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GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 703 AIRFOIL (goe703-il)
Reynolds number: 500,000
Max Cl/Cd: 67 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe703-il-500000.txt
Download as CSV file: xf-goe703-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 703 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.8007   0.10547   0.10188  -0.0659   1.0000   0.0367
 -18.750  -0.8785   0.08867   0.08468  -0.0763   1.0000   0.0363
 -18.500  -0.9111   0.08041   0.07619  -0.0811   1.0000   0.0363
 -18.250  -0.9364   0.07372   0.06931  -0.0844   1.0000   0.0364
 -18.000  -0.9536   0.06855   0.06397  -0.0867   1.0000   0.0364
 -17.750  -0.9677   0.06407   0.05934  -0.0882   1.0000   0.0364
 -17.500  -0.9791   0.06015   0.05527  -0.0891   1.0000   0.0365
 -17.250  -0.9875   0.05678   0.05177  -0.0895   1.0000   0.0366
 -17.000  -0.9947   0.05375   0.04862  -0.0896   1.0000   0.0368
 -16.750  -1.0004   0.05099   0.04573  -0.0892   1.0000   0.0370
 -16.500  -1.0037   0.04857   0.04320  -0.0886   1.0000   0.0370
 -16.250  -1.0079   0.04630   0.04081  -0.0876   1.0000   0.0373
 -16.000  -1.0081   0.04435   0.03875  -0.0865   1.0000   0.0374
 -15.750  -1.0105   0.04245   0.03673  -0.0850   1.0000   0.0377
 -15.500  -1.0100   0.04079   0.03497  -0.0834   1.0000   0.0378
 -15.250  -1.0110   0.03923   0.03329  -0.0815   1.0000   0.0381
 -15.000  -1.0099   0.03784   0.03180  -0.0794   1.0000   0.0382
 -14.750  -1.0081   0.03661   0.03047  -0.0772   1.0000   0.0383
 -14.500  -0.9970   0.03516   0.02900  -0.0758   1.0000   0.0387
 -14.250  -0.9876   0.03397   0.02780  -0.0741   1.0000   0.0390
 -14.000  -0.9801   0.03295   0.02677  -0.0721   1.0000   0.0392
 -13.750  -0.9734   0.03197   0.02577  -0.0698   1.0000   0.0395
 -13.500  -0.9671   0.03107   0.02483  -0.0674   1.0000   0.0397
 -13.250  -0.9620   0.03023   0.02398  -0.0647   1.0000   0.0400
 -13.000  -0.9585   0.02948   0.02320  -0.0616   1.0000   0.0403
 -12.750  -0.9573   0.02883   0.02253  -0.0581   0.9999   0.0406
 -12.500  -0.9283   0.02779   0.02144  -0.0598   0.9979   0.0411
 -12.250  -0.8985   0.02680   0.02039  -0.0615   0.9950   0.0416
 -12.000  -0.8695   0.02584   0.01938  -0.0630   0.9911   0.0421
 -11.750  -0.8419   0.02496   0.01844  -0.0641   0.9867   0.0426
 -11.500  -0.8129   0.02403   0.01745  -0.0655   0.9824   0.0432
 -11.250  -0.7879   0.02291   0.01635  -0.0662   0.9767   0.0439
 -11.000  -0.7620   0.02205   0.01550  -0.0669   0.9691   0.0447
 -10.750  -0.7369   0.02126   0.01470  -0.0673   0.9606   0.0454
 -10.500  -0.7079   0.02050   0.01392  -0.0683   0.9534   0.0463
 -10.250  -0.6766   0.01980   0.01316  -0.0698   0.9455   0.0471
 -10.000  -0.6398   0.01909   0.01239  -0.0723   0.9378   0.0481
  -9.750  -0.6028   0.01807   0.01140  -0.0754   0.9293   0.0497
  -9.500  -0.5566   0.01734   0.01064  -0.0800   0.9212   0.0512
  -9.250  -0.5096   0.01672   0.00995  -0.0847   0.9115   0.0532
  -9.000  -0.4663   0.01597   0.00917  -0.0888   0.8992   0.0555
  -8.750  -0.4309   0.01551   0.00865  -0.0910   0.8842   0.0585
  -8.500  -0.4033   0.01502   0.00811  -0.0916   0.8690   0.0617
  -8.250  -0.3781   0.01466   0.00768  -0.0915   0.8547   0.0661
  -8.000  -0.3593   0.01427   0.00728  -0.0901   0.8408   0.0717
  -7.750  -0.3421   0.01390   0.00691  -0.0883   0.8278   0.0804
  -7.500  -0.3244   0.01351   0.00656  -0.0866   0.8150   0.0969
  -7.250  -0.3093   0.01317   0.00631  -0.0843   0.8016   0.1170
  -7.000  -0.2919   0.01291   0.00608  -0.0824   0.7888   0.1338
  -6.750  -0.2740   0.01272   0.00588  -0.0805   0.7757   0.1472
  -6.500  -0.2560   0.01255   0.00570  -0.0786   0.7626   0.1581
  -6.250  -0.2386   0.01237   0.00551  -0.0767   0.7496   0.1699
  -6.000  -0.2213   0.01220   0.00533  -0.0746   0.7360   0.1800
  -5.750  -0.2025   0.01208   0.00517  -0.0728   0.7228   0.1896
  -5.500  -0.1851   0.01193   0.00500  -0.0708   0.7109   0.2002
  -5.250  -0.1667   0.01179   0.00485  -0.0689   0.6996   0.2108
  -5.000  -0.1480   0.01169   0.00471  -0.0671   0.6893   0.2226
  -4.750  -0.1303   0.01153   0.00458  -0.0651   0.6796   0.2345
  -4.500  -0.1119   0.01142   0.00444  -0.0632   0.6707   0.2477
  -4.000  -0.0749   0.01115   0.00421  -0.0595   0.6554   0.2786
  -3.750  -0.0578   0.01099   0.00409  -0.0574   0.6483   0.2995
  -3.500  -0.0422   0.01077   0.00397  -0.0550   0.6416   0.3253
  -3.250  -0.0304   0.01048   0.00382  -0.0518   0.6353   0.3631
  -3.000  -0.0245   0.01010   0.00366  -0.0475   0.6294   0.4217
  -2.750  -0.0275   0.00960   0.00350  -0.0413   0.6242   0.4985
  -2.500  -0.0329   0.00917   0.00335  -0.0343   0.6188   0.5719
  -2.250  -0.0389   0.00885   0.00328  -0.0271   0.6138   0.6392
  -2.000  -0.0344   0.00864   0.00333  -0.0219   0.6088   0.7084
  -1.750  -0.0110   0.00858   0.00347  -0.0206   0.6037   0.7590
  -1.500   0.0101   0.00864   0.00358  -0.0188   0.5982   0.7896
  -1.250   0.0375   0.00878   0.00371  -0.0185   0.5932   0.8101
  -1.000   0.0571   0.00893   0.00383  -0.0164   0.5883   0.8260
  -0.750   0.0975   0.00912   0.00404  -0.0188   0.5833   0.8362
  -0.250   0.1512   0.00949   0.00433  -0.0178   0.5734   0.8537
   0.000   0.1501   0.00960   0.00439  -0.0114   0.5691   0.8647
   0.250   0.2011   0.00987   0.00467  -0.0161   0.5643   0.8678
   0.500   0.2454   0.01018   0.00496  -0.0193   0.5588   0.8710
   0.750   0.2776   0.01047   0.00520  -0.0199   0.5540   0.8761
   1.000   0.2927   0.01067   0.00534  -0.0170   0.5493   0.8839
   1.250   0.3415   0.01105   0.00573  -0.0211   0.5444   0.8852
   1.500   0.3877   0.01147   0.00613  -0.0246   0.5388   0.8862
   1.750   0.4326   0.01192   0.00652  -0.0278   0.5332   0.8873
   2.000   0.4732   0.01228   0.00684  -0.0303   0.5281   0.8889
   2.250   0.5080   0.01252   0.00710  -0.0315   0.5217   0.8918
   2.500   0.5107   0.01250   0.00706  -0.0262   0.5167   0.9012
   2.750   0.5566   0.01292   0.00740  -0.0298   0.5097   0.9022
   3.000   0.5988   0.01318   0.00769  -0.0325   0.5032   0.9036
   3.250   0.6342   0.01335   0.00783  -0.0340   0.4969   0.9051
   3.500   0.6653   0.01352   0.00794  -0.0347   0.4905   0.9070
   3.750   0.6919   0.01358   0.00804  -0.0345   0.4843   0.9100
   4.000   0.6892   0.01355   0.00800  -0.0283   0.4788   0.9187
   4.250   0.7218   0.01370   0.00809  -0.0294   0.4719   0.9198
   4.500   0.7546   0.01377   0.00820  -0.0305   0.4647   0.9210
   4.750   0.7838   0.01389   0.00828  -0.0309   0.4565   0.9226
   5.000   0.8116   0.01400   0.00838  -0.0310   0.4488   0.9247
   5.250   0.8320   0.01410   0.00847  -0.0296   0.4408   0.9284
   5.500   0.8284   0.01417   0.00850  -0.0232   0.4348   0.9358
   5.750   0.8606   0.01423   0.00860  -0.0243   0.4265   0.9368
   6.000   0.8887   0.01439   0.00871  -0.0246   0.4182   0.9383
   6.250   0.9158   0.01448   0.00882  -0.0247   0.4106   0.9400
   6.500   0.9351   0.01463   0.00894  -0.0232   0.4020   0.9431
   6.750   0.9233   0.01472   0.00904  -0.0152   0.3969   0.9514
   7.000   0.9516   0.01481   0.00912  -0.0156   0.3877   0.9526
   7.250   0.9770   0.01497   0.00926  -0.0155   0.3787   0.9541
   7.500   1.0018   0.01513   0.00942  -0.0153   0.3692   0.9562
   7.750   1.0198   0.01535   0.00961  -0.0138   0.3609   0.9594
   8.000   1.0139   0.01556   0.00985  -0.0073   0.3549   0.9662
   8.500   1.0672   0.01597   0.01023  -0.0081   0.3363   0.9689
   8.750   1.0886   0.01629   0.01051  -0.0075   0.3275   0.9710
   9.000   1.1082   0.01654   0.01079  -0.0066   0.3182   0.9736
   9.250   1.1130   0.01701   0.01123  -0.0029   0.3102   0.9783
   9.500   1.1322   0.01732   0.01156  -0.0020   0.3007   0.9808
   9.750   1.1553   0.01772   0.01194  -0.0022   0.2895   0.9824
  10.250   1.1908   0.01879   0.01296  -0.0009   0.2650   0.9869
  10.500   1.2031   0.01950   0.01365   0.0005   0.2520   0.9899
  10.750   1.2137   0.02038   0.01449   0.0020   0.2380   0.9928
  11.000   1.2299   0.02132   0.01537   0.0020   0.2217   0.9948
  11.250   1.2423   0.02246   0.01645   0.0025   0.2064   0.9972
  11.500   1.2532   0.02378   0.01771   0.0029   0.1923   0.9993
  11.750   1.2525   0.02515   0.01905   0.0055   0.1829   1.0000
  12.000   1.2494   0.02627   0.02018   0.0089   0.1766   1.0000
  12.250   1.2421   0.02769   0.02158   0.0125   0.1707   1.0000
  12.500   1.2399   0.02890   0.02282   0.0156   0.1667   1.0000
  12.750   1.2378   0.03019   0.02413   0.0184   0.1625   1.0000
  13.000   1.2332   0.03169   0.02565   0.0213   0.1589   1.0000
  13.250   1.2287   0.03328   0.02725   0.0241   0.1556   1.0000
  13.500   1.2305   0.03451   0.02853   0.0262   0.1530   1.0000
  13.750   1.2300   0.03597   0.03003   0.0284   0.1499   1.0000
  14.000   1.2275   0.03764   0.03172   0.0305   0.1468   1.0000
  14.250   1.2233   0.03951   0.03359   0.0326   0.1439   1.0000
  14.500   1.2249   0.04100   0.03513   0.0343   0.1413   1.0000
  14.750   1.2269   0.04250   0.03668   0.0359   0.1385   1.0000
  15.000   1.2269   0.04421   0.03843   0.0375   0.1355   1.0000
  15.250   1.2239   0.04625   0.04048   0.0390   0.1328   1.0000
  15.500   1.2226   0.04818   0.04244   0.0404   0.1302   1.0000
  15.750   1.2270   0.04971   0.04403   0.0414   0.1274   1.0000
  16.000   1.2278   0.05157   0.04593   0.0425   0.1244   1.0000
  16.250   1.2247   0.05386   0.04823   0.0435   0.1212   1.0000
  16.500   1.2245   0.05595   0.05037   0.0444   0.1178   1.0000
  16.750   1.2262   0.05793   0.05239   0.0451   0.1136   1.0000
  17.000   1.2211   0.06062   0.05509   0.0458   0.1096   1.0000
  17.250   1.2225   0.06271   0.05723   0.0464   0.1044   1.0000
  17.500   1.2186   0.06542   0.05996   0.0468   0.1001   1.0000
  17.750   1.2172   0.06792   0.06249   0.0472   0.0936   1.0000
  18.000   1.2118   0.07094   0.06551   0.0474   0.0874   1.0000
  18.250   1.2058   0.07407   0.06864   0.0475   0.0818   1.0000
  18.500   1.2001   0.07719   0.07177   0.0475   0.0766   1.0000
  18.750   1.1910   0.08080   0.07538   0.0474   0.0732   1.0000
  19.000   1.1855   0.08402   0.07863   0.0472   0.0708   1.0000
  19.250   1.1783   0.08752   0.08215   0.0469   0.0687   1.0000
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