00200  -0.1401   0.6609   0.4193
   0.500   0.6502   0.00832   0.00206  -0.1397   0.6552   0.4608
   0.750   0.6757   0.00831   0.00213  -0.1393   0.6496   0.4987
   1.000   0.7013   0.00832   0.00220  -0.1388   0.6442   0.5306
   1.250   0.7270   0.00832   0.00228  -0.1384   0.6384   0.5616
   1.500   0.7524   0.00834   0.00236  -0.1379   0.6333   0.5899
   1.750   0.7779   0.00837   0.00244  -0.1374   0.6284   0.6166
   2.250   0.8276   0.00839   0.00263  -0.1362   0.6169   0.6779
   2.500   0.8514   0.00839   0.00274  -0.1353   0.6107   0.7173
   2.750   0.8741   0.00836   0.00285  -0.1342   0.6031   0.7658
   3.000   0.8958   0.00818   0.00297  -0.1327   0.5961   0.8765
   3.250   0.9436   0.00827   0.00310  -0.1373   0.5850   1.0000
   3.500   0.9669   0.00840   0.00321  -0.1364   0.5751   1.0000
   3.750   0.9892   0.00857   0.00333  -0.1352   0.5641   1.0000
   4.000   1.0113   0.00872   0.00345  -0.1341   0.5518   1.0000
   4.250   1.0336   0.00887   0.00358  -0.1330   0.5399   1.0000
   4.500   1.0549   0.00905   0.00373  -0.1317   0.5271   1.0000
   4.750   1.0755   0.00925   0.00389  -0.1303   0.5141   1.0000
   5.000   1.0953   0.00946   0.00407  -0.1287   0.5001   1.0000
   5.250   1.1129   0.00969   0.00425  -0.1267   0.4847   1.0000
   5.500   1.1287   0.00998   0.00447  -0.1243   0.4664   1.0000
   5.750   1.1442   0.01030   0.00473  -0.1219   0.4481   1.0000
   6.000   1.1586   0.01067   0.00502  -0.1194   0.4279   1.0000
   6.250   1.1720   0.01110   0.00536  -0.1167   0.4069   1.0000
   6.500   1.1870   0.01151   0.00571  -0.1144   0.3864   1.0000
   6.750   1.2009   0.01198   0.00609  -0.1120   0.3638   1.0000
   7.000   1.2085   0.01270   0.00662  -0.1085   0.3261   1.0000
   7.250   1.2105   0.01371   0.00735  -0.1042   0.2746   1.0000
   7.500   1.2145   0.01472   0.00812  -0.1005   0.2348   1.0000
   7.750   1.2222   0.01560   0.00886  -0.0975   0.2062   1.0000
   8.000   1.2321   0.01640   0.00955  -0.0948   0.1807   1.0000
   8.250   1.2406   0.01732   0.01033  -0.0921   0.1532   1.0000
   8.500   1.2462   0.01842   0.01125  -0.0891   0.1203   1.0000
   8.750   1.2521   0.01955   0.01224  -0.0863   0.0945   1.0000
   9.000   1.2615   0.02053   0.01316  -0.0840   0.0802   1.0000
   9.250   1.2721   0.02146   0.01406  -0.0819   0.0706   1.0000
   9.500   1.2835   0.02237   0.01496  -0.0800   0.0643   1.0000
   9.750   1.2962   0.02321   0.01583  -0.0784   0.0589   1.0000
  10.000   1.3070   0.02422   0.01682  -0.0765   0.0534   1.0000
  10.250   1.3200   0.02509   0.01774  -0.0750   0.0483   1.0000
  10.500   1.3302   0.02617   0.01881  -0.0733   0.0416   1.0000
  10.750   1.3400   0.02731   0.01994  -0.0716   0.0347   1.0000
  11.000   1.3491   0.02853   0.02116  -0.0699   0.0294   1.0000
  11.250   1.3574   0.02984   0.02247  -0.0682   0.0257   1.0000
  11.500   1.3669   0.03109   0.02376  -0.0667   0.0233   1.0000
  11.750   1.3749   0.03250   0.02521  -0.0652   0.0212   1.0000
  12.000   1.3832   0.03391   0.02666  -0.0637   0.0195   1.0000
  12.250   1.3916   0.03535   0.02816  -0.0624   0.0182   1.0000
  12.500   1.3989   0.03692   0.02978  -0.0610   0.0170   1.0000
  12.750   1.4055   0.03860   0.03151  -0.0597   0.0161   1.0000
  13.000   1.4133   0.04021   0.03319  -0.0586   0.0153   1.0000
  13.250   1.4201   0.04195   0.03500  -0.0575   0.0146   1.0000
  13.500   1.4266   0.04375   0.03687  -0.0565   0.0139   1.0000
  13.750   1.4306   0.04585   0.03902  -0.0554   0.0132   1.0000
  14.000   1.4364   0.04782   0.04106  -0.0545   0.0127   1.0000
  14.250   1.4418   0.04987   0.04320  -0.0537   0.0122   1.0000
  14.500   1.4464   0.05204   0.04546  -0.0530   0.0118   1.0000
  14.750   1.4500   0.05438   0.04787  -0.0523   0.0113   1.0000
  15.000   1.4529   0.05683   0.05039  -0.0517   0.0110   1.0000
  15.250   1.4539   0.05957   0.05320  -0.0512   0.0106   1.0000
  15.500   1.4553   0.06233   0.05605  -0.0508   0.0104   1.0000
  15.750   1.4579   0.06498   0.05880  -0.0506   0.0101   1.0000
  16.000   1.4592   0.06783   0.06176  -0.0504   0.0098   1.0000
  16.250   1.4601   0.07080   0.06483  -0.0503   0.0095   1.0000
  16.500   1.4608   0.07386   0.06798  -0.0504   0.0092   1.0000
  16.750   1.4603   0.07714   0.07135  -0.0505   0.0090   1.0000
  17.000   1.4597   0.08048   0.07479  -0.0508   0.0088   1.0000
  17.250   1.4577   0.08407   0.07846  -0.0513   0.0086   1.0000
  17.500   1.4529   0.08817   0.08265  -0.0520   0.0084   1.0000
  17.750   1.4498   0.09209   0.08668  -0.0528   0.0082   1.0000
  18.000   1.4473   0.09600   0.09070  -0.0536   0.0081   1.0000
  18.250   1.4438   0.10009   0.09491  -0.0547   0.0080   1.0000
  18.500   1.4396   0.10437   0.09930  -0.0559   0.0078   1.0000
  18.750   1.4357   0.10867   0.10371  -0.0572   0.0077   1.0000
  19.000   1.4313   0.11310   0.10826  -0.0588   0.0075   1.0000
  19.250   1.4267   0.11762   0.11288  -0.0605   0.0074   1.0000
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