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GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 703 AIRFOIL (goe703-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.51 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe703-il-1000000.txt
Download as CSV file: xf-goe703-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0395   0.07966   0.07579  -0.0760   1.0000   0.0286
 -19.500  -1.0481   0.07534   0.07138  -0.0779   1.0000   0.0286
 -19.250  -1.0560   0.07115   0.06710  -0.0797   1.0000   0.0288
 -19.000  -1.0625   0.06720   0.06305  -0.0813   1.0000   0.0289
 -18.750  -1.0689   0.06344   0.05921  -0.0826   1.0000   0.0289
 -18.500  -1.0732   0.05999   0.05567  -0.0837   1.0000   0.0291
 -18.250  -1.0774   0.05667   0.05227  -0.0846   1.0000   0.0292
 -18.000  -1.0802   0.05367   0.04918  -0.0852   1.0000   0.0293
 -17.750  -1.0822   0.05083   0.04626  -0.0856   1.0000   0.0294
 -17.500  -1.0840   0.04814   0.04350  -0.0857   1.0000   0.0294
 -17.250  -1.0839   0.04575   0.04103  -0.0855   1.0000   0.0295
 -17.000  -1.0829   0.04357   0.03877  -0.0852   1.0000   0.0297
 -16.750  -1.0820   0.04149   0.03662  -0.0846   1.0000   0.0298
 -16.500  -1.0804   0.03957   0.03463  -0.0837   1.0000   0.0298
 -16.250  -1.0755   0.03802   0.03301  -0.0828   1.0000   0.0300
 -16.000  -1.0733   0.03635   0.03128  -0.0815   1.0000   0.0300
 -15.750  -1.0741   0.03455   0.02941  -0.0798   1.0000   0.0302
 -15.500  -1.0761   0.03276   0.02757  -0.0778   1.0000   0.0304
 -15.250  -1.0769   0.03117   0.02593  -0.0756   1.0000   0.0307
 -15.000  -1.0750   0.02986   0.02458  -0.0734   1.0000   0.0309
 -14.750  -1.0708   0.02877   0.02345  -0.0712   1.0000   0.0310
 -14.500  -1.0668   0.02774   0.02239  -0.0688   1.0000   0.0312
 -14.250  -1.0625   0.02680   0.02141  -0.0662   1.0000   0.0314
 -14.000  -1.0579   0.02596   0.02054  -0.0635   1.0000   0.0316
 -13.750  -1.0536   0.02519   0.01974  -0.0606   1.0000   0.0318
 -13.500  -1.0300   0.02423   0.01874  -0.0614   0.9989   0.0320
 -13.250  -1.0033   0.02339   0.01787  -0.0626   0.9972   0.0324
 -13.000  -0.9750   0.02258   0.01702  -0.0640   0.9948   0.0327
 -12.750  -0.9492   0.02179   0.01620  -0.0648   0.9913   0.0331
 -12.500  -0.9250   0.02100   0.01538  -0.0653   0.9872   0.0334
 -12.250  -0.8981   0.02027   0.01461  -0.0661   0.9827   0.0337
 -12.000  -0.8741   0.01966   0.01396  -0.0662   0.9749   0.0339
 -11.750  -0.8515   0.01883   0.01310  -0.0663   0.9653   0.0343
 -11.500  -0.8260   0.01792   0.01216  -0.0670   0.9542   0.0349
 -11.250  -0.7890   0.01719   0.01141  -0.0698   0.9441   0.0355
 -11.000  -0.7449   0.01656   0.01075  -0.0739   0.9331   0.0362
 -10.750  -0.6965   0.01600   0.01013  -0.0790   0.9185   0.0370
 -10.500  -0.6469   0.01554   0.00960  -0.0842   0.9047   0.0379
 -10.250  -0.6002   0.01507   0.00905  -0.0888   0.8911   0.0385
 -10.000  -0.5647   0.01454   0.00844  -0.0912   0.8753   0.0398
  -9.750  -0.5355   0.01421   0.00804  -0.0921   0.8601   0.0410
  -9.500  -0.5111   0.01393   0.00770  -0.0918   0.8467   0.0417
  -9.250  -0.4871   0.01370   0.00739  -0.0914   0.8340   0.0427
  -9.000  -0.4667   0.01341   0.00705  -0.0902   0.8225   0.0437
  -8.750  -0.4468   0.01311   0.00672  -0.0890   0.8116   0.0454
  -8.500  -0.4268   0.01289   0.00645  -0.0877   0.8002   0.0471
  -8.250  -0.4076   0.01263   0.00616  -0.0862   0.7896   0.0492
  -8.000  -0.3890   0.01239   0.00589  -0.0845   0.7768   0.0517
  -7.750  -0.3699   0.01216   0.00563  -0.0829   0.7653   0.0552
  -7.500  -0.3517   0.01194   0.00538  -0.0811   0.7522   0.0595
  -7.250  -0.3342   0.01166   0.00511  -0.0792   0.7384   0.0668
  -7.000  -0.3182   0.01137   0.00485  -0.0771   0.7236   0.0797
  -6.750  -0.3028   0.01110   0.00460  -0.0747   0.7078   0.0971
  -6.500  -0.2864   0.01087   0.00441  -0.0726   0.6925   0.1128
  -6.250  -0.2681   0.01069   0.00424  -0.0708   0.6792   0.1265
  -6.000  -0.2497   0.01054   0.00410  -0.0689   0.6674   0.1378
  -5.750  -0.2305   0.01042   0.00396  -0.0672   0.6566   0.1477
  -5.500  -0.2111   0.01031   0.00384  -0.0656   0.6474   0.1568
  -5.250  -0.1918   0.01017   0.00372  -0.0639   0.6391   0.1662
  -5.000  -0.1726   0.01009   0.00361  -0.0621   0.6309   0.1751
  -4.750  -0.1521   0.00995   0.00351  -0.0607   0.6250   0.1858
  -4.500  -0.1322   0.00983   0.00341  -0.0591   0.6185   0.1969
  -4.000  -0.0926   0.00962   0.00323  -0.0558   0.6065   0.2195
  -3.750  -0.0728   0.00950   0.00315  -0.0542   0.6011   0.2330
  -3.500  -0.0535   0.00941   0.00307  -0.0524   0.5954   0.2462
  -3.250  -0.0348   0.00932   0.00300  -0.0505   0.5895   0.2619
  -3.000  -0.0150   0.00916   0.00292  -0.0489   0.5854   0.2811
  -2.750   0.0029   0.00899   0.00284  -0.0468   0.5806   0.3056
  -2.500   0.0185   0.00880   0.00274  -0.0443   0.5756   0.3351
  -2.250   0.0291   0.00855   0.00264  -0.0408   0.5701   0.3839
  -2.000   0.0329   0.00810   0.00251  -0.0359   0.5669   0.4625
  -1.750   0.0365   0.00774   0.00240  -0.0308   0.5631   0.5290
  -1.500   0.0349   0.00742   0.00230  -0.0245   0.5592   0.5886
  -1.250   0.0279   0.00714   0.00223  -0.0169   0.5549   0.6480
  -1.000   0.0173   0.00696   0.00222  -0.0084   0.5506   0.7012
  -0.750   0.0158   0.00681   0.00224  -0.0018   0.5475   0.7467
  -0.500   0.0273   0.00671   0.00227   0.0019   0.5441   0.7807
  -0.250   0.0433   0.00669   0.00231   0.0047   0.5399   0.8053
   0.000   0.0619   0.00671   0.00235   0.0069   0.5354   0.8228
   0.250   0.0830   0.00678   0.00241   0.0085   0.5301   0.8353
   0.500   0.0998   0.00679   0.00243   0.0111   0.5271   0.8467
   0.750   0.1283   0.00683   0.00250   0.0110   0.5231   0.8555
   1.000   0.1399   0.00685   0.00250   0.0147   0.5189   0.8646
   1.250   0.1715   0.00697   0.00261   0.0140   0.5135   0.8718
   1.500   0.1799   0.00702   0.00264   0.0184   0.5093   0.8808
   1.750   0.2122   0.00709   0.00273   0.0175   0.5056   0.8863
   2.000   0.2365   0.00718   0.00282   0.0184   0.5000   0.8920
   2.250   0.2363   0.00720   0.00281   0.0247   0.4947   0.9001
   2.500   0.2752   0.00737   0.00297   0.0223   0.4888   0.9040
   2.750   0.3085   0.00753   0.00314   0.0212   0.4832   0.9087
   3.000   0.3167   0.00761   0.00321   0.0256   0.4786   0.9163
   3.250   0.3487   0.00783   0.00339   0.0248   0.4727   0.9203
   3.500   0.3901   0.00801   0.00359   0.0219   0.4672   0.9223
   3.750   0.4249   0.00820   0.00375   0.0203   0.4602   0.9243
   4.000   0.4552   0.00843   0.00394   0.0197   0.4533   0.9271
   4.250   0.4508   0.00841   0.00394   0.0268   0.4494   0.9352
   4.500   0.4917   0.00863   0.00414   0.0239   0.4418   0.9363
   4.750   0.5269   0.00885   0.00431   0.0221   0.4331   0.9372
   5.000   0.5624   0.00901   0.00445   0.0203   0.4238   0.9378
   5.250   0.5945   0.00921   0.00460   0.0191   0.4147   0.9386
   5.500   0.6257   0.00938   0.00475   0.0182   0.4054   0.9396
   5.750   0.6545   0.00960   0.00493   0.0178   0.3971   0.9409
   6.000   0.6828   0.00976   0.00508   0.0175   0.3891   0.9424
   6.250   0.6692   0.00978   0.00509   0.0261   0.3839   0.9511
   6.500   0.7024   0.00998   0.00526   0.0246   0.3748   0.9517
   7.000   0.7636   0.01046   0.00568   0.0227   0.3559   0.9531
   7.500   0.8202   0.01098   0.00615   0.0216   0.3381   0.9547
   7.750   0.8461   0.01132   0.00644   0.0215   0.3282   0.9558
   8.000   0.8736   0.01157   0.00667   0.0211   0.3194   0.9571
   8.250   0.8954   0.01191   0.00698   0.0217   0.3107   0.9591
   8.500   0.8935   0.01207   0.00715   0.0275   0.3055   0.9660
   8.750   0.9208   0.01242   0.00747   0.0268   0.2959   0.9667
   9.000   0.9492   0.01274   0.00777   0.0260   0.2867   0.9674
   9.250   0.9748   0.01320   0.00817   0.0256   0.2742   0.9683
   9.500   0.9991   0.01367   0.00860   0.0253   0.2621   0.9693
   9.750   1.0212   0.01419   0.00907   0.0254   0.2479   0.9707
  10.000   1.0402   0.01479   0.00961   0.0259   0.2332   0.9724
  10.250   1.0548   0.01550   0.01025   0.0271   0.2179   0.9750
  10.500   1.0557   0.01634   0.01103   0.0309   0.2029   0.9801
  10.750   1.0737   0.01731   0.01190   0.0308   0.1853   0.9810
  11.000   1.0917   0.01826   0.01279   0.0307   0.1717   0.9819
  11.250   1.1101   0.01916   0.01366   0.0305   0.1620   0.9830
  11.500   1.1271   0.02014   0.01461   0.0305   0.1534   0.9843
  11.750   1.1441   0.02109   0.01554   0.0304   0.1471   0.9857
  12.000   1.1606   0.02208   0.01654   0.0305   0.1423   0.9875
  12.250   1.1778   0.02296   0.01744   0.0306   0.1386   0.9893
  12.500   1.1898   0.02403   0.01851   0.0314   0.1356   0.9915
  12.750   1.2029   0.02520   0.01969   0.0317   0.1319   0.9928
  13.000   1.2220   0.02618   0.02071   0.0310   0.1295   0.9936
  13.250   1.2403   0.02721   0.02177   0.0305   0.1265   0.9945
  13.500   1.2561   0.02843   0.02299   0.0300   0.1235   0.9956
  13.750   1.2694   0.02993   0.02451   0.0295   0.1200   0.9969
  14.000   1.2870   0.03111   0.02573   0.0288   0.1176   0.9980
  14.250   1.3030   0.03243   0.02709   0.0282   0.1146   0.9989
  14.500   1.3149   0.03413   0.02879   0.0277   0.1110   0.9997
  14.750   1.3203   0.03570   0.03039   0.0285   0.1077   1.0000
  15.000   1.3226   0.03707   0.03180   0.0303   0.1044   1.0000
  15.250   1.3186   0.03899   0.03371   0.0323   0.1000   1.0000
  15.500   1.3193   0.04059   0.03534   0.0339   0.0956   1.0000
  15.750   1.3147   0.04267   0.03740   0.0356   0.0883   1.0000
  16.000   1.3066   0.04513   0.03983   0.0373   0.0782   1.0000
  16.250   1.2941   0.04809   0.04274   0.0390   0.0695   1.0000
  16.500   1.2840   0.05093   0.04557   0.0404   0.0649   1.0000
  16.750   1.2776   0.05350   0.04817   0.0415   0.0624   1.0000
  17.000   1.2703   0.05628   0.05097   0.0425   0.0601   1.0000
  17.250   1.2675   0.05869   0.05344   0.0433   0.0590   1.0000
  17.500   1.2650   0.06111   0.05590   0.0440   0.0580   1.0000
  17.750   1.2590   0.06397   0.05881   0.0446   0.0569   1.0000
  18.000   1.2534   0.06686   0.06174   0.0450   0.0558   1.0000
  18.250   1.2457   0.07005   0.06498   0.0453   0.0545   1.0000
  18.500   1.2443   0.07261   0.06760   0.0456   0.0539   1.0000
  18.750   1.2428   0.07519   0.07024   0.0458   0.0532   1.0000
  19.000   1.2402   0.07796   0.07307   0.0458   0.0525   1.0000
  19.250   1.2372   0.08081   0.07597   0.0458   0.0518   1.0000
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