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NACA 23024 (naca23024-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: NACA 23024 (naca23024-il)
Reynolds number: 200,000
Max Cl/Cd: 41.34 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca23024-il-200000.txt
Download as CSV file: xf-naca23024-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0718   0.07630   0.06929  -0.0759   1.0000   0.1090
 -19.500  -1.0636   0.07480   0.06785  -0.0755   1.0000   0.1112
 -19.250  -1.0632   0.07237   0.06536  -0.0756   1.0000   0.1134
 -19.000  -1.0689   0.06927   0.06212  -0.0758   1.0000   0.1156
 -18.750  -1.0633   0.06755   0.06041  -0.0753   1.0000   0.1180
 -18.500  -1.0565   0.06598   0.05890  -0.0748   1.0000   0.1206
 -18.250  -1.0556   0.06375   0.05663  -0.0745   1.0000   0.1232
 -18.000  -1.0624   0.06076   0.05347  -0.0744   1.0000   0.1259
 -17.750  -1.0511   0.05976   0.05260  -0.0735   1.0000   0.1289
 -17.500  -1.0484   0.05787   0.05071  -0.0729   1.0000   0.1319
 -17.250  -1.0515   0.05544   0.04818  -0.0723   1.0000   0.1354
 -17.000  -1.0462   0.05389   0.04669  -0.0714   1.0000   0.1388
 -16.750  -1.0440   0.05211   0.04493  -0.0705   1.0000   0.1422
 -16.500  -1.0461   0.04997   0.04270  -0.0695   1.0000   0.1461
 -16.250  -1.0431   0.04836   0.04115  -0.0683   1.0000   0.1502
 -16.000  -1.0429   0.04659   0.03940  -0.0670   1.0000   0.1543
 -15.750  -1.0460   0.04460   0.03729  -0.0656   1.0000   0.1588
 -15.500  -1.0431   0.04319   0.03601  -0.0640   1.0000   0.1633
 -15.250  -1.0451   0.04149   0.03428  -0.0622   1.0000   0.1683
 -15.000  -1.0459   0.03994   0.03270  -0.0603   1.0000   0.1732
 -14.750  -1.0470   0.03851   0.03133  -0.0581   1.0000   0.1782
 -14.500  -1.0506   0.03702   0.02975  -0.0557   1.0000   0.1838
 -14.250  -1.0513   0.03579   0.02862  -0.0532   1.0000   0.1889
 -14.000  -1.0553   0.03454   0.02736  -0.0502   1.0000   0.1945
 -13.750  -1.0589   0.03340   0.02620  -0.0471   1.0000   0.2002
 -13.500  -1.0632   0.03239   0.02525  -0.0437   1.0000   0.2054
 -13.250  -1.0703   0.03141   0.02420  -0.0398   1.0000   0.2113
 -13.000  -1.0749   0.03058   0.02343  -0.0359   1.0000   0.2166
 -12.750  -1.0821   0.02982   0.02269  -0.0317   1.0000   0.2220
 -12.500  -1.0919   0.02911   0.02188  -0.0269   1.0000   0.2277
 -12.250  -1.0970   0.02850   0.02137  -0.0226   1.0000   0.2327
 -12.000  -1.1056   0.02795   0.02082  -0.0178   1.0000   0.2379
 -11.750  -1.1057   0.02742   0.02018  -0.0145   0.9987   0.2445
 -11.500  -1.0759   0.02689   0.01975  -0.0162   0.9934   0.2532
 -11.250  -1.0501   0.02633   0.01911  -0.0171   0.9872   0.2622
 -11.000  -1.0217   0.02585   0.01871  -0.0183   0.9813   0.2708
 -10.750  -0.9958   0.02539   0.01816  -0.0190   0.9752   0.2795
 -10.500  -0.9688   0.02492   0.01776  -0.0195   0.9682   0.2877
 -10.250  -0.9380   0.02453   0.01727  -0.0209   0.9639   0.2970
 -10.000  -0.9169   0.02403   0.01688  -0.0201   0.9544   0.3043
  -9.750  -0.8867   0.02364   0.01639  -0.0210   0.9495   0.3133
  -9.500  -0.8643   0.02318   0.01602  -0.0203   0.9405   0.3206
  -9.250  -0.8346   0.02277   0.01559  -0.0208   0.9347   0.3294
  -9.000  -0.7957   0.02226   0.01509  -0.0231   0.9316   0.3384
  -8.750  -0.7834   0.02196   0.01482  -0.0202   0.9197   0.3454
  -8.500  -0.7538   0.02151   0.01424  -0.0205   0.9149   0.3541
  -8.250  -0.7074   0.02090   0.01379  -0.0239   0.9129   0.3636
  -8.000  -0.7008   0.02069   0.01352  -0.0197   0.8996   0.3705
  -7.750  -0.6609   0.02008   0.01295  -0.0218   0.8960   0.3795
  -7.500  -0.6191   0.01953   0.01242  -0.0243   0.8931   0.3891
  -7.250  -0.6112   0.01932   0.01212  -0.0202   0.8805   0.3962
  -7.000  -0.5640   0.01876   0.01169  -0.0237   0.8757   0.4056
  -6.750  -0.5207   0.01824   0.01108  -0.0266   0.8711   0.4157
  -6.500  -0.4563   0.01758   0.01054  -0.0336   0.8680   0.4262
  -6.250  -0.4532   0.01749   0.01041  -0.0284   0.8523   0.4333
  -6.000  -0.4017   0.01695   0.00987  -0.0329   0.8459   0.4433
  -5.750  -0.3844   0.01681   0.00975  -0.0305   0.8325   0.4512
  -5.500  -0.3565   0.01654   0.00934  -0.0303   0.8221   0.4606
  -5.250  -0.3256   0.01627   0.00920  -0.0306   0.8096   0.4690
  -5.000  -0.2973   0.01606   0.00891  -0.0304   0.7983   0.4787
  -4.750  -0.2800   0.01591   0.00875  -0.0280   0.7847   0.4870
  -4.500  -0.2457   0.01571   0.00854  -0.0289   0.7737   0.4965
  -4.250  -0.2414   0.01569   0.00844  -0.0239   0.7596   0.5051
  -4.000  -0.2001   0.01546   0.00823  -0.0263   0.7486   0.5148
  -3.750  -0.1936   0.01545   0.00821  -0.0217   0.7347   0.5235
  -3.500  -0.1626   0.01531   0.00799  -0.0221   0.7237   0.5336
  -3.250  -0.1518   0.01528   0.00803  -0.0183   0.7101   0.5421
  -3.000  -0.1310   0.01525   0.00782  -0.0166   0.6993   0.5526
  -2.750  -0.1131   0.01517   0.00788  -0.0143   0.6862   0.5614
  -2.500  -0.0897   0.01515   0.00775  -0.0131   0.6752   0.5721
  -2.250  -0.0782   0.01510   0.00776  -0.0095   0.6626   0.5813
  -2.000  -0.0526   0.01509   0.00769  -0.0087   0.6516   0.5918
  -1.750  -0.0457   0.01508   0.00767  -0.0042   0.6399   0.6021
  -1.500  -0.0179   0.01504   0.00765  -0.0038   0.6285   0.6123
  -1.250  -0.0099   0.01506   0.00763   0.0004   0.6175   0.6233
  -1.000   0.0157   0.01502   0.00763   0.0012   0.6060   0.6334
  -0.750   0.0296   0.01505   0.00763   0.0043   0.5956   0.6450
  -0.500   0.0483   0.01503   0.00764   0.0064   0.5846   0.6556
  -0.250   0.0689   0.01509   0.00765   0.0082   0.5746   0.6675
   0.000   0.0818   0.01506   0.00768   0.0115   0.5639   0.6786
   0.250   0.1093   0.01516   0.00770   0.0119   0.5540   0.6907
   0.500   0.1177   0.01514   0.00776   0.0160   0.5441   0.7026
   0.750   0.1405   0.01521   0.00783   0.0173   0.5343   0.7146
   1.000   0.1570   0.01526   0.00789   0.0198   0.5249   0.7272
   1.250   0.1751   0.01532   0.00800   0.0221   0.5148   0.7394
   1.500   0.1998   0.01544   0.00806   0.0230   0.5055   0.7520
   1.750   0.2130   0.01550   0.00821   0.0262   0.4957   0.7648
   2.000   0.2405   0.01566   0.00831   0.0265   0.4862   0.7771
   2.250   0.2532   0.01576   0.00848   0.0298   0.4772   0.7908
   2.500   0.2804   0.01593   0.00867   0.0301   0.4672   0.8023
   2.750   0.2972   0.01610   0.00879   0.0325   0.4588   0.8165
   3.000   0.3270   0.01634   0.00911   0.0323   0.4481   0.8268
   3.250   0.3521   0.01659   0.00924   0.0330   0.4393   0.8401
   3.500   0.3828   0.01691   0.00966   0.0325   0.4287   0.8496
   3.750   0.4283   0.01740   0.01002   0.0291   0.4180   0.8580
   4.000   0.4425   0.01760   0.01031   0.0319   0.4091   0.8706
   4.250   0.4988   0.01822   0.01080   0.0262   0.3975   0.8745
   4.500   0.5328   0.01868   0.01132   0.0249   0.3871   0.8816
   4.750   0.5526   0.01898   0.01155   0.0265   0.3788   0.8927
   5.000   0.5972   0.01963   0.01220   0.0232   0.3682   0.8956
   5.250   0.6368   0.02022   0.01272   0.0209   0.3587   0.8994
   5.500   0.6637   0.02073   0.01321   0.0210   0.3503   0.9073
   5.750   0.6879   0.02114   0.01363   0.0215   0.3420   0.9148
   6.000   0.7304   0.02179   0.01416   0.0185   0.3333   0.9178
   6.250   0.7587   0.02227   0.01469   0.0181   0.3253   0.9245
   6.500   0.7830   0.02270   0.01504   0.0185   0.3186   0.9331
   6.750   0.8206   0.02327   0.01562   0.0161   0.3109   0.9369
   7.000   0.8466   0.02372   0.01608   0.0160   0.3042   0.9449
   7.250   0.8823   0.02427   0.01646   0.0141   0.2975   0.9504
   7.500   0.9121   0.02472   0.01702   0.0129   0.2910   0.9558
   7.750   0.9347   0.02518   0.01749   0.0132   0.2854   0.9645
   8.000   0.9778   0.02569   0.01785   0.0097   0.2789   0.9675
   8.250   1.0028   0.02614   0.01843   0.0092   0.2735   0.9747
   8.500   1.0323   0.02655   0.01884   0.0079   0.2677   0.9805
   8.750   1.0756   0.02703   0.01915   0.0043   0.2622   0.9841
   9.000   1.0984   0.02757   0.01984   0.0039   0.2575   0.9912
   9.250   1.1308   0.02788   0.02018   0.0017   0.2520   0.9960
   9.500   1.1692   0.02828   0.02047  -0.0012   0.2470   1.0000
   9.750   1.1700   0.02872   0.02093   0.0025   0.2439   1.0000
  10.000   1.1613   0.02917   0.02147   0.0075   0.2411   1.0000
  10.250   1.1571   0.02964   0.02198   0.0119   0.2381   1.0000
  10.500   1.1570   0.03008   0.02243   0.0156   0.2352   1.0000
  10.750   1.1612   0.03052   0.02281   0.0187   0.2322   1.0000
  11.000   1.1732   0.03106   0.02328   0.0206   0.2288   1.0000
  11.250   1.1637   0.03178   0.02411   0.0254   0.2263   1.0000
  11.500   1.1591   0.03250   0.02491   0.0293   0.2233   1.0000
  11.750   1.1606   0.03317   0.02559   0.0324   0.2204   1.0000
  12.000   1.1680   0.03375   0.02613   0.0347   0.2175   1.0000
  12.250   1.1884   0.03427   0.02652   0.0354   0.2140   1.0000
  12.500   1.1775   0.03543   0.02784   0.0395   0.2117   1.0000
  12.750   1.1735   0.03654   0.02905   0.0426   0.2089   1.0000
  13.000   1.1756   0.03750   0.03004   0.0450   0.2059   1.0000
  13.250   1.1844   0.03825   0.03076   0.0467   0.2032   1.0000
  13.500   1.2107   0.03860   0.03095   0.0468   0.1998   1.0000
  13.750   1.1951   0.04039   0.03293   0.0502   0.1976   1.0000
  14.000   1.1883   0.04201   0.03468   0.0526   0.1950   1.0000
  14.250   1.1886   0.04338   0.03611   0.0544   0.1922   1.0000
  14.500   1.1977   0.04428   0.03698   0.0556   0.1895   1.0000
  14.750   1.2235   0.04451   0.03705   0.0558   0.1866   1.0000
  15.000   1.2089   0.04686   0.03960   0.0580   0.1844   1.0000
  15.250   1.1952   0.04938   0.04227   0.0597   0.1818   1.0000
  15.500   1.1915   0.05136   0.04433   0.0609   0.1792   1.0000
  15.750   1.1991   0.05254   0.04550   0.0616   0.1767   1.0000
  16.000   1.2241   0.05257   0.04539   0.0620   0.1740   1.0000
  16.250   1.2095   0.05558   0.04857   0.0630   0.1718   1.0000
  16.500   1.1860   0.05949   0.05269   0.0638   0.1693   1.0000
  16.750   1.1760   0.06247   0.05577   0.0642   0.1669   1.0000
  17.000   1.1831   0.06391   0.05721   0.0645   0.1645   1.0000
  17.250   1.2140   0.06318   0.05631   0.0649   0.1620   1.0000
  17.500   1.1926   0.06747   0.06078   0.0650   0.1599   1.0000
  17.750   1.1467   0.07456   0.06816   0.0640   0.1574   1.0000
  18.000   1.1199   0.08007   0.07384   0.0630   0.1549   1.0000
  18.250   1.1351   0.08075   0.07447   0.0631   0.1526   1.0000
  18.500   1.1809   0.07796   0.07146   0.0643   0.1506   1.0000
  18.750   1.1037   0.08971   0.08362   0.0611   0.1480   1.0000
  19.000   0.5502   0.19082   0.18576   0.0216   0.1209   1.0000
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