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GOE 503 AIRFOIL (goe503-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 503 AIRFOIL (goe503-il)
Reynolds number: 1,000,000
Max Cl/Cd: 120.29 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe503-il-1000000.txt
Download as CSV file: xf-goe503-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 503 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.3798   0.10416   0.10215  -0.0828   0.9911   0.0116
 -15.000  -0.4015   0.09506   0.09295  -0.0888   0.9896   0.0115
 -14.750  -0.4279   0.08529   0.08306  -0.0959   0.9879   0.0117
 -14.500  -0.4283   0.07968   0.07738  -0.1011   0.9863   0.0116
 -14.250  -0.4463   0.07157   0.06918  -0.1083   0.9848   0.0117
 -14.000  -0.4543   0.06475   0.06227  -0.1153   0.9835   0.0116
 -13.750  -0.4718   0.05860   0.05606  -0.1202   0.9780   0.0116
 -13.500  -0.5000   0.04887   0.04622  -0.1315   0.9733   0.0116
 -13.250  -0.5752   0.03372   0.03072  -0.1457   0.9594   0.0114
 -13.000  -0.5600   0.02824   0.02500  -0.1509   0.9553   0.0115
 -12.750  -0.5466   0.02542   0.02196  -0.1520   0.9478   0.0117
 -12.500  -0.5263   0.02253   0.01884  -0.1546   0.9431   0.0120
 -12.250  -0.5138   0.02118   0.01737  -0.1532   0.9328   0.0122
 -12.000  -0.4910   0.01986   0.01591  -0.1537   0.9253   0.0124
 -11.750  -0.4703   0.01893   0.01487  -0.1533   0.9148   0.0127
 -11.500  -0.4515   0.01810   0.01391  -0.1523   0.9032   0.0130
 -11.250  -0.4322   0.01731   0.01298  -0.1512   0.8900   0.0133
 -11.000  -0.4132   0.01666   0.01219  -0.1499   0.8758   0.0135
 -10.750  -0.3950   0.01609   0.01147  -0.1483   0.8592   0.0138
 -10.500  -0.3770   0.01562   0.01084  -0.1466   0.8408   0.0141
 -10.250  -0.3590   0.01524   0.01031  -0.1447   0.8218   0.0143
 -10.000  -0.3458   0.01459   0.00947  -0.1421   0.8027   0.0148
  -9.750  -0.3305   0.01403   0.00877  -0.1398   0.7865   0.0153
  -9.500  -0.3121   0.01362   0.00824  -0.1380   0.7732   0.0158
  -9.250  -0.2923   0.01327   0.00778  -0.1365   0.7621   0.0163
  -9.000  -0.2721   0.01296   0.00735  -0.1349   0.7521   0.0169
  -8.750  -0.2502   0.01267   0.00697  -0.1337   0.7431   0.0175
  -8.500  -0.2305   0.01222   0.00641  -0.1322   0.7351   0.0187
  -8.250  -0.2082   0.01186   0.00600  -0.1310   0.7281   0.0200
  -8.000  -0.1856   0.01163   0.00567  -0.1299   0.7212   0.0211
  -7.750  -0.1632   0.01123   0.00525  -0.1288   0.7151   0.0240
  -7.500  -0.1405   0.01091   0.00492  -0.1278   0.7086   0.0294
  -7.250  -0.1173   0.01069   0.00471  -0.1268   0.7024   0.0378
  -7.000  -0.0922   0.01055   0.00456  -0.1262   0.6969   0.0426
  -6.750  -0.0677   0.01045   0.00444  -0.1254   0.6910   0.0463
  -6.500  -0.0427   0.01042   0.00435  -0.1247   0.6853   0.0486
  -6.250  -0.0185   0.01020   0.00414  -0.1239   0.6794   0.0519
  -6.000   0.0057   0.01012   0.00400  -0.1231   0.6732   0.0542
  -5.750   0.0305   0.01005   0.00388  -0.1223   0.6675   0.0559
  -5.500   0.0548   0.00990   0.00370  -0.1215   0.6614   0.0581
  -5.250   0.0779   0.00977   0.00353  -0.1205   0.6549   0.0611
  -5.000   0.1025   0.00965   0.00340  -0.1197   0.6488   0.0637
  -4.750   0.1267   0.00959   0.00329  -0.1189   0.6419   0.0657
  -4.500   0.1497   0.00946   0.00313  -0.1178   0.6355   0.0696
  -4.250   0.1737   0.00934   0.00301  -0.1169   0.6286   0.0731
  -3.750   0.2201   0.00916   0.00280  -0.1148   0.6141   0.0837
  -3.500   0.2427   0.00912   0.00273  -0.1137   0.6065   0.0904
  -3.250   0.2659   0.00903   0.00265  -0.1126   0.5993   0.0988
  -3.000   0.2883   0.00899   0.00258  -0.1114   0.5917   0.1058
  -2.750   0.3110   0.00894   0.00252  -0.1103   0.5849   0.1128
  -2.500   0.3338   0.00892   0.00246  -0.1092   0.5777   0.1181
  -2.250   0.3550   0.00889   0.00242  -0.1077   0.5709   0.1254
  -2.000   0.3773   0.00886   0.00237  -0.1065   0.5645   0.1306
  -1.750   0.3969   0.00884   0.00234  -0.1047   0.5580   0.1394
  -1.500   0.4189   0.00881   0.00231  -0.1035   0.5524   0.1477
  -1.250   0.4404   0.00879   0.00230  -0.1021   0.5467   0.1582
  -1.000   0.4607   0.00881   0.00231  -0.1005   0.5409   0.1682
  -0.750   0.4841   0.00881   0.00231  -0.0995   0.5364   0.1770
  -0.500   0.5063   0.00880   0.00232  -0.0983   0.5314   0.1866
  -0.250   0.5279   0.00887   0.00235  -0.0970   0.5265   0.1940
   0.000   0.5498   0.00887   0.00237  -0.0958   0.5220   0.2033
   0.250   0.5730   0.00890   0.00239  -0.0948   0.5177   0.2097
   0.500   0.5947   0.00894   0.00244  -0.0936   0.5131   0.2184
   0.750   0.6155   0.00903   0.00250  -0.0922   0.5083   0.2257
   1.000   0.6392   0.00903   0.00253  -0.0913   0.5048   0.2337
   1.250   0.6620   0.00907   0.00258  -0.0903   0.5007   0.2409
   1.500   0.6836   0.00913   0.00263  -0.0891   0.4964   0.2479
   1.750   0.7038   0.00923   0.00272  -0.0876   0.4920   0.2568
   2.000   0.7271   0.00924   0.00277  -0.0867   0.4885   0.2671
   2.250   0.7494   0.00928   0.00283  -0.0856   0.4845   0.2796
   2.500   0.7704   0.00933   0.00292  -0.0843   0.4806   0.2982
   2.750   0.7898   0.00941   0.00304  -0.0828   0.4762   0.3240
   3.000   0.8119   0.00940   0.00313  -0.0817   0.4729   0.3565
   3.250   0.8323   0.00939   0.00323  -0.0803   0.4687   0.4028
   3.500   0.8286   0.00865   0.00339  -0.0739   0.4653   0.7673
   3.750   0.9810   0.00880   0.00402  -0.1016   0.4573   0.9832
   4.000   1.0229   0.00899   0.00418  -0.1049   0.4513   0.9887
   4.250   1.0569   0.00923   0.00437  -0.1066   0.4457   0.9933
   4.500   1.0987   0.00939   0.00450  -0.1100   0.4399   0.9967
   4.750   1.1421   0.00957   0.00465  -0.1137   0.4330   0.9991
   5.000   1.1687   0.00976   0.00479  -0.1139   0.4270   1.0000
   5.250   1.1836   0.00984   0.00489  -0.1114   0.4226   1.0000
   5.500   1.1970   0.00997   0.00501  -0.1087   0.4178   1.0000
   5.750   1.2084   0.01016   0.00517  -0.1056   0.4128   1.0000
   6.000   1.2249   0.01028   0.00530  -0.1036   0.4088   1.0000
   6.250   1.2409   0.01043   0.00545  -0.1015   0.4039   1.0000
   6.500   1.2545   0.01066   0.00565  -0.0989   0.3987   1.0000
   6.750   1.2708   0.01084   0.00584  -0.0969   0.3941   1.0000
   7.000   1.2878   0.01104   0.00604  -0.0951   0.3886   1.0000
   7.250   1.3024   0.01131   0.00629  -0.0929   0.3832   1.0000
   7.500   1.3189   0.01155   0.00653  -0.0910   0.3767   1.0000
   7.750   1.3325   0.01190   0.00683  -0.0888   0.3674   1.0000
   8.000   1.3494   0.01218   0.00711  -0.0871   0.3612   1.0000
   8.250   1.3642   0.01254   0.00746  -0.0851   0.3537   1.0000
   8.500   1.3802   0.01289   0.00780  -0.0834   0.3474   1.0000
   8.750   1.3947   0.01331   0.00820  -0.0815   0.3390   1.0000
   9.000   1.4098   0.01373   0.00861  -0.0798   0.3316   1.0000
   9.250   1.4239   0.01421   0.00908  -0.0779   0.3235   1.0000
   9.500   1.4378   0.01473   0.00957  -0.0761   0.3148   1.0000
   9.750   1.4493   0.01536   0.01018  -0.0740   0.3057   1.0000
  10.000   1.4643   0.01587   0.01070  -0.0725   0.2982   1.0000
  10.250   1.4740   0.01665   0.01143  -0.0703   0.2878   1.0000
  10.500   1.4860   0.01735   0.01212  -0.0685   0.2782   1.0000
  10.750   1.4959   0.01819   0.01293  -0.0665   0.2676   1.0000
  11.000   1.5023   0.01925   0.01394  -0.0642   0.2543   1.0000
  11.250   1.5055   0.02055   0.01517  -0.0617   0.2379   1.0000
  11.500   1.5069   0.02203   0.01658  -0.0591   0.2215   1.0000
  11.750   1.5037   0.02389   0.01835  -0.0562   0.2031   1.0000
  12.000   1.5003   0.02588   0.02026  -0.0536   0.1859   1.0000
  12.250   1.4959   0.02806   0.02236  -0.0511   0.1695   1.0000
  12.500   1.4893   0.03051   0.02473  -0.0487   0.1527   1.0000
  12.750   1.4777   0.03346   0.02759  -0.0462   0.1339   1.0000
  13.000   1.4583   0.03720   0.03118  -0.0434   0.1069   1.0000
  13.250   1.4278   0.04212   0.03596  -0.0404   0.0746   1.0000
  13.500   1.3956   0.04754   0.04128  -0.0379   0.0456   1.0000
  13.750   1.3759   0.05200   0.04568  -0.0363   0.0245   1.0000
  14.000   1.3678   0.05544   0.04913  -0.0353   0.0178   1.0000
  14.250   1.3671   0.05820   0.05194  -0.0347   0.0157   1.0000
  14.500   1.3672   0.06091   0.05472  -0.0343   0.0148   1.0000
  14.750   1.3664   0.06377   0.05764  -0.0339   0.0141   1.0000
  15.000   1.3624   0.06701   0.06095  -0.0335   0.0132   1.0000
  15.250   1.3633   0.06973   0.06373  -0.0332   0.0130   1.0000
  15.500   1.3631   0.07264   0.06672  -0.0331   0.0126   1.0000
  15.750   1.3626   0.07559   0.06974  -0.0329   0.0123   1.0000
  16.000   1.3613   0.07866   0.07288  -0.0329   0.0119   1.0000
  16.250   1.3572   0.08211   0.07640  -0.0329   0.0115   1.0000
  16.500   1.3536   0.08555   0.07991  -0.0329   0.0111   1.0000
  16.750   1.3471   0.08941   0.08385  -0.0331   0.0109   1.0000
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