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GOE 528 AIRFOIL (goe528-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 528 AIRFOIL (goe528-il)
Reynolds number: 1,000,000
Max Cl/Cd: 128.91 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe528-il-1000000-n5.txt
Download as CSV file: xf-goe528-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 528 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.5215   0.02682   0.02383  -0.1381   0.8373   0.0172
 -11.500  -0.5068   0.02544   0.02229  -0.1375   0.8277   0.0174
 -11.250  -0.4916   0.02406   0.02073  -0.1369   0.8184   0.0177
 -11.000  -0.4753   0.02271   0.01921  -0.1363   0.8099   0.0179
 -10.750  -0.4580   0.02147   0.01776  -0.1355   0.8013   0.0183
 -10.500  -0.4399   0.02022   0.01630  -0.1348   0.7935   0.0187
 -10.250  -0.4200   0.01918   0.01506  -0.1341   0.7860   0.0191
 -10.000  -0.3991   0.01826   0.01393  -0.1334   0.7790   0.0193
  -9.750  -0.3776   0.01742   0.01295  -0.1327   0.7714   0.0196
  -9.500  -0.3542   0.01691   0.01235  -0.1321   0.7641   0.0198
  -9.250  -0.3283   0.01674   0.01215  -0.1318   0.7570   0.0200
  -9.000  -0.3032   0.01649   0.01183  -0.1313   0.7500   0.0202
  -8.750  -0.2777   0.01621   0.01149  -0.1309   0.7435   0.0205
  -8.500  -0.2530   0.01582   0.01100  -0.1304   0.7358   0.0207
  -8.250  -0.2281   0.01543   0.01051  -0.1299   0.7286   0.0210
  -8.000  -0.2032   0.01500   0.00997  -0.1294   0.7210   0.0214
  -7.750  -0.1784   0.01456   0.00941  -0.1289   0.7141   0.0218
  -7.500  -0.1533   0.01407   0.00879  -0.1284   0.7064   0.0221
  -7.250  -0.1285   0.01361   0.00820  -0.1278   0.6982   0.0224
  -7.000  -0.1030   0.01318   0.00765  -0.1273   0.6899   0.0226
  -6.750  -0.0774   0.01287   0.00723  -0.1268   0.6817   0.0228
  -6.500  -0.0516   0.01249   0.00674  -0.1264   0.6731   0.0231
  -6.250  -0.0268   0.01200   0.00615  -0.1258   0.6636   0.0235
  -6.000  -0.0010   0.01168   0.00576  -0.1253   0.6533   0.0237
  -5.750   0.0251   0.01144   0.00545  -0.1249   0.6435   0.0240
  -5.500   0.0510   0.01122   0.00514  -0.1244   0.6324   0.0242
  -5.250   0.0772   0.01101   0.00486  -0.1240   0.6205   0.0245
  -5.000   0.1033   0.01082   0.00459  -0.1235   0.6087   0.0249
  -4.750   0.1293   0.01065   0.00434  -0.1230   0.5970   0.0252
  -4.500   0.1555   0.01050   0.00411  -0.1226   0.5852   0.0256
  -4.250   0.1817   0.01033   0.00386  -0.1221   0.5741   0.0259
  -4.000   0.2079   0.01018   0.00363  -0.1216   0.5645   0.0263
  -3.750   0.2342   0.01003   0.00342  -0.1212   0.5547   0.0265
  -3.500   0.2607   0.00991   0.00323  -0.1208   0.5464   0.0268
  -3.250   0.2873   0.00979   0.00306  -0.1204   0.5383   0.0270
  -3.000   0.3138   0.00970   0.00291  -0.1200   0.5311   0.0272
  -2.750   0.3402   0.00948   0.00265  -0.1196   0.5245   0.0277
  -2.500   0.3665   0.00938   0.00250  -0.1192   0.5180   0.0282
  -2.250   0.3935   0.00928   0.00238  -0.1189   0.5126   0.0287
  -2.000   0.4204   0.00921   0.00229  -0.1186   0.5067   0.0293
  -1.750   0.4470   0.00917   0.00222  -0.1182   0.5013   0.0299
  -1.500   0.4742   0.00911   0.00214  -0.1180   0.4965   0.0305
  -1.250   0.5012   0.00906   0.00207  -0.1177   0.4912   0.0310
  -1.000   0.5279   0.00904   0.00201  -0.1173   0.4860   0.0315
  -0.750   0.5549   0.00902   0.00197  -0.1170   0.4814   0.0320
  -0.500   0.5820   0.00896   0.00191  -0.1168   0.4767   0.0331
  -0.250   0.6088   0.00894   0.00188  -0.1165   0.4719   0.0344
   0.000   0.6353   0.00896   0.00187  -0.1161   0.4669   0.0360
   0.500   0.6892   0.00893   0.00186  -0.1156   0.4574   0.0440
   0.750   0.7152   0.00891   0.00189  -0.1152   0.4519   0.0692
   1.000   0.7418   0.00887   0.00191  -0.1149   0.4475   0.0938
   1.250   0.7681   0.00881   0.00195  -0.1145   0.4423   0.1362
   1.500   0.7932   0.00871   0.00202  -0.1141   0.4364   0.2226
   1.750   0.8190   0.00865   0.00210  -0.1137   0.4314   0.2846
   2.000   0.8440   0.00851   0.00219  -0.1132   0.4255   0.3886
   2.250   0.8674   0.00836   0.00231  -0.1124   0.4189   0.5209
   2.750   0.9476   0.00773   0.00265  -0.1181   0.4021   1.0000
   3.000   0.9725   0.00784   0.00272  -0.1175   0.3953   1.0000
   3.250   0.9966   0.00799   0.00282  -0.1167   0.3881   1.0000
   3.500   1.0213   0.00811   0.00291  -0.1161   0.3823   1.0000
   3.750   1.0458   0.00825   0.00301  -0.1154   0.3760   1.0000
   4.000   1.0698   0.00841   0.00313  -0.1146   0.3701   1.0000
   4.250   1.0944   0.00853   0.00323  -0.1140   0.3644   1.0000
   4.500   1.1182   0.00870   0.00336  -0.1133   0.3578   1.0000
   4.750   1.1421   0.00886   0.00350  -0.1125   0.3509   1.0000
   5.000   1.1649   0.00908   0.00366  -0.1116   0.3412   1.0000
   5.250   1.1881   0.00926   0.00381  -0.1108   0.3325   1.0000
   5.500   1.2103   0.00949   0.00399  -0.1098   0.3238   1.0000
   5.750   1.2335   0.00967   0.00415  -0.1090   0.3163   1.0000
   6.000   1.2553   0.00992   0.00435  -0.1079   0.3081   1.0000
   6.250   1.2777   0.01012   0.00454  -0.1070   0.3002   1.0000
   6.500   1.2989   0.01037   0.00475  -0.1058   0.2930   1.0000
   6.750   1.3208   0.01058   0.00495  -0.1048   0.2856   1.0000
   7.000   1.3406   0.01087   0.00519  -0.1035   0.2768   1.0000
   7.250   1.3594   0.01114   0.00543  -0.1019   0.2674   1.0000
   7.500   1.3772   0.01141   0.00568  -0.1001   0.2599   1.0000
   7.750   1.3946   0.01171   0.00595  -0.0983   0.2515   1.0000
   8.000   1.4114   0.01204   0.00625  -0.0965   0.2424   1.0000
   8.250   1.4286   0.01236   0.00656  -0.0947   0.2354   1.0000
   8.500   1.4458   0.01269   0.00687  -0.0930   0.2282   1.0000
   8.750   1.4618   0.01308   0.00723  -0.0911   0.2204   1.0000
   9.000   1.4781   0.01346   0.00761  -0.0894   0.2126   1.0000
   9.250   1.4925   0.01394   0.00805  -0.0874   0.2043   1.0000
   9.500   1.5095   0.01431   0.00844  -0.0858   0.1989   1.0000
   9.750   1.5229   0.01485   0.00895  -0.0838   0.1908   1.0000
  10.000   1.5375   0.01536   0.00946  -0.0820   0.1830   1.0000
  10.250   1.5481   0.01609   0.01013  -0.0798   0.1715   1.0000
  10.500   1.5590   0.01682   0.01084  -0.0777   0.1625   1.0000
  10.750   1.5661   0.01781   0.01176  -0.0752   0.1477   1.0000
  11.000   1.5743   0.01879   0.01269  -0.0731   0.1356   1.0000
  11.250   1.5682   0.02069   0.01442  -0.0696   0.1038   1.0000
  11.500   1.5629   0.02272   0.01633  -0.0665   0.0841   1.0000
  11.750   1.5694   0.02406   0.01768  -0.0648   0.0781   1.0000
  12.000   1.5771   0.02537   0.01901  -0.0633   0.0730   1.0000
  12.250   1.5841   0.02678   0.02044  -0.0619   0.0693   1.0000
  12.500   1.5925   0.02812   0.02183  -0.0607   0.0661   1.0000
  12.750   1.6023   0.02938   0.02314  -0.0596   0.0645   1.0000
  13.000   1.6078   0.03104   0.02482  -0.0584   0.0604   1.0000
  13.250   1.6120   0.03285   0.02666  -0.0573   0.0567   1.0000
  13.500   1.6188   0.03449   0.02834  -0.0563   0.0543   1.0000
  13.750   1.6218   0.03650   0.03039  -0.0553   0.0506   1.0000
  14.000   1.6251   0.03858   0.03249  -0.0544   0.0476   1.0000
  14.250   1.6289   0.04063   0.03459  -0.0537   0.0450   1.0000
  14.500   1.6284   0.04317   0.03716  -0.0529   0.0416   1.0000
  14.750   1.6304   0.04554   0.03957  -0.0523   0.0390   1.0000
  15.000   1.6290   0.04831   0.04238  -0.0517   0.0357   1.0000
  15.250   1.6277   0.05114   0.04525  -0.0513   0.0329   1.0000
  15.500   1.6227   0.05443   0.04858  -0.0509   0.0292   1.0000
  15.750   1.6173   0.05786   0.05205  -0.0506   0.0255   1.0000
  16.000   1.6085   0.06174   0.05597  -0.0505   0.0214   1.0000
  16.250   1.5994   0.06573   0.06000  -0.0505   0.0183   1.0000
  16.500   1.5941   0.06933   0.06367  -0.0505   0.0171   1.0000
  16.750   1.5872   0.07321   0.06762  -0.0507   0.0157   1.0000
  17.250   1.5733   0.08110   0.07565  -0.0514   0.0137   1.0000
  17.500   1.5675   0.08498   0.07960  -0.0519   0.0129   1.0000
  17.750   1.5604   0.08912   0.08382  -0.0525   0.0123   1.0000
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