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GOE 619 AIRFOIL (goe619-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 619 AIRFOIL (goe619-il)
Reynolds number: 200,000
Max Cl/Cd: 67.57 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe619-il-200000-n5.txt
Download as CSV file: xf-goe619-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 619 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.6232   0.06292   0.05861  -0.0752   1.0000   0.0364
 -12.000  -0.6794   0.05360   0.04917  -0.0803   1.0000   0.0361
 -11.750  -0.7267   0.04650   0.04196  -0.0847   0.9992   0.0360
 -11.500  -0.7247   0.03987   0.03488  -0.0953   0.9873   0.0362
 -11.250  -0.7103   0.03638   0.03104  -0.0994   0.9791   0.0366
 -11.000  -0.6909   0.03379   0.02812  -0.1022   0.9722   0.0370
 -10.750  -0.6726   0.03177   0.02598  -0.1031   0.9646   0.0377
 -10.500  -0.6472   0.03015   0.02428  -0.1047   0.9595   0.0383
 -10.250  -0.6249   0.02876   0.02278  -0.1053   0.9526   0.0388
 -10.000  -0.5993   0.02739   0.02127  -0.1064   0.9469   0.0394
  -9.750  -0.5693   0.02603   0.01975  -0.1081   0.9434   0.0400
  -9.500  -0.5476   0.02492   0.01851  -0.1079   0.9348   0.0406
  -9.250  -0.5172   0.02377   0.01721  -0.1093   0.9304   0.0413
  -9.000  -0.4885   0.02276   0.01604  -0.1103   0.9250   0.0421
  -8.750  -0.4616   0.02187   0.01499  -0.1106   0.9179   0.0430
  -8.500  -0.4298   0.02089   0.01392  -0.1120   0.9133   0.0440
  -8.250  -0.4032   0.02010   0.01308  -0.1123   0.9059   0.0449
  -8.000  -0.3736   0.01937   0.01226  -0.1130   0.8996   0.0460
  -7.750  -0.3406   0.01865   0.01144  -0.1143   0.8948   0.0472
  -7.500  -0.3154   0.01809   0.01079  -0.1140   0.8858   0.0485
  -7.250  -0.2837   0.01749   0.01007  -0.1149   0.8798   0.0501
  -7.000  -0.2578   0.01697   0.00951  -0.1146   0.8714   0.0519
  -6.750  -0.2284   0.01649   0.00898  -0.1150   0.8644   0.0549
  -6.500  -0.2008   0.01607   0.00851  -0.1150   0.8568   0.0590
  -6.250  -0.1730   0.01571   0.00812  -0.1150   0.8487   0.0652
  -6.000  -0.1446   0.01540   0.00777  -0.1150   0.8415   0.0729
  -5.750  -0.1178   0.01514   0.00746  -0.1147   0.8334   0.0807
  -5.500  -0.0883   0.01493   0.00713  -0.1149   0.8267   0.0882
  -5.250  -0.0630   0.01470   0.00687  -0.1143   0.8180   0.0941
  -5.000  -0.0341   0.01451   0.00657  -0.1143   0.8113   0.1001
  -4.750  -0.0084   0.01432   0.00633  -0.1138   0.8031   0.1049
  -4.500   0.0190   0.01410   0.00607  -0.1136   0.7959   0.1113
  -4.250   0.0456   0.01396   0.00585  -0.1132   0.7884   0.1172
  -4.000   0.0721   0.01374   0.00562  -0.1128   0.7809   0.1230
  -3.750   0.0992   0.01357   0.00541  -0.1125   0.7741   0.1297
  -3.500   0.1252   0.01340   0.00523  -0.1120   0.7662   0.1364
  -3.250   0.1530   0.01324   0.00503  -0.1119   0.7599   0.1456
  -3.000   0.1782   0.01308   0.00493  -0.1112   0.7517   0.1569
  -2.750   0.2055   0.01294   0.00479  -0.1110   0.7448   0.1721
  -2.500   0.2314   0.01283   0.00472  -0.1104   0.7369   0.1890
  -2.250   0.2582   0.01275   0.00462  -0.1100   0.7293   0.2069
  -2.000   0.2844   0.01269   0.00456  -0.1095   0.7210   0.2238
  -1.750   0.3110   0.01263   0.00447  -0.1090   0.7118   0.2394
  -1.500   0.3364   0.01258   0.00441  -0.1083   0.7009   0.2527
  -1.250   0.3623   0.01255   0.00431  -0.1076   0.6889   0.2649
  -1.000   0.3880   0.01253   0.00423  -0.1069   0.6772   0.2768
  -0.750   0.4132   0.01249   0.00420  -0.1062   0.6662   0.2877
  -0.500   0.4394   0.01249   0.00415  -0.1056   0.6576   0.2994
  -0.250   0.4650   0.01248   0.00415  -0.1050   0.6486   0.3120
   0.000   0.4908   0.01247   0.00415  -0.1044   0.6402   0.3258
   0.250   0.5161   0.01245   0.00416  -0.1037   0.6306   0.3405
   0.500   0.5415   0.01245   0.00418  -0.1030   0.6216   0.3567
   0.750   0.5666   0.01244   0.00421  -0.1023   0.6122   0.3762
   1.000   0.5915   0.01244   0.00426  -0.1016   0.6029   0.3979
   1.500   0.6403   0.01243   0.00435  -0.0999   0.5814   0.4441
   1.750   0.6642   0.01243   0.00439  -0.0989   0.5693   0.4702
   2.000   0.6872   0.01240   0.00443  -0.0978   0.5564   0.5021
   2.250   0.7087   0.01231   0.00448  -0.0965   0.5422   0.5520
   2.500   0.7712   0.01167   0.00473  -0.1032   0.5214   1.0000
   2.750   0.7923   0.01186   0.00480  -0.1018   0.5040   1.0000
   3.000   0.8129   0.01207   0.00489  -0.1002   0.4850   1.0000
   3.250   0.8325   0.01232   0.00501  -0.0985   0.4647   1.0000
   3.500   0.8512   0.01262   0.00515  -0.0966   0.4439   1.0000
   3.750   0.8700   0.01293   0.00533  -0.0948   0.4228   1.0000
   4.000   0.8882   0.01327   0.00554  -0.0929   0.4026   1.0000
   4.250   0.9064   0.01363   0.00577  -0.0910   0.3845   1.0000
   4.500   0.9246   0.01398   0.00602  -0.0892   0.3683   1.0000
   4.750   0.9424   0.01436   0.00629  -0.0873   0.3527   1.0000
   5.000   0.9600   0.01474   0.00658  -0.0854   0.3382   1.0000
   5.250   0.9771   0.01514   0.00688  -0.0835   0.3248   1.0000
   5.500   0.9931   0.01556   0.00720  -0.0814   0.3115   1.0000
   5.750   1.0100   0.01592   0.00752  -0.0794   0.3008   1.0000
   6.000   1.0262   0.01631   0.00784  -0.0773   0.2915   1.0000
   6.250   1.0429   0.01669   0.00819  -0.0753   0.2837   1.0000
   6.500   1.0598   0.01709   0.00856  -0.0734   0.2775   1.0000
   6.750   1.0778   0.01745   0.00893  -0.0718   0.2711   1.0000
   7.000   1.0945   0.01788   0.00933  -0.0699   0.2658   1.0000
   7.250   1.1118   0.01830   0.00974  -0.0682   0.2607   1.0000
   7.500   1.1299   0.01869   0.01016  -0.0667   0.2556   1.0000
   7.750   1.1458   0.01917   0.01062  -0.0649   0.2499   1.0000
   8.000   1.1621   0.01965   0.01110  -0.0632   0.2444   1.0000
   8.250   1.1794   0.02010   0.01157  -0.0617   0.2388   1.0000
   8.500   1.1951   0.02062   0.01211  -0.0600   0.2338   1.0000
   8.750   1.2102   0.02119   0.01267  -0.0583   0.2301   1.0000
   9.000   1.2283   0.02165   0.01320  -0.0570   0.2264   1.0000
   9.250   1.2447   0.02218   0.01378  -0.0555   0.2219   1.0000
   9.500   1.2580   0.02284   0.01445  -0.0537   0.2163   1.0000
   9.750   1.2730   0.02345   0.01510  -0.0522   0.2103   1.0000
  10.000   1.2866   0.02414   0.01581  -0.0506   0.2029   1.0000
  10.250   1.2991   0.02490   0.01658  -0.0490   0.1958   1.0000
  10.500   1.3128   0.02563   0.01736  -0.0475   0.1881   1.0000
  10.750   1.3248   0.02649   0.01824  -0.0460   0.1806   1.0000
  11.000   1.3357   0.02743   0.01919  -0.0444   0.1699   1.0000
  11.250   1.3463   0.02844   0.02020  -0.0429   0.1571   1.0000
  11.500   1.3531   0.02974   0.02145  -0.0413   0.1397   1.0000
  11.750   1.3567   0.03134   0.02295  -0.0395   0.1204   1.0000
  12.000   1.3528   0.03361   0.02506  -0.0375   0.0954   1.0000
  12.250   1.3511   0.03582   0.02718  -0.0358   0.0808   1.0000
  12.500   1.3531   0.03781   0.02917  -0.0344   0.0737   1.0000
  12.750   1.3558   0.03979   0.03118  -0.0332   0.0692   1.0000
  13.000   1.3594   0.04175   0.03320  -0.0322   0.0661   1.0000
  13.250   1.3614   0.04393   0.03544  -0.0313   0.0631   1.0000
  13.500   1.3623   0.04630   0.03787  -0.0305   0.0604   1.0000
  13.750   1.3662   0.04843   0.04011  -0.0299   0.0585   1.0000
  14.000   1.3683   0.05081   0.04258  -0.0295   0.0563   1.0000
  14.250   1.3678   0.05355   0.04540  -0.0291   0.0542   1.0000
  14.500   1.3673   0.05639   0.04833  -0.0289   0.0528   1.0000
  14.750   1.3646   0.05958   0.05161  -0.0289   0.0512   1.0000
  15.000   1.3672   0.06222   0.05437  -0.0289   0.0497   1.0000
  15.250   1.3679   0.06516   0.05744  -0.0291   0.0482   1.0000
  15.500   1.3663   0.06847   0.06087  -0.0295   0.0462   1.0000
  15.750   1.3601   0.07250   0.06499  -0.0302   0.0440   1.0000
  16.000   1.3578   0.07610   0.06871  -0.0309   0.0420   1.0000
  16.250   1.3558   0.07974   0.07247  -0.0317   0.0388   1.0000
  16.500   1.3512   0.08385   0.07670  -0.0327   0.0341   1.0000
  16.750   1.3345   0.08993   0.08280  -0.0347   0.0208   1.0000
  17.000   1.3176   0.09623   0.08916  -0.0369   0.0195   1.0000
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