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GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 735 AIRFOIL (goe735-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.03 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe735-il-1000000.txt
Download as CSV file: xf-goe735-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 735 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
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.0682   0.08044   0.07711  -0.0500   1.0000   0.0330
 -19.250  -1.1202   0.06978   0.06627  -0.0564   1.0000   0.0329
 -19.000  -1.1627   0.06025   0.05656  -0.0624   1.0000   0.0330
 -18.750  -1.1910   0.05261   0.04875  -0.0675   1.0000   0.0332
 -18.500  -1.2100   0.04655   0.04254  -0.0715   1.0000   0.0333
 -18.250  -1.2185   0.04224   0.03812  -0.0740   1.0000   0.0336
 -18.000  -1.2241   0.03863   0.03440  -0.0758   1.0000   0.0339
 -17.750  -1.2260   0.03574   0.03142  -0.0767   1.0000   0.0343
 -17.500  -1.2244   0.03342   0.02902  -0.0770   1.0000   0.0346
 -17.250  -1.2214   0.03144   0.02696  -0.0769   1.0000   0.0349
 -17.000  -1.1959   0.02971   0.02513  -0.0800   0.9468   0.0354
 -16.750  -1.1784   0.02758   0.02266  -0.0829   0.8602   0.0362
 -16.500  -1.1799   0.02629   0.02121  -0.0806   0.8323   0.0365
 -16.250  -1.1780   0.02515   0.01996  -0.0784   0.8153   0.0372
 -16.000  -1.1732   0.02420   0.01891  -0.0762   0.8026   0.0377
 -15.750  -1.1668   0.02331   0.01793  -0.0741   0.7920   0.0382
 -15.500  -1.1573   0.02261   0.01714  -0.0720   0.7830   0.0389
 -15.250  -1.1471   0.02192   0.01638  -0.0700   0.7748   0.0394
 -15.000  -1.1380   0.02124   0.01560  -0.0677   0.7670   0.0400
 -14.750  -1.1307   0.02045   0.01478  -0.0651   0.7605   0.0410
 -14.500  -1.1199   0.01982   0.01411  -0.0628   0.7538   0.0418
 -14.250  -1.1074   0.01931   0.01352  -0.0606   0.7468   0.0427
 -14.000  -1.0929   0.01883   0.01299  -0.0586   0.7414   0.0437
 -13.750  -1.0783   0.01836   0.01247  -0.0565   0.7356   0.0446
 -13.500  -1.0658   0.01781   0.01189  -0.0541   0.7297   0.0460
 -13.250  -1.0507   0.01737   0.01141  -0.0520   0.7235   0.0473
 -13.000  -1.0335   0.01699   0.01099  -0.0502   0.7184   0.0487
 -12.750  -1.0174   0.01657   0.01054  -0.0482   0.7125   0.0502
 -12.500  -1.0006   0.01618   0.01012  -0.0462   0.7066   0.0521
 -12.250  -0.9818   0.01587   0.00977  -0.0445   0.7013   0.0540
 -12.000  -0.9638   0.01551   0.00940  -0.0426   0.6954   0.0560
 -11.750  -0.9451   0.01520   0.00907  -0.0409   0.6890   0.0580
 -11.500  -0.9249   0.01499   0.00881  -0.0393   0.6829   0.0600
 -11.250  -0.9055   0.01470   0.00852  -0.0376   0.6775   0.0620
 -11.000  -0.8849   0.01447   0.00827  -0.0361   0.6707   0.0641
 -10.750  -0.8621   0.01431   0.00805  -0.0349   0.6633   0.0661
 -10.500  -0.8394   0.01405   0.00778  -0.0338   0.6571   0.0681
 -10.250  -0.8163   0.01383   0.00755  -0.0327   0.6496   0.0702
 -10.000  -0.7923   0.01367   0.00734  -0.0318   0.6419   0.0720
  -9.750  -0.7672   0.01353   0.00716  -0.0310   0.6339   0.0735
  -9.500  -0.7446   0.01327   0.00686  -0.0299   0.6249   0.0755
  -9.250  -0.7202   0.01308   0.00667  -0.0290   0.6163   0.0773
  -9.000  -0.6953   0.01294   0.00648  -0.0282   0.6067   0.0790
  -8.750  -0.6696   0.01283   0.00632  -0.0275   0.5976   0.0805
  -8.500  -0.6450   0.01266   0.00609  -0.0267   0.5872   0.0822
  -8.250  -0.6208   0.01246   0.00587  -0.0258   0.5776   0.0841
  -8.000  -0.5955   0.01233   0.00571  -0.0251   0.5673   0.0858
  -7.750  -0.5697   0.01222   0.00556  -0.0245   0.5587   0.0874
  -7.500  -0.5436   0.01213   0.00541  -0.0239   0.5496   0.0887
  -7.250  -0.5182   0.01200   0.00522  -0.0232   0.5412   0.0904
  -7.000  -0.4933   0.01180   0.00502  -0.0224   0.5329   0.0926
  -6.750  -0.4677   0.01170   0.00488  -0.0218   0.5242   0.0943
  -6.500  -0.4412   0.01159   0.00475  -0.0213   0.5181   0.0960
  -6.250  -0.4146   0.01152   0.00463  -0.0208   0.5110   0.0975
  -6.000  -0.3883   0.01144   0.00450  -0.0202   0.5039   0.0991
  -5.750  -0.3628   0.01125   0.00433  -0.0196   0.4982   0.1023
  -5.500  -0.3363   0.01116   0.00423  -0.0191   0.4916   0.1046
  -5.250  -0.3098   0.01111   0.00412  -0.0186   0.4849   0.1065
  -5.000  -0.2825   0.01102   0.00402  -0.0182   0.4802   0.1080
  -4.750  -0.2566   0.01088   0.00386  -0.0177   0.4748   0.1106
  -4.500  -0.2307   0.01077   0.00374  -0.0171   0.4690   0.1133
  -4.250  -0.2039   0.01069   0.00365  -0.0167   0.4641   0.1157
  -4.000  -0.1766   0.01062   0.00356  -0.0163   0.4594   0.1181
  -3.750  -0.1496   0.01056   0.00347  -0.0159   0.4541   0.1203
  -3.500  -0.1239   0.01047   0.00336  -0.0153   0.4483   0.1242
  -3.250  -0.0968   0.01038   0.00329  -0.0150   0.4448   0.1277
  -3.000  -0.0694   0.01032   0.00323  -0.0147   0.4408   0.1308
  -2.750  -0.0428   0.01024   0.00314  -0.0142   0.4364   0.1356
  -2.500  -0.0164   0.01019   0.00309  -0.0138   0.4315   0.1406
  -2.250   0.0108   0.01017   0.00305  -0.0135   0.4271   0.1447
  -2.000   0.0376   0.01006   0.00298  -0.0131   0.4237   0.1522
  -1.750   0.0646   0.01001   0.00293  -0.0128   0.4196   0.1589
  -1.500   0.0908   0.00994   0.00289  -0.0123   0.4156   0.1694
  -1.250   0.1168   0.00991   0.00287  -0.0118   0.4108   0.1813
  -1.000   0.1432   0.00980   0.00284  -0.0114   0.4081   0.1982
  -0.750   0.1691   0.00967   0.00281  -0.0109   0.4051   0.2237
  -0.500   0.1942   0.00952   0.00278  -0.0103   0.4015   0.2589
  -0.250   0.2188   0.00940   0.00278  -0.0096   0.3976   0.2994
   0.000   0.2430   0.00931   0.00279  -0.0089   0.3930   0.3390
   0.250   0.2678   0.00918   0.00280  -0.0082   0.3903   0.3806
   0.500   0.2917   0.00898   0.00278  -0.0073   0.3878   0.4339
   0.750   0.3110   0.00864   0.00278  -0.0057   0.3849   0.5312
   1.000   0.3294   0.00836   0.00278  -0.0037   0.3819   0.6216
   1.250   0.3450   0.00810   0.00281  -0.0011   0.3787   0.7117
   1.500   0.3615   0.00795   0.00290   0.0014   0.3749   0.7906
   1.750   0.3855   0.00787   0.00299   0.0025   0.3725   0.8417
   2.000   0.4152   0.00786   0.00309   0.0023   0.3700   0.8776
   2.250   0.4490   0.00794   0.00321   0.0013   0.3668   0.8996
   2.500   0.4830   0.00806   0.00333   0.0001   0.3634   0.9160
   2.750   0.5162   0.00824   0.00348  -0.0010   0.3598   0.9283
   3.000   0.5549   0.00846   0.00367  -0.0032   0.3560   0.9363
   3.250   0.5839   0.00858   0.00380  -0.0033   0.3542   0.9457
   3.500   0.6243   0.00876   0.00397  -0.0058   0.3517   0.9507
   3.750   0.6695   0.00902   0.00421  -0.0092   0.3485   0.9545
   4.000   0.7066   0.00930   0.00444  -0.0111   0.3452   0.9591
   4.250   0.7349   0.00956   0.00466  -0.0112   0.3416   0.9645
   4.500   0.7745   0.00979   0.00486  -0.0137   0.3385   0.9656
   4.750   0.8140   0.00994   0.00501  -0.0161   0.3367   0.9668
   5.000   0.8542   0.01011   0.00518  -0.0186   0.3343   0.9685
   5.250   0.8930   0.01031   0.00536  -0.0210   0.3315   0.9707
   5.500   0.9266   0.01051   0.00553  -0.0223   0.3285   0.9736
   5.750   0.9490   0.01077   0.00576  -0.0214   0.3256   0.9785
   6.000   0.9853   0.01099   0.00595  -0.0234   0.3222   0.9795
   6.250   1.0227   0.01109   0.00606  -0.0256   0.3204   0.9804
   6.500   1.0586   0.01120   0.00618  -0.0274   0.3181   0.9816
   6.750   1.0929   0.01134   0.00632  -0.0290   0.3153   0.9829
   7.000   1.1255   0.01151   0.00647  -0.0303   0.3126   0.9845
   7.250   1.1564   0.01174   0.00667  -0.0313   0.3095   0.9866
   7.500   1.1841   0.01205   0.00695  -0.0318   0.3061   0.9891
   7.750   1.2102   0.01222   0.00715  -0.0318   0.3048   0.9917
   8.000   1.2443   0.01231   0.00726  -0.0334   0.3029   0.9925
   8.250   1.2780   0.01243   0.00740  -0.0350   0.3007   0.9936
   8.500   1.3106   0.01259   0.00757  -0.0365   0.2983   0.9950
   8.750   1.3419   0.01280   0.00777  -0.0377   0.2959   0.9966
   9.000   1.3717   0.01306   0.00802  -0.0388   0.2931   0.9983
   9.250   1.4005   0.01341   0.00834  -0.0398   0.2899   0.9997
   9.500   1.4202   0.01356   0.00855  -0.0387   0.2886   1.0000
   9.750   1.4322   0.01376   0.00878  -0.0362   0.2870   1.0000
  10.000   1.4354   0.01398   0.00903  -0.0321   0.2855   1.0000
  10.250   1.4294   0.01426   0.00935  -0.0266   0.2839   1.0000
  10.500   1.4283   0.01469   0.00981  -0.0224   0.2821   1.0000
  10.750   1.4306   0.01523   0.01037  -0.0189   0.2802   1.0000
  11.000   1.4340   0.01588   0.01102  -0.0159   0.2780   1.0000
  11.250   1.4370   0.01666   0.01181  -0.0131   0.2753   1.0000
  11.500   1.4465   0.01728   0.01245  -0.0112   0.2736   1.0000
  11.750   1.4592   0.01781   0.01304  -0.0097   0.2722   1.0000
  12.000   1.4713   0.01841   0.01368  -0.0083   0.2705   1.0000
  12.250   1.4830   0.01907   0.01437  -0.0069   0.2684   1.0000
  12.500   1.4931   0.01986   0.01518  -0.0055   0.2658   1.0000
  12.750   1.5012   0.02080   0.01614  -0.0040   0.2635   1.0000
  13.000   1.5047   0.02205   0.01737  -0.0023   0.2597   1.0000
  13.250   1.5172   0.02284   0.01821  -0.0013   0.2575   1.0000
  13.500   1.5297   0.02365   0.01907  -0.0005   0.2552   1.0000
  13.750   1.5398   0.02463   0.02008   0.0005   0.2523   1.0000
  14.000   1.5453   0.02596   0.02142   0.0016   0.2488   1.0000
  14.250   1.5482   0.02748   0.02295   0.0028   0.2457   1.0000
  14.500   1.5562   0.02872   0.02423   0.0036   0.2423   1.0000
  14.750   1.5662   0.02984   0.02540   0.0042   0.2400   1.0000
  15.000   1.5715   0.03138   0.02697   0.0049   0.2359   1.0000
  15.250   1.5704   0.03351   0.02910   0.0057   0.2318   1.0000
  15.500   1.5735   0.03534   0.03096   0.0063   0.2286   1.0000
  15.750   1.5819   0.03679   0.03247   0.0066   0.2255   1.0000
  16.000   1.5855   0.03869   0.03441   0.0070   0.2224   1.0000
  16.250   1.5800   0.04143   0.03716   0.0074   0.2177   1.0000
  16.500   1.5802   0.04373   0.03949   0.0077   0.2138   1.0000
  16.750   1.5826   0.04587   0.04169   0.0079   0.2105   1.0000
  17.000   1.5790   0.04860   0.04445   0.0080   0.2064   1.0000
  17.250   1.5685   0.05203   0.04789   0.0082   0.2021   1.0000
  17.500   1.5693   0.05443   0.05035   0.0081   0.1995   1.0000
  17.750   1.5664   0.05723   0.05319   0.0080   0.1954   1.0000
  18.000   1.5572   0.06069   0.05667   0.0079   0.1914   1.0000
  18.250   1.5453   0.06452   0.06054   0.0077   0.1876   1.0000
  18.500   1.5433   0.06734   0.06341   0.0074   0.1838   1.0000
  18.750   1.5374   0.07060   0.06671   0.0070   0.1807   1.0000
  19.000   1.5192   0.07530   0.07142   0.0064   0.1761   1.0000
  19.250   1.5187   0.07804   0.07422   0.0060   0.1736   1.0000
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