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N-24 (n24-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: N-24 (n24-il)
Reynolds number: 500,000
Max Cl/Cd: 84.43 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n24-il-500000-n5.txt
Download as CSV file: xf-n24-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: N-24                                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.7466   0.08997   0.08665  -0.0437   0.9014   0.0258
 -17.000  -0.8176   0.07430   0.07068  -0.0557   0.8979   0.0257
 -16.750  -0.8597   0.06328   0.05944  -0.0647   0.8923   0.0257
 -16.500  -0.8893   0.05402   0.04995  -0.0729   0.8859   0.0257
 -16.250  -0.9074   0.04581   0.04150  -0.0817   0.8795   0.0257
 -16.000  -0.9182   0.03963   0.03507  -0.0892   0.8705   0.0257
 -15.750  -0.9246   0.03677   0.03202  -0.0894   0.8624   0.0258
 -15.500  -0.9262   0.03485   0.02997  -0.0879   0.8536   0.0259
 -15.250  -0.9194   0.03322   0.02819  -0.0866   0.8461   0.0260
 -15.000  -0.9081   0.03176   0.02660  -0.0856   0.8399   0.0261
 -14.750  -0.8939   0.03043   0.02516  -0.0847   0.8337   0.0262
 -14.500  -0.8781   0.02923   0.02383  -0.0836   0.8278   0.0263
 -14.250  -0.8606   0.02812   0.02259  -0.0826   0.8224   0.0265
 -14.000  -0.8412   0.02707   0.02144  -0.0818   0.8164   0.0266
 -13.750  -0.8211   0.02610   0.02034  -0.0810   0.8103   0.0268
 -13.500  -0.8002   0.02521   0.01932  -0.0801   0.8051   0.0270
 -13.250  -0.7775   0.02436   0.01838  -0.0794   0.7998   0.0272
 -13.000  -0.7544   0.02357   0.01749  -0.0788   0.7940   0.0275
 -12.750  -0.7309   0.02283   0.01662  -0.0780   0.7882   0.0277
 -12.500  -0.7067   0.02211   0.01581  -0.0774   0.7826   0.0279
 -12.250  -0.6818   0.02142   0.01502  -0.0769   0.7764   0.0280
 -12.000  -0.6567   0.02078   0.01428  -0.0763   0.7706   0.0282
 -11.750  -0.6311   0.02019   0.01358  -0.0758   0.7653   0.0284
 -11.500  -0.6048   0.01962   0.01294  -0.0753   0.7594   0.0285
 -11.250  -0.5783   0.01909   0.01232  -0.0749   0.7532   0.0286
 -11.000  -0.5521   0.01853   0.01167  -0.0744   0.7473   0.0288
 -10.750  -0.5259   0.01786   0.01097  -0.0741   0.7406   0.0291
 -10.500  -0.4992   0.01730   0.01036  -0.0737   0.7336   0.0293
 -10.250  -0.4721   0.01681   0.00980  -0.0734   0.7274   0.0296
 -10.000  -0.4443   0.01635   0.00930  -0.0731   0.7207   0.0299
  -9.750  -0.4164   0.01594   0.00883  -0.0729   0.7138   0.0301
  -9.500  -0.3882   0.01556   0.00838  -0.0727   0.7074   0.0305
  -9.250  -0.3596   0.01519   0.00797  -0.0726   0.7001   0.0308
  -9.000  -0.3311   0.01487   0.00757  -0.0724   0.6927   0.0311
  -8.750  -0.3022   0.01455   0.00720  -0.0723   0.6851   0.0315
  -8.500  -0.2732   0.01427   0.00685  -0.0723   0.6768   0.0319
  -8.250  -0.2440   0.01402   0.00652  -0.0722   0.6695   0.0324
  -8.000  -0.2147   0.01376   0.00621  -0.0722   0.6617   0.0329
  -7.500  -0.1562   0.01322   0.00557  -0.0723   0.6471   0.0341
  -7.250  -0.1267   0.01301   0.00530  -0.0723   0.6393   0.0349
  -7.000  -0.0971   0.01282   0.00506  -0.0724   0.6313   0.0357
  -6.750  -0.0674   0.01265   0.00483  -0.0725   0.6216   0.0366
  -6.500  -0.0378   0.01247   0.00460  -0.0726   0.6123   0.0380
  -6.250  -0.0082   0.01229   0.00439  -0.0727   0.6029   0.0406
  -6.000   0.0210   0.01206   0.00426  -0.0729   0.5948   0.0559
  -5.750   0.0511   0.01201   0.00419  -0.0731   0.5860   0.0656
  -5.500   0.0811   0.01199   0.00410  -0.0733   0.5775   0.0699
  -5.250   0.1110   0.01193   0.00402  -0.0735   0.5684   0.0738
  -5.000   0.1410   0.01193   0.00394  -0.0737   0.5609   0.0765
  -4.750   0.1708   0.01183   0.00384  -0.0740   0.5549   0.0791
  -4.500   0.2007   0.01177   0.00376  -0.0742   0.5487   0.0819
  -4.000   0.2605   0.01170   0.00361  -0.0748   0.5370   0.0854
  -3.750   0.2902   0.01164   0.00354  -0.0751   0.5314   0.0877
  -3.500   0.3199   0.01160   0.00349  -0.0754   0.5261   0.0904
  -3.250   0.3497   0.01157   0.00344  -0.0757   0.5215   0.0939
  -3.000   0.3795   0.01151   0.00341  -0.0760   0.5161   0.0988
  -2.750   0.4090   0.01147   0.00339  -0.0763   0.5101   0.1068
  -2.500   0.4383   0.01143   0.00339  -0.0766   0.5045   0.1261
  -2.250   0.4679   0.01136   0.00340  -0.0770   0.4994   0.1477
  -2.000   0.4974   0.01133   0.00341  -0.0774   0.4938   0.1652
  -1.750   0.5267   0.01133   0.00343  -0.0777   0.4882   0.1811
  -1.500   0.5561   0.01131   0.00346  -0.0781   0.4831   0.2000
  -1.250   0.5854   0.01128   0.00349  -0.0785   0.4766   0.2216
  -1.000   0.6143   0.01130   0.00354  -0.0788   0.4694   0.2456
  -0.750   0.6434   0.01128   0.00360  -0.0792   0.4626   0.2757
  -0.500   0.6721   0.01125   0.00366  -0.0795   0.4548   0.3158
  -0.250   0.7006   0.01125   0.00374  -0.0799   0.4476   0.3568
   0.000   0.7289   0.01119   0.00383  -0.0802   0.4390   0.4146
   0.250   0.7561   0.01110   0.00394  -0.0804   0.4303   0.4979
   0.500   0.7823   0.01092   0.00408  -0.0804   0.4198   0.6180
   0.750   0.8070   0.01077   0.00421  -0.0800   0.4087   0.7286
   1.250   0.8980   0.01090   0.00469  -0.0881   0.3793   1.0002
   1.500   0.9239   0.01114   0.00485  -0.0880   0.3687   1.0002
   1.750   0.9494   0.01140   0.00503  -0.0879   0.3597   1.0002
   2.000   0.9748   0.01165   0.00522  -0.0878   0.3512   1.0002
   2.250   0.9997   0.01192   0.00543  -0.0876   0.3437   1.0002
   2.500   1.0248   0.01217   0.00563  -0.0874   0.3367   1.0002
   2.750   1.0486   0.01249   0.00588  -0.0871   0.3294   1.0002
   3.000   1.0734   0.01273   0.00609  -0.0869   0.3238   1.0002
   3.250   1.0976   0.01300   0.00633  -0.0867   0.3184   1.0002
   3.500   1.1207   0.01331   0.00660  -0.0863   0.3134   1.0002
   3.750   1.1441   0.01360   0.00686  -0.0859   0.3092   1.0002
   4.000   1.1677   0.01385   0.00710  -0.0856   0.3048   1.0002
   4.250   1.1900   0.01416   0.00739  -0.0851   0.3003   1.0002
   4.500   1.2111   0.01451   0.00771  -0.0844   0.2963   1.0002
   4.750   1.2316   0.01486   0.00805  -0.0837   0.2928   1.0002
   5.000   1.2533   0.01514   0.00835  -0.0831   0.2893   1.0002
   5.250   1.2717   0.01550   0.00872  -0.0821   0.2850   1.0002
   5.500   1.2872   0.01594   0.00914  -0.0805   0.2810   1.0002
   5.750   1.3026   0.01644   0.00963  -0.0791   0.2774   1.0002
   6.000   1.3209   0.01686   0.01006  -0.0781   0.2742   1.0002
   6.250   1.3402   0.01727   0.01050  -0.0774   0.2710   1.0002
   6.500   1.3589   0.01773   0.01097  -0.0766   0.2679   1.0002
   6.750   1.3766   0.01825   0.01151  -0.0758   0.2648   1.0002
   7.000   1.3934   0.01884   0.01210  -0.0749   0.2617   1.0002
   7.250   1.4099   0.01948   0.01274  -0.0741   0.2588   1.0002
   7.500   1.4292   0.01997   0.01328  -0.0736   0.2563   1.0002
   7.750   1.4475   0.02054   0.01388  -0.0731   0.2533   1.0002
   8.000   1.4646   0.02119   0.01455  -0.0725   0.2500   1.0002
   8.250   1.4802   0.02194   0.01532  -0.0718   0.2466   1.0002
   8.500   1.4945   0.02280   0.01618  -0.0710   0.2433   1.0002
   8.750   1.5117   0.02349   0.01692  -0.0705   0.2405   1.0002
   9.000   1.5282   0.02423   0.01771  -0.0701   0.2370   1.0002
   9.250   1.5428   0.02513   0.01863  -0.0695   0.2329   1.0002
   9.500   1.5549   0.02621   0.01972  -0.0687   0.2287   1.0002
   9.750   1.5686   0.02720   0.02075  -0.0682   0.2247   1.0002
  10.000   1.5822   0.02821   0.02179  -0.0676   0.2195   1.0002
  10.250   1.5911   0.02961   0.02318  -0.0668   0.2135   1.0002
  10.500   1.6018   0.03088   0.02449  -0.0662   0.2073   1.0002
  10.750   1.6089   0.03248   0.02608  -0.0654   0.1996   1.0002
  11.000   1.6157   0.03415   0.02775  -0.0647   0.1920   1.0002
  11.250   1.6188   0.03619   0.02978  -0.0638   0.1838   1.0002
  11.500   1.6239   0.03811   0.03171  -0.0632   0.1755   1.0002
  11.750   1.6254   0.04042   0.03401  -0.0625   0.1679   1.0002
  12.000   1.6282   0.04266   0.03627  -0.0619   0.1607   1.0002
  12.250   1.6288   0.04517   0.03878  -0.0613   0.1547   1.0002
  12.500   1.6306   0.04761   0.04126  -0.0609   0.1487   1.0002
  12.750   1.6289   0.05047   0.04413  -0.0605   0.1433   1.0002
  13.000   1.6295   0.05313   0.04682  -0.0602   0.1379   1.0002
  13.250   1.6253   0.05636   0.05007  -0.0599   0.1325   1.0002
  13.500   1.6237   0.05937   0.05312  -0.0597   0.1280   1.0002
  13.750   1.6221   0.06243   0.05622  -0.0597   0.1241   1.0002
  14.000   1.6184   0.06574   0.05957  -0.0596   0.1208   1.0002
  14.250   1.6165   0.06890   0.06279  -0.0597   0.1182   1.0002
  14.500   1.6163   0.07190   0.06587  -0.0599   0.1158   1.0002
  14.750   1.6153   0.07501   0.06903  -0.0601   0.1134   1.0002
  15.000   1.6114   0.07853   0.07261  -0.0604   0.1112   1.0002
  15.250   1.6055   0.08230   0.07644  -0.0607   0.1089   1.0002
  15.500   1.6025   0.08574   0.07995  -0.0611   0.1071   1.0002
  15.750   1.6011   0.08904   0.08334  -0.0616   0.1052   1.0002
  16.000   1.5992   0.09240   0.08677  -0.0621   0.1031   1.0002
  16.250   1.5940   0.09623   0.09066  -0.0627   0.1010   1.0002
  16.500   1.5870   0.10032   0.09482  -0.0634   0.0989   1.0002
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