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GOE 575 AIRFOIL (goe575-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 575 AIRFOIL (goe575-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.36 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe575-il-1000000-n5.txt
Download as CSV file: xf-goe575-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 575 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -1.2258   0.03671   0.03302  -0.1170   0.9807   0.0198
 -17.250  -1.2341   0.03453   0.03074  -0.1150   0.9799   0.0200
 -17.000  -1.2361   0.03289   0.02899  -0.1127   0.9792   0.0202
 -16.750  -1.2280   0.03175   0.02781  -0.1113   0.9786   0.0209
 -16.500  -1.2233   0.03051   0.02646  -0.1092   0.9780   0.0210
 -16.250  -1.2117   0.02973   0.02562  -0.1075   0.9776   0.0218
 -16.000  -1.2017   0.02886   0.02466  -0.1056   0.9772   0.0221
 -15.750  -1.1895   0.02808   0.02379  -0.1039   0.9769   0.0225
 -15.500  -1.2024   0.02721   0.02285  -0.0967   0.9729   0.0227
 -15.250  -1.1929   0.02656   0.02211  -0.0939   0.9716   0.0230
 -15.000  -1.1843   0.02576   0.02123  -0.0911   0.9705   0.0232
 -14.750  -1.1688   0.02522   0.02065  -0.0893   0.9697   0.0237
 -14.500  -1.1502   0.02480   0.02021  -0.0879   0.9691   0.0243
 -14.250  -1.1330   0.02429   0.01963  -0.0864   0.9685   0.0246
 -14.000  -1.1148   0.02378   0.01906  -0.0849   0.9680   0.0249
 -13.750  -1.0920   0.02347   0.01871  -0.0842   0.9677   0.0256
 -13.500  -1.0999   0.02294   0.01812  -0.0771   0.9629   0.0258
 -13.250  -1.0835   0.02256   0.01767  -0.0750   0.9615   0.0263
 -13.000  -1.0672   0.02207   0.01709  -0.0730   0.9604   0.0265
 -12.750  -1.0476   0.02168   0.01665  -0.0715   0.9596   0.0270
 -12.500  -1.0276   0.02126   0.01619  -0.0702   0.9589   0.0273
 -12.250  -1.0070   0.02084   0.01573  -0.0689   0.9584   0.0275
 -12.000  -0.9830   0.02061   0.01548  -0.0682   0.9580   0.0280
 -11.750  -0.9892   0.02028   0.01510  -0.0610   0.9525   0.0282
 -11.500  -0.9703   0.02000   0.01478  -0.0592   0.9510   0.0286
 -11.250  -0.9496   0.01965   0.01439  -0.0577   0.9500   0.0290
 -11.000  -0.9263   0.01938   0.01408  -0.0568   0.9492   0.0295
 -10.750  -0.9040   0.01894   0.01357  -0.0557   0.9485   0.0298
 -10.500  -0.8779   0.01866   0.01324  -0.0553   0.9479   0.0303
 -10.000  -0.8501   0.01798   0.01246  -0.0493   0.9410   0.0309
  -9.750  -0.8279   0.01752   0.01196  -0.0481   0.9394   0.0311
  -9.500  -0.8016   0.01729   0.01174  -0.0477   0.9384   0.0318
  -9.250  -0.7755   0.01686   0.01127  -0.0473   0.9374   0.0321
  -9.000  -0.7476   0.01666   0.01106  -0.0472   0.9368   0.0326
  -8.750  -0.7195   0.01635   0.01072  -0.0472   0.9362   0.0332
  -8.500  -0.7160   0.01613   0.01046  -0.0418   0.9301   0.0333
  -8.250  -0.6918   0.01583   0.01013  -0.0409   0.9281   0.0337
  -8.000  -0.6656   0.01544   0.00970  -0.0404   0.9266   0.0340
  -7.750  -0.6373   0.01514   0.00937  -0.0404   0.9255   0.0345
  -7.500  -0.6084   0.01482   0.00902  -0.0405   0.9245   0.0348
  -7.250  -0.5792   0.01447   0.00864  -0.0406   0.9236   0.0350
  -7.000  -0.5698   0.01428   0.00842  -0.0364   0.9175   0.0352
  -6.750  -0.5452   0.01391   0.00804  -0.0356   0.9149   0.0359
  -6.500  -0.5177   0.01352   0.00763  -0.0353   0.9127   0.0361
  -6.250  -0.4895   0.01321   0.00731  -0.0352   0.9111   0.0366
  -6.000  -0.4591   0.01288   0.00698  -0.0356   0.9096   0.0371
  -5.750  -0.4446   0.01276   0.00684  -0.0325   0.9028   0.0375
  -5.500  -0.4163   0.01244   0.00650  -0.0323   0.8978   0.0381
  -5.250  -0.3820   0.01209   0.00614  -0.0335   0.8952   0.0388
  -5.000  -0.3551   0.01181   0.00583  -0.0331   0.8852   0.0390
  -4.750  -0.3149   0.01142   0.00541  -0.0356   0.8791   0.0396
  -4.500  -0.2754   0.01110   0.00507  -0.0381   0.8699   0.0400
  -4.250  -0.2235   0.01057   0.00451  -0.0433   0.8595   0.0408
  -4.000  -0.1605   0.01011   0.00396  -0.0511   0.8268   0.0418
  -3.750  -0.1267   0.01007   0.00367  -0.0523   0.7665   0.0424
  -3.250  -0.0989   0.01032   0.00357  -0.0457   0.6919   0.0438
  -3.000  -0.0771   0.01029   0.00348  -0.0443   0.6767   0.0443
  -2.750  -0.0554   0.01028   0.00339  -0.0428   0.6601   0.0447
  -2.500  -0.0338   0.01028   0.00333  -0.0413   0.6444   0.0454
  -2.250  -0.0103   0.01023   0.00324  -0.0402   0.6300   0.0460
  -2.000   0.0134   0.01017   0.00313  -0.0392   0.6149   0.0470
  -1.750   0.0366   0.01015   0.00306  -0.0380   0.5996   0.0480
  -1.500   0.0591   0.01015   0.00301  -0.0367   0.5834   0.0489
  -1.250   0.0814   0.01016   0.00296  -0.0354   0.5655   0.0502
  -1.000   0.1044   0.01018   0.00291  -0.0342   0.5507   0.0513
  -0.750   0.1271   0.01021   0.00288  -0.0330   0.5330   0.0519
  -0.500   0.1506   0.01022   0.00284  -0.0320   0.5175   0.0537
  -0.250   0.1749   0.01022   0.00281  -0.0311   0.5023   0.0561
   0.250   0.2213   0.01033   0.00278  -0.0291   0.4586   0.0663
   0.500   0.2470   0.01028   0.00280  -0.0287   0.4389   0.1070
   0.750   0.2712   0.01032   0.00282  -0.0279   0.4239   0.1174
   1.000   0.2946   0.01041   0.00285  -0.0269   0.4053   0.1246
   1.250   0.3190   0.01045   0.00289  -0.0261   0.3927   0.1353
   1.500   0.3433   0.01050   0.00294  -0.0254   0.3781   0.1488
   1.750   0.3679   0.01054   0.00299  -0.0247   0.3670   0.1677
   2.250   0.4162   0.01066   0.00310  -0.0231   0.3450   0.1911
   2.500   0.4404   0.01072   0.00317  -0.0223   0.3377   0.2039
   2.750   0.4654   0.01075   0.00323  -0.0217   0.3307   0.2222
   3.000   0.4907   0.01077   0.00331  -0.0213   0.3223   0.2534
   3.250   0.5375   0.00980   0.00358  -0.0264   0.3106   0.6918
   3.750   0.7274   0.01170   0.00605  -0.0567   0.2840   0.9710
   4.000   0.7463   0.01195   0.00629  -0.0546   0.2782   0.9737
   4.250   0.8005   0.01221   0.00645  -0.0607   0.2651   0.9758
   4.500   0.8388   0.01239   0.00660  -0.0631   0.2569   0.9779
   4.750   0.8635   0.01257   0.00672  -0.0626   0.2470   0.9788
   5.000   0.8901   0.01314   0.00719  -0.0624   0.2299   0.9840
   5.250   0.9195   0.01324   0.00724  -0.0630   0.2194   0.9844
   5.500   0.9584   0.01339   0.00728  -0.0657   0.2011   0.9858
   5.750   0.9853   0.01369   0.00745  -0.0658   0.1802   0.9868
   6.000   1.0130   0.01386   0.00759  -0.0660   0.1736   0.9878
   6.250   1.0465   0.01406   0.00775  -0.0675   0.1660   0.9904
   6.500   1.0572   0.01426   0.00792  -0.0639   0.1614   0.9889
   6.750   1.0874   0.01450   0.00815  -0.0647   0.1554   0.9914
   7.000   1.1069   0.01470   0.00834  -0.0631   0.1521   0.9917
   7.250   1.1252   0.01495   0.00857  -0.0613   0.1463   0.9921
   7.500   1.1433   0.01522   0.00883  -0.0594   0.1415   0.9924
   8.000   1.1854   0.01573   0.00933  -0.0570   0.1332   0.9939
   8.250   1.2032   0.01601   0.00958  -0.0552   0.1271   0.9940
   8.500   1.2218   0.01623   0.00981  -0.0535   0.1224   0.9941
   8.750   1.2380   0.01659   0.01011  -0.0514   0.1132   0.9941
   9.000   1.2533   0.01696   0.01044  -0.0492   0.1031   0.9942
   9.250   1.2662   0.01746   0.01085  -0.0466   0.0892   0.9943
   9.500   1.2791   0.01797   0.01130  -0.0440   0.0782   0.9944
   9.750   1.2915   0.01850   0.01179  -0.0414   0.0691   0.9945
  10.000   1.3061   0.01889   0.01218  -0.0392   0.0661   0.9946
  10.250   1.3192   0.01936   0.01265  -0.0367   0.0624   0.9947
  10.750   1.3483   0.02016   0.01350  -0.0324   0.0592   0.9948
  11.000   1.3622   0.02062   0.01397  -0.0302   0.0572   0.9950
  11.250   1.3787   0.02106   0.01444  -0.0287   0.0563   0.9953
  11.500   1.3909   0.02160   0.01500  -0.0263   0.0546   0.9954
  11.750   1.4013   0.02219   0.01561  -0.0236   0.0530   0.9954
  12.000   1.4133   0.02271   0.01617  -0.0212   0.0526   0.9954
  12.250   1.4250   0.02323   0.01673  -0.0188   0.0517   0.9953
  12.500   1.4359   0.02381   0.01736  -0.0163   0.0511   0.9953
  12.750   1.4458   0.02444   0.01803  -0.0138   0.0500   0.9952
  13.000   1.4555   0.02510   0.01874  -0.0113   0.0498   0.9952
  13.250   1.4642   0.02582   0.01951  -0.0087   0.0493   0.9951
  13.500   1.4709   0.02667   0.02039  -0.0060   0.0481   0.9950
  13.750   1.4775   0.02756   0.02131  -0.0033   0.0471   0.9949
  14.000   1.4839   0.02847   0.02227  -0.0007   0.0467   0.9948
  14.250   1.4892   0.02945   0.02331   0.0019   0.0461   0.9947
  14.500   1.4941   0.03051   0.02442   0.0045   0.0452   0.9946
  14.750   1.5001   0.03154   0.02551   0.0069   0.0450   0.9945
  15.000   1.5059   0.03262   0.02665   0.0090   0.0443   0.9944
  15.250   1.5111   0.03380   0.02789   0.0112   0.0435   0.9943
  15.500   1.5155   0.03511   0.02925   0.0132   0.0423   0.9942
  15.750   1.5203   0.03662   0.03080   0.0146   0.0411   0.9943
  16.000   1.5273   0.03808   0.03234   0.0157   0.0412   0.9945
  16.250   1.5270   0.03997   0.03426   0.0173   0.0395   0.9944
  16.500   1.5287   0.04174   0.03611   0.0189   0.0394   0.9944
  16.750   1.5292   0.04368   0.03812   0.0203   0.0380   0.9943
  17.000   1.5295   0.04574   0.04024   0.0215   0.0374   0.9942
  17.250   1.5283   0.04798   0.04255   0.0226   0.0359   0.9942
  17.500   1.5264   0.05034   0.04498   0.0235   0.0356   0.9941
  17.750   1.5207   0.05318   0.04787   0.0244   0.0338   0.9941
  18.000   1.5164   0.05592   0.05069   0.0251   0.0327   0.9940
  18.250   1.5089   0.05909   0.05392   0.0256   0.0306   0.9940
  18.500   1.4932   0.06327   0.05813   0.0259   0.0251   0.9939
  18.750   1.4670   0.06882   0.06371   0.0258   0.0198   0.9938
  19.000   1.4369   0.07510   0.07007   0.0252   0.0164   0.9938
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