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RG 15A 2.5/13.0 AIRFOIL (rg15a213-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: RG 15A 2.5/13.0 AIRFOIL (rg15a213-il)
Reynolds number: 100,000
Max Cl/Cd: 51.25 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rg15a213-il-100000-n5.txt
Download as CSV file: xf-rg15a213-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RG 15A 2.5/13.0 AIRFOIL                         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.4940   0.09120   0.08588  -0.0489   1.0000   0.0311
 -11.250  -0.5323   0.07831   0.07302  -0.0559   1.0000   0.0305
 -11.000  -0.5852   0.06500   0.05962  -0.0654   1.0000   0.0292
 -10.750  -0.6274   0.05775   0.05220  -0.0689   1.0000   0.0287
 -10.500  -0.6629   0.05345   0.04774  -0.0681   1.0000   0.0283
 -10.250  -0.6906   0.05092   0.04509  -0.0645   1.0000   0.0283
 -10.000  -0.7076   0.04829   0.04229  -0.0615   1.0000   0.0285
  -9.750  -0.7193   0.04577   0.03956  -0.0585   1.0000   0.0289
  -9.500  -0.7268   0.04322   0.03675  -0.0555   1.0000   0.0294
  -9.250  -0.7301   0.04069   0.03393  -0.0528   1.0000   0.0298
  -9.000  -0.7292   0.03824   0.03115  -0.0503   1.0000   0.0304
  -8.750  -0.7242   0.03599   0.02856  -0.0479   1.0000   0.0309
  -8.500  -0.7160   0.03394   0.02613  -0.0458   1.0000   0.0317
  -8.250  -0.7049   0.03247   0.02457  -0.0440   1.0000   0.0327
  -8.000  -0.6920   0.03147   0.02352  -0.0424   1.0000   0.0340
  -7.750  -0.6675   0.03014   0.02200  -0.0429   0.9973   0.0360
  -7.500  -0.6363   0.02855   0.02011  -0.0443   0.9931   0.0379
  -7.250  -0.6065   0.02710   0.01851  -0.0455   0.9883   0.0397
  -7.000  -0.5742   0.02608   0.01744  -0.0473   0.9838   0.0425
  -6.750  -0.5441   0.02509   0.01626  -0.0482   0.9783   0.0465
  -6.500  -0.5127   0.02406   0.01523  -0.0497   0.9731   0.0507
  -6.250  -0.4821   0.02311   0.01415  -0.0507   0.9676   0.0568
  -6.000  -0.4516   0.02227   0.01331  -0.0518   0.9615   0.0664
  -5.750  -0.4180   0.02152   0.01255  -0.0534   0.9567   0.0807
  -5.500  -0.3896   0.02086   0.01187  -0.0540   0.9492   0.0948
  -5.250  -0.3546   0.02025   0.01131  -0.0559   0.9445   0.1128
  -5.000  -0.3266   0.01980   0.01090  -0.0563   0.9367   0.1366
  -4.750  -0.2925   0.01924   0.01043  -0.0579   0.9312   0.1622
  -4.500  -0.2626   0.01873   0.00998  -0.0586   0.9242   0.1868
  -4.250  -0.2303   0.01821   0.00954  -0.0597   0.9177   0.2168
  -4.000  -0.1942   0.01765   0.00910  -0.0615   0.9133   0.2570
  -3.750  -0.1679   0.01719   0.00879  -0.0614   0.9042   0.3004
  -3.500  -0.1319   0.01660   0.00842  -0.0631   0.8995   0.3604
  -3.250  -0.1056   0.01614   0.00820  -0.0629   0.8905   0.4224
  -3.000  -0.0718   0.01568   0.00804  -0.0638   0.8849   0.4977
  -2.750  -0.0453   0.01548   0.00808  -0.0631   0.8760   0.5663
  -2.500  -0.0124   0.01536   0.00803  -0.0634   0.8694   0.6268
  -2.250   0.0147   0.01534   0.00803  -0.0626   0.8599   0.6668
  -2.000   0.0481   0.01527   0.00792  -0.0630   0.8530   0.6985
  -1.750   0.0750   0.01525   0.00784  -0.0624   0.8425   0.7210
  -1.500   0.1088   0.01516   0.00769  -0.0628   0.8353   0.7408
  -1.250   0.1348   0.01514   0.00764  -0.0619   0.8242   0.7584
  -1.000   0.1627   0.01510   0.00755  -0.0613   0.8139   0.7753
  -0.750   0.1945   0.01501   0.00740  -0.0614   0.8050   0.7913
  -0.500   0.2197   0.01499   0.00734  -0.0604   0.7928   0.8063
  -0.250   0.2466   0.01495   0.00726  -0.0597   0.7813   0.8207
   0.000   0.2753   0.01489   0.00714  -0.0593   0.7704   0.8348
   0.250   0.3029   0.01483   0.00703  -0.0586   0.7587   0.8479
   0.500   0.3283   0.01480   0.00698  -0.0576   0.7457   0.8604
   0.750   0.3548   0.01477   0.00691  -0.0569   0.7328   0.8727
   1.000   0.3822   0.01474   0.00683  -0.0565   0.7199   0.8847
   1.250   0.4101   0.01471   0.00675  -0.0561   0.7068   0.8968
   1.500   0.4401   0.01469   0.00668  -0.0562   0.6935   0.9073
   1.750   0.4702   0.01469   0.00664  -0.0564   0.6794   0.9180
   2.000   0.5005   0.01472   0.00662  -0.0568   0.6644   0.9290
   2.250   0.5330   0.01476   0.00663  -0.0577   0.6493   0.9392
   2.500   0.5675   0.01482   0.00665  -0.0590   0.6336   0.9490
   2.750   0.6023   0.01490   0.00668  -0.0604   0.6175   0.9596
   3.000   0.6377   0.01500   0.00674  -0.0621   0.6010   0.9708
   3.250   0.6740   0.01513   0.00681  -0.0640   0.5840   0.9832
   3.500   0.7090   0.01527   0.00693  -0.0657   0.5662   1.0000
   3.750   0.7255   0.01543   0.00703  -0.0638   0.5510   1.0000
   4.000   0.7455   0.01563   0.00716  -0.0626   0.5352   1.0000
   4.250   0.7672   0.01586   0.00733  -0.0616   0.5191   1.0000
   4.500   0.7897   0.01611   0.00754  -0.0608   0.5028   1.0000
   4.750   0.8124   0.01638   0.00776  -0.0599   0.4862   1.0000
   5.000   0.8351   0.01667   0.00801  -0.0591   0.4697   1.0000
   5.250   0.8576   0.01699   0.00830  -0.0583   0.4531   1.0000
   5.500   0.8800   0.01732   0.00859  -0.0574   0.4364   1.0000
   5.750   0.9020   0.01767   0.00891  -0.0565   0.4198   1.0000
   6.000   0.9237   0.01804   0.00926  -0.0555   0.4033   1.0000
   6.250   0.9451   0.01844   0.00964  -0.0545   0.3869   1.0000
   6.500   0.9659   0.01885   0.01003  -0.0534   0.3703   1.0000
   6.750   0.9862   0.01929   0.01045  -0.0522   0.3538   1.0000
   7.000   1.0058   0.01976   0.01089  -0.0510   0.3371   1.0000
   7.250   1.0249   0.02026   0.01138  -0.0497   0.3208   1.0000
   7.500   1.0434   0.02078   0.01188  -0.0483   0.3046   1.0000
   7.750   1.0612   0.02133   0.01242  -0.0469   0.2889   1.0000
   8.000   1.0785   0.02191   0.01301  -0.0453   0.2735   1.0000
   8.250   1.0952   0.02251   0.01362  -0.0438   0.2589   1.0000
   8.500   1.1111   0.02314   0.01427  -0.0421   0.2448   1.0000
   8.750   1.1257   0.02379   0.01495  -0.0402   0.2316   1.0000
   9.000   1.1393   0.02449   0.01568  -0.0383   0.2188   1.0000
   9.250   1.1521   0.02526   0.01648  -0.0363   0.2066   1.0000
   9.500   1.1638   0.02609   0.01731  -0.0342   0.1950   1.0000
   9.750   1.1740   0.02700   0.01821  -0.0321   0.1835   1.0000
  10.000   1.1843   0.02793   0.01918  -0.0301   0.1709   1.0000
  10.250   1.1935   0.02894   0.02023  -0.0281   0.1586   1.0000
  10.500   1.2020   0.03004   0.02137  -0.0261   0.1475   1.0000
  10.750   1.2090   0.03126   0.02260  -0.0242   0.1380   1.0000
  11.000   1.2161   0.03254   0.02393  -0.0224   0.1291   1.0000
  11.250   1.2234   0.03389   0.02536  -0.0208   0.1213   1.0000
  11.500   1.2278   0.03545   0.02695  -0.0191   0.1144   1.0000
  11.750   1.2341   0.03699   0.02861  -0.0177   0.1074   1.0000
  12.000   1.2366   0.03883   0.03050  -0.0163   0.1015   1.0000
  12.250   1.2410   0.04066   0.03245  -0.0151   0.0955   1.0000
  12.500   1.2428   0.04274   0.03461  -0.0141   0.0902   1.0000
  12.750   1.2434   0.04504   0.03696  -0.0132   0.0860   1.0000
  13.000   1.2458   0.04730   0.03938  -0.0125   0.0813   1.0000
  13.250   1.2448   0.04994   0.04209  -0.0121   0.0777   1.0000
  13.500   1.2435   0.05272   0.04492  -0.0117   0.0744   1.0000
  13.750   1.2439   0.05548   0.04786  -0.0116   0.0707   1.0000
  14.000   1.2423   0.05851   0.05100  -0.0117   0.0677   1.0000
  14.250   1.2388   0.06182   0.05435  -0.0121   0.0653   1.0000
  14.500   1.2374   0.06505   0.05771  -0.0124   0.0630   1.0000
  14.750   1.2364   0.06839   0.06124  -0.0129   0.0607   1.0000
  15.000   1.2345   0.07191   0.06490  -0.0136   0.0587   1.0000
  15.250   1.2320   0.07557   0.06867  -0.0145   0.0570   1.0000
  15.500   1.2295   0.07930   0.07248  -0.0155   0.0555   1.0000
  15.750   1.2291   0.08269   0.07587  -0.0163   0.0540   1.0000
  16.000   1.2231   0.08730   0.08074  -0.0180   0.0527   1.0000
  16.250   1.2164   0.09213   0.08579  -0.0199   0.0514   1.0000
  16.500   1.2084   0.09731   0.09116  -0.0222   0.0502   1.0000
  16.750   1.2001   0.10265   0.09668  -0.0247   0.0491   1.0000
  17.000   1.1916   0.10811   0.10230  -0.0273   0.0481   1.0000
  17.250   1.1830   0.11374   0.10807  -0.0302   0.0473   1.0000
  17.500   1.1753   0.11928   0.11373  -0.0332   0.0465   1.0000
  17.750   1.1710   0.12411   0.11864  -0.0357   0.0456   1.0000
  18.000   1.1671   0.12892   0.12350  -0.0382   0.0448   1.0000
  18.250   1.1416   0.13895   0.13377  -0.0446   0.0445   1.0000
  18.500   1.1029   0.15285   0.14791  -0.0536   0.0445   1.0000
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