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NACA 23024 (naca23024-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 23024 (naca23024-il)
Reynolds number: 100,000
Max Cl/Cd: 28.49 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca23024-il-100000-n5.txt
Download as CSV file: xf-naca23024-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 23024                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.7868   0.11309   0.10534  -0.0606   1.0000   0.1124
 -19.250  -0.8322   0.10310   0.09506  -0.0648   1.0000   0.1160
 -19.000  -0.8255   0.10130   0.09330  -0.0648   1.0000   0.1182
 -18.750  -0.8231   0.09889   0.09090  -0.0651   1.0000   0.1208
 -18.500  -0.8373   0.09401   0.08591  -0.0666   1.0000   0.1240
 -18.250  -0.8487   0.08967   0.08146  -0.0676   1.0000   0.1271
 -18.000  -0.8428   0.08789   0.07975  -0.0675   1.0000   0.1299
 -17.750  -0.8490   0.08439   0.07619  -0.0681   1.0000   0.1332
 -17.500  -0.8623   0.08001   0.07167  -0.0689   1.0000   0.1369
 -17.250  -0.8569   0.07830   0.07004  -0.0686   1.0000   0.1400
 -17.000  -0.8620   0.07519   0.06689  -0.0687   1.0000   0.1437
 -16.750  -0.8729   0.07141   0.06298  -0.0690   1.0000   0.1479
 -16.500  -0.8697   0.06954   0.06119  -0.0685   1.0000   0.1514
 -16.250  -0.8757   0.06659   0.05819  -0.0684   1.0000   0.1557
 -16.000  -0.8825   0.06361   0.05514  -0.0680   1.0000   0.1601
 -15.750  -0.8828   0.06153   0.05312  -0.0673   1.0000   0.1641
 -15.500  -0.8904   0.05870   0.05021  -0.0667   1.0000   0.1691
 -15.250  -0.8940   0.05640   0.04790  -0.0658   1.0000   0.1736
 -15.000  -0.8973   0.05428   0.04579  -0.0647   1.0000   0.1783
 -14.750  -0.9046   0.05182   0.04323  -0.0635   1.0000   0.1836
 -14.500  -0.9071   0.05000   0.04147  -0.0619   1.0000   0.1883
 -14.250  -0.9125   0.04803   0.03948  -0.0602   1.0000   0.1937
 -14.000  -0.9184   0.04609   0.03747  -0.0583   1.0000   0.1990
 -13.750  -0.9213   0.04461   0.03605  -0.0561   1.0000   0.2039
 -13.500  -0.9274   0.04296   0.03435  -0.0537   1.0000   0.2095
 -13.250  -0.9330   0.04150   0.03288  -0.0510   1.0000   0.2149
 -13.000  -0.9379   0.04027   0.03168  -0.0481   1.0000   0.2200
 -12.750  -0.9455   0.03896   0.03031  -0.0447   1.0000   0.2257
 -12.500  -0.9516   0.03791   0.02928  -0.0412   1.0000   0.2309
 -12.250  -0.9584   0.03697   0.02836  -0.0375   1.0000   0.2359
 -12.000  -0.9674   0.03602   0.02735  -0.0333   1.0000   0.2415
 -11.750  -0.9754   0.03523   0.02657  -0.0291   1.0000   0.2464
 -11.500  -0.9587   0.03434   0.02568  -0.0291   0.9958   0.2538
 -11.250  -0.9366   0.03341   0.02468  -0.0300   0.9896   0.2622
 -11.000  -0.9149   0.03265   0.02394  -0.0305   0.9829   0.2700
 -10.750  -0.8934   0.03184   0.02302  -0.0311   0.9765   0.2788
 -10.500  -0.8719   0.03120   0.02245  -0.0310   0.9685   0.2860
 -10.250  -0.8524   0.03048   0.02161  -0.0309   0.9610   0.2947
 -10.000  -0.8302   0.02992   0.02111  -0.0306   0.9526   0.3019
  -9.750  -0.8098   0.02932   0.02047  -0.0302   0.9448   0.3100
  -9.250  -0.7635   0.02826   0.01940  -0.0297   0.9294   0.3257
  -9.000  -0.7500   0.02771   0.01873  -0.0277   0.9187   0.3337
  -8.750  -0.7163   0.02724   0.01835  -0.0290   0.9137   0.3416
  -8.500  -0.7041   0.02683   0.01790  -0.0264   0.9022   0.3491
  -8.250  -0.6766   0.02630   0.01736  -0.0265   0.8955   0.3572
  -8.000  -0.6415   0.02578   0.01685  -0.0279   0.8912   0.3657
  -7.750  -0.6368   0.02547   0.01646  -0.0238   0.8769   0.3730
  -7.500  -0.6002   0.02499   0.01605  -0.0253   0.8712   0.3808
  -7.250  -0.5793   0.02463   0.01566  -0.0240   0.8615   0.3888
  -7.000  -0.5601   0.02425   0.01521  -0.0224   0.8510   0.3967
  -6.750  -0.5172   0.02377   0.01480  -0.0250   0.8455   0.4052
  -6.500  -0.5077   0.02354   0.01451  -0.0215   0.8324   0.4128
  -6.250  -0.4716   0.02311   0.01410  -0.0229   0.8242   0.4212
  -6.000  -0.4386   0.02275   0.01373  -0.0237   0.8157   0.4301
  -5.750  -0.4266   0.02248   0.01337  -0.0206   0.8028   0.4383
  -5.500  -0.3764   0.02204   0.01299  -0.0246   0.7959   0.4473
  -5.250  -0.3691   0.02191   0.01283  -0.0205   0.7816   0.4551
  -5.000  -0.3294   0.02151   0.01240  -0.0226   0.7730   0.4646
  -4.750  -0.3140   0.02139   0.01231  -0.0199   0.7595   0.4724
  -4.500  -0.2849   0.02107   0.01187  -0.0200   0.7497   0.4827
  -4.250  -0.2626   0.02096   0.01184  -0.0186   0.7368   0.4903
  -4.000  -0.2323   0.02072   0.01154  -0.0188   0.7261   0.5002
  -3.750  -0.2173   0.02062   0.01142  -0.0162   0.7136   0.5088
  -3.500  -0.1857   0.02046   0.01126  -0.0166   0.7026   0.5180
  -3.250  -0.1734   0.02037   0.01111  -0.0134   0.6906   0.5277
  -3.000  -0.1440   0.02026   0.01103  -0.0133   0.6793   0.5367
  -2.750  -0.1247   0.02019   0.01093  -0.0114   0.6680   0.5464
  -2.500  -0.1062   0.02011   0.01083  -0.0094   0.6564   0.5560
  -2.250  -0.0790   0.02007   0.01078  -0.0089   0.6459   0.5658
  -2.000  -0.0704   0.02002   0.01068  -0.0050   0.6344   0.5762
  -1.750  -0.0356   0.01998   0.01066  -0.0060   0.6240   0.5856
  -1.500  -0.0262   0.01999   0.01067  -0.0022   0.6125   0.5963
  -1.250   0.0034   0.01995   0.01059  -0.0022   0.6023   0.6064
  -1.000   0.0167   0.01999   0.01068   0.0009   0.5908   0.6168
  -0.750   0.0372   0.01997   0.01061   0.0026   0.5806   0.6278
  -0.500   0.0587   0.02004   0.01071   0.0041   0.5696   0.6383
  -0.250   0.0709   0.02002   0.01065   0.0073   0.5595   0.6501
   0.000   0.1006   0.02012   0.01078   0.0073   0.5487   0.6602
   0.250   0.1090   0.02013   0.01077   0.0113   0.5385   0.6728
   0.500   0.1430   0.02025   0.01088   0.0104   0.5283   0.6829
   0.750   0.1524   0.02031   0.01098   0.0141   0.5181   0.6954
   1.000   0.1850   0.02045   0.01108   0.0135   0.5083   0.7061
   1.250   0.1978   0.02056   0.01123   0.0165   0.4984   0.7186
   1.500   0.2253   0.02073   0.01140   0.0168   0.4884   0.7295
   1.750   0.2459   0.02088   0.01155   0.0184   0.4791   0.7418
   2.000   0.2696   0.02109   0.01179   0.0193   0.4690   0.7528
   2.250   0.2977   0.02131   0.01195   0.0195   0.4602   0.7646
   2.500   0.3167   0.02155   0.01226   0.0213   0.4503   0.7760
   2.750   0.3469   0.02182   0.01247   0.0210   0.4409   0.7868
   3.000   0.3641   0.02206   0.01276   0.0230   0.4317   0.7987
   3.250   0.3958   0.02242   0.01310   0.0224   0.4220   0.8083
   3.500   0.4121   0.02264   0.01329   0.0246   0.4141   0.8210
   3.750   0.4494   0.02311   0.01379   0.0227   0.4034   0.8284
   4.000   0.4599   0.02326   0.01385   0.0261   0.3968   0.8430
   4.250   0.4989   0.02381   0.01447   0.0237   0.3859   0.8486
   4.500   0.5313   0.02423   0.01483   0.0228   0.3773   0.8565
   4.750   0.5439   0.02453   0.01516   0.0255   0.3697   0.8691
   5.000   0.5788   0.02507   0.01569   0.0239   0.3604   0.8747
   5.250   0.6053   0.02552   0.01607   0.0239   0.3529   0.8834
   5.500   0.6227   0.02594   0.01655   0.0255   0.3449   0.8935
   5.750   0.6556   0.02648   0.01703   0.0243   0.3373   0.8990
   6.000   0.6739   0.02696   0.01752   0.0256   0.3303   0.9093
   6.500   0.7305   0.02801   0.01848   0.0243   0.3163   0.9226
   6.750   0.7465   0.02857   0.01912   0.0257   0.3095   0.9328
   7.000   0.7754   0.02914   0.01970   0.0247   0.3024   0.9389
   7.250   0.7964   0.02965   0.02009   0.0253   0.2973   0.9487
   7.500   0.8233   0.03032   0.02088   0.0242   0.2904   0.9546
   7.750   0.8424   0.03096   0.02152   0.0248   0.2848   0.9640
   8.000   0.8746   0.03146   0.02190   0.0230   0.2794   0.9690
   8.250   0.8940   0.03226   0.02283   0.0230   0.2737   0.9775
   8.500   0.9213   0.03291   0.02351   0.0216   0.2679   0.9828
   8.750   0.9498   0.03349   0.02402   0.0202   0.2632   0.9887
   9.000   0.9746   0.03432   0.02492   0.0190   0.2578   0.9947
   9.250   1.0011   0.03514   0.02580   0.0174   0.2524   0.9999
   9.500   0.9998   0.03572   0.02636   0.0209   0.2493   1.0000
   9.750   1.0025   0.03622   0.02677   0.0240   0.2463   1.0000
  10.000   0.9981   0.03703   0.02765   0.0278   0.2430   1.0000
  10.250   0.9926   0.03797   0.02866   0.0315   0.2396   1.0000
  10.500   0.9901   0.03887   0.02958   0.0347   0.2363   1.0000
  10.750   0.9914   0.03968   0.03038   0.0375   0.2332   1.0000
  11.000   0.9991   0.04031   0.03093   0.0396   0.2303   1.0000
  11.250   0.9955   0.04156   0.03225   0.0424   0.2272   1.0000
  11.500   0.9895   0.04303   0.03382   0.0452   0.2238   1.0000
  11.750   0.9883   0.04434   0.03516   0.0475   0.2206   1.0000
  12.000   0.9919   0.04542   0.03623   0.0494   0.2176   1.0000
  12.250   1.0033   0.04609   0.03682   0.0507   0.2148   1.0000
  12.500   0.9941   0.04818   0.03903   0.0529   0.2118   1.0000
  12.750   0.9837   0.05048   0.04146   0.0549   0.2085   1.0000
  13.000   0.9809   0.05234   0.04338   0.0563   0.2054   1.0000
  13.250   0.9854   0.05368   0.04471   0.0575   0.2026   1.0000
  13.500   1.0012   0.05420   0.04513   0.0583   0.2001   1.0000
  13.750   0.9772   0.05811   0.04926   0.0596   0.1971   1.0000
  14.000   0.9553   0.06216   0.05348   0.0604   0.1938   1.0000
  14.250   0.9475   0.06503   0.05642   0.0609   0.1907   1.0000
  14.500   0.9571   0.06618   0.05753   0.0615   0.1882   1.0000
  14.750   0.9687   0.06717   0.05847   0.0621   0.1858   1.0000
  15.000   0.8161   0.08813   0.08010   0.0574   0.1782   1.0000
  15.250   0.8239   0.08970   0.08165   0.0576   0.1758   1.0000
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