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GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 703 AIRFOIL (goe703-il)
Reynolds number: 100,000
Max Cl/Cd: 43.02 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe703-il-100000-n5.txt
Download as CSV file: xf-goe703-il-100000-n5.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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.7311   0.07282   0.06538  -0.0846   1.0000   0.0536
 -15.000  -0.7553   0.06769   0.06006  -0.0858   1.0000   0.0536
 -14.750  -0.7717   0.06382   0.05603  -0.0860   1.0000   0.0538
 -14.500  -0.7826   0.06072   0.05281  -0.0855   1.0000   0.0541
 -14.250  -0.7930   0.05786   0.04982  -0.0845   1.0000   0.0542
 -14.000  -0.7998   0.05551   0.04738  -0.0832   1.0000   0.0546
 -13.750  -0.8063   0.05330   0.04507  -0.0815   1.0000   0.0550
 -13.500  -0.8121   0.05131   0.04299  -0.0794   1.0000   0.0555
 -13.250  -0.8175   0.04945   0.04101  -0.0771   1.0000   0.0560
 -13.000  -0.8220   0.04773   0.03917  -0.0745   1.0000   0.0565
 -12.750  -0.8270   0.04613   0.03745  -0.0716   1.0000   0.0571
 -12.500  -0.8307   0.04469   0.03588  -0.0684   1.0000   0.0577
 -12.250  -0.8347   0.04337   0.03443  -0.0650   1.0000   0.0583
 -12.000  -0.8390   0.04219   0.03311  -0.0612   1.0000   0.0589
 -11.750  -0.8434   0.04122   0.03202  -0.0572   1.0000   0.0593
 -11.500  -0.8449   0.04044   0.03129  -0.0534   1.0000   0.0598
 -11.250  -0.8217   0.03915   0.03001  -0.0542   0.9957   0.0607
 -11.000  -0.7942   0.03778   0.02859  -0.0557   0.9886   0.0618
 -10.750  -0.7667   0.03647   0.02720  -0.0572   0.9816   0.0632
 -10.500  -0.7410   0.03523   0.02582  -0.0581   0.9733   0.0647
 -10.250  -0.7126   0.03403   0.02456  -0.0595   0.9665   0.0665
 -10.000  -0.6901   0.03297   0.02352  -0.0597   0.9565   0.0682
  -9.750  -0.6632   0.03190   0.02239  -0.0607   0.9489   0.0706
  -9.500  -0.6373   0.03087   0.02128  -0.0612   0.9400   0.0732
  -9.250  -0.6104   0.02982   0.02025  -0.0621   0.9325   0.0758
  -9.000  -0.5838   0.02886   0.01923  -0.0627   0.9234   0.0790
  -8.750  -0.5505   0.02779   0.01816  -0.0647   0.9177   0.0834
  -8.500  -0.5248   0.02698   0.01731  -0.0650   0.9069   0.0890
  -8.250  -0.4916   0.02601   0.01636  -0.0669   0.8998   0.0964
  -8.000  -0.4667   0.02526   0.01564  -0.0670   0.8885   0.1052
  -7.750  -0.4332   0.02444   0.01482  -0.0687   0.8804   0.1186
  -7.500  -0.4084   0.02385   0.01426  -0.0686   0.8687   0.1328
  -7.250  -0.3767   0.02319   0.01363  -0.0699   0.8593   0.1498
  -7.000  -0.3546   0.02277   0.01321  -0.0691   0.8468   0.1646
  -6.750  -0.3246   0.02228   0.01270  -0.0699   0.8374   0.1816
  -6.500  -0.3051   0.02197   0.01238  -0.0686   0.8248   0.1954
  -6.250  -0.2764   0.02156   0.01193  -0.0690   0.8156   0.2118
  -6.000  -0.2591   0.02133   0.01168  -0.0671   0.8028   0.2257
  -5.500  -0.2173   0.02070   0.01110  -0.0648   0.7819   0.2578
  -5.250  -0.1928   0.02034   0.01075  -0.0643   0.7735   0.2777
  -5.000  -0.1764   0.02009   0.01057  -0.0622   0.7622   0.2955
  -4.750  -0.1510   0.01973   0.01022  -0.0618   0.7541   0.3153
  -4.500  -0.1328   0.01948   0.01004  -0.0600   0.7439   0.3347
  -4.250  -0.1098   0.01912   0.00977  -0.0591   0.7360   0.3596
  -4.000  -0.0912   0.01881   0.00960  -0.0574   0.7274   0.3918
  -3.750  -0.0727   0.01843   0.00946  -0.0556   0.7191   0.4391
  -3.500  -0.0482   0.01804   0.00938  -0.0548   0.7122   0.5123
  -3.250  -0.0022   0.01813   0.00992  -0.0575   0.7041   0.6068
  -3.000   0.0601   0.01881   0.01075  -0.0625   0.6972   0.6744
  -2.750   0.1005   0.01938   0.01128  -0.0639   0.6900   0.7077
  -2.500   0.1221   0.01965   0.01150  -0.0621   0.6822   0.7339
  -2.250   0.1494   0.01995   0.01168  -0.0614   0.6760   0.7541
  -2.000   0.1696   0.02025   0.01191  -0.0595   0.6690   0.7723
  -1.750   0.2024   0.02076   0.01235  -0.0597   0.6617   0.7842
  -1.500   0.2307   0.02109   0.01254  -0.0592   0.6558   0.7970
  -1.250   0.2494   0.02137   0.01277  -0.0571   0.6491   0.8114
  -1.000   0.2858   0.02182   0.01314  -0.0582   0.6419   0.8197
  -0.750   0.3120   0.02209   0.01329  -0.0575   0.6361   0.8316
  -0.500   0.3429   0.02251   0.01365  -0.0577   0.6296   0.8429
  -0.250   0.3775   0.02292   0.01402  -0.0585   0.6224   0.8525
   0.250   0.4465   0.02354   0.01447  -0.0604   0.6104   0.8716
   0.500   0.4646   0.02382   0.01476  -0.0585   0.6037   0.8835
   0.750   0.5063   0.02394   0.01480  -0.0611   0.5973   0.8880
   1.000   0.5380   0.02401   0.01477  -0.0619   0.5921   0.8936
   1.250   0.5512   0.02418   0.01498  -0.0593   0.5853   0.9016
   1.500   0.5851   0.02421   0.01498  -0.0606   0.5790   0.9050
   1.750   0.6166   0.02422   0.01490  -0.0615   0.5737   0.9093
   2.000   0.6310   0.02441   0.01512  -0.0591   0.5676   0.9167
   2.250   0.6590   0.02446   0.01518  -0.0594   0.5610   0.9206
   2.500   0.6911   0.02445   0.01512  -0.0604   0.5553   0.9241
   2.750   0.7164   0.02454   0.01519  -0.0602   0.5495   0.9289
   3.000   0.7298   0.02476   0.01546  -0.0577   0.5430   0.9353
   3.250   0.7619   0.02472   0.01540  -0.0588   0.5369   0.9381
   3.500   0.7925   0.02472   0.01534  -0.0595   0.5316   0.9415
   3.750   0.8114   0.02492   0.01564  -0.0582   0.5245   0.9466
   4.000   0.8293   0.02507   0.01579  -0.0566   0.5185   0.9515
   4.250   0.8626   0.02499   0.01565  -0.0578   0.5134   0.9539
   4.500   0.8845   0.02517   0.01594  -0.0572   0.5058   0.9579
   4.750   0.9066   0.02527   0.01606  -0.0564   0.4994   0.9618
   5.000   0.9286   0.02534   0.01606  -0.0555   0.4939   0.9659
   5.250   0.9512   0.02547   0.01631  -0.0550   0.4849   0.9692
   5.500   0.9768   0.02540   0.01620  -0.0548   0.4770   0.9721
   5.750   0.9942   0.02556   0.01644  -0.0533   0.4674   0.9764
   6.000   1.0143   0.02559   0.01641  -0.0520   0.4584   0.9802
   6.250   1.0344   0.02566   0.01655  -0.0511   0.4475   0.9832
   6.500   1.0578   0.02564   0.01648  -0.0506   0.4390   0.9862
   6.750   1.0751   0.02591   0.01685  -0.0493   0.4297   0.9902
   7.000   1.0969   0.02602   0.01696  -0.0486   0.4224   0.9931
   7.250   1.1157   0.02624   0.01724  -0.0476   0.4141   0.9961
   7.500   1.1362   0.02641   0.01745  -0.0468   0.4060   0.9991
   7.750   1.1464   0.02671   0.01777  -0.0440   0.3990   1.0000
   8.000   1.1467   0.02711   0.01823  -0.0395   0.3919   1.0000
   8.250   1.1485   0.02739   0.01848  -0.0350   0.3858   1.0000
   8.500   1.1417   0.02783   0.01899  -0.0293   0.3795   1.0000
   8.750   1.1363   0.02828   0.01948  -0.0239   0.3729   1.0000
   9.000   1.1379   0.02862   0.01977  -0.0197   0.3669   1.0000
   9.250   1.1285   0.02933   0.02058  -0.0141   0.3599   1.0000
   9.500   1.1253   0.02990   0.02117  -0.0096   0.3531   1.0000
   9.750   1.1227   0.03054   0.02181  -0.0052   0.3463   1.0000
  10.000   1.1150   0.03142   0.02275  -0.0005   0.3388   1.0000
  10.250   1.1161   0.03201   0.02329   0.0031   0.3319   1.0000
  10.500   1.1058   0.03319   0.02457   0.0076   0.3240   1.0000
  10.750   1.1028   0.03408   0.02542   0.0113   0.3163   1.0000
  11.000   1.0951   0.03534   0.02674   0.0152   0.3081   1.0000
  11.250   1.0902   0.03648   0.02786   0.0187   0.2996   1.0000
  11.500   1.0829   0.03792   0.02933   0.0221   0.2912   1.0000
  11.750   1.0773   0.03930   0.03070   0.0252   0.2823   1.0000
  12.000   1.0696   0.04098   0.03243   0.0282   0.2735   1.0000
  12.250   1.0647   0.04251   0.03392   0.0309   0.2647   1.0000
  12.500   1.0575   0.04442   0.03589   0.0333   0.2562   1.0000
  12.750   1.0546   0.04601   0.03744   0.0355   0.2483   1.0000
  13.000   1.0483   0.04806   0.03954   0.0376   0.2402   1.0000
  13.250   1.0458   0.04980   0.04124   0.0394   0.2326   1.0000
  13.500   1.0425   0.05178   0.04327   0.0410   0.2256   1.0000
  13.750   1.0404   0.05370   0.04519   0.0425   0.2190   1.0000
  14.000   1.0393   0.05556   0.04703   0.0439   0.2126   1.0000
  14.250   1.0360   0.05779   0.04930   0.0451   0.2063   1.0000
  14.500   1.0372   0.05950   0.05094   0.0463   0.2005   1.0000
  14.750   1.0342   0.06187   0.05339   0.0473   0.1950   1.0000
  15.000   1.0327   0.06407   0.05562   0.0481   0.1896   1.0000
  15.250   1.0371   0.06558   0.05705   0.0491   0.1851   1.0000
  15.500   1.0318   0.06842   0.06002   0.0496   0.1799   1.0000
  15.750   1.0312   0.07070   0.06232   0.0502   0.1753   1.0000
  16.000   1.0365   0.07220   0.06375   0.0509   0.1710   1.0000
  16.250   1.0313   0.07524   0.06692   0.0512   0.1667   1.0000
  16.500   1.0289   0.07792   0.06968   0.0514   0.1625   1.0000
  16.750   1.0344   0.07953   0.07125   0.0519   0.1587   1.0000
  17.000   1.0309   0.08248   0.07428   0.0519   0.1547   1.0000
  17.250   1.0250   0.08580   0.07772   0.0517   0.1505   1.0000
  17.500   1.0267   0.08803   0.07994   0.0518   0.1465   1.0000
  17.750   1.0265   0.09060   0.08254   0.0518   0.1428   1.0000
  18.000   1.0148   0.09495   0.08704   0.0510   0.1383   1.0000
  18.250   1.0141   0.09764   0.08977   0.0507   0.1343   1.0000
  18.500   1.0134   0.10038   0.09252   0.0504   0.1303   1.0000
  18.750   0.9980   0.10551   0.09782   0.0491   0.1258   1.0000
  19.000   0.9979   0.10822   0.10053   0.0486   0.1217   1.0000
  19.250   0.9917   0.11198   0.10436   0.0476   0.1177   1.0000
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