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GOE 289 (MVA 289) AIRFOIL (goe289-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 289 (MVA 289) AIRFOIL (goe289-il)
Reynolds number: 1,000,000
Max Cl/Cd: 109.25 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe289-il-1000000-n5.txt
Download as CSV file: xf-goe289-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 289 (MVA 289) 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.5520   0.07015   0.06763  -0.1027   0.9760   0.0209
 -14.750  -0.5870   0.05968   0.05697  -0.1119   0.9660   0.0210
 -14.500  -0.6008   0.05058   0.04768  -0.1230   0.9543   0.0211
 -14.250  -0.5960   0.04216   0.03902  -0.1368   0.9396   0.0211
 -14.000  -0.5669   0.03488   0.03146  -0.1531   0.9262   0.0212
 -13.750  -0.5353   0.02951   0.02582  -0.1664   0.9099   0.0213
 -13.500  -0.5252   0.02627   0.02234  -0.1720   0.8918   0.0213
 -13.250  -0.5242   0.02456   0.02045  -0.1721   0.8748   0.0214
 -13.000  -0.5248   0.02344   0.01918  -0.1699   0.8586   0.0214
 -12.750  -0.5261   0.02255   0.01815  -0.1665   0.8425   0.0215
 -12.500  -0.5264   0.02183   0.01730  -0.1629   0.8259   0.0215
 -12.250  -0.5173   0.02123   0.01658  -0.1605   0.8093   0.0216
 -12.000  -0.5078   0.02061   0.01581  -0.1581   0.7909   0.0216
 -11.750  -0.4972   0.01997   0.01502  -0.1559   0.7737   0.0217
 -11.500  -0.4848   0.01931   0.01423  -0.1539   0.7597   0.0217
 -11.250  -0.4733   0.01847   0.01327  -0.1518   0.7483   0.0219
 -11.000  -0.4588   0.01781   0.01251  -0.1500   0.7383   0.0221
 -10.750  -0.4414   0.01725   0.01186  -0.1486   0.7294   0.0222
 -10.500  -0.4231   0.01677   0.01129  -0.1472   0.7210   0.0223
 -10.250  -0.4029   0.01630   0.01076  -0.1462   0.7145   0.0224
 -10.000  -0.3823   0.01590   0.01028  -0.1451   0.7076   0.0226
  -9.750  -0.3613   0.01549   0.00981  -0.1440   0.7012   0.0227
  -9.500  -0.3385   0.01518   0.00945  -0.1433   0.6949   0.0230
  -9.250  -0.3169   0.01481   0.00901  -0.1423   0.6884   0.0231
  -9.000  -0.2940   0.01448   0.00862  -0.1415   0.6830   0.0233
  -8.750  -0.2711   0.01413   0.00821  -0.1407   0.6768   0.0235
  -8.500  -0.2484   0.01382   0.00782  -0.1398   0.6702   0.0237
  -8.250  -0.2251   0.01349   0.00744  -0.1390   0.6646   0.0238
  -8.000  -0.2013   0.01320   0.00709  -0.1383   0.6581   0.0240
  -7.750  -0.1781   0.01293   0.00674  -0.1374   0.6514   0.0242
  -7.500  -0.1538   0.01265   0.00641  -0.1368   0.6451   0.0244
  -7.250  -0.1298   0.01240   0.00610  -0.1360   0.6376   0.0245
  -7.000  -0.1058   0.01217   0.00581  -0.1353   0.6307   0.0247
  -6.750  -0.0813   0.01195   0.00553  -0.1346   0.6225   0.0249
  -6.500  -0.0573   0.01176   0.00527  -0.1339   0.6142   0.0250
  -6.250  -0.0326   0.01157   0.00502  -0.1332   0.6055   0.0252
  -6.000  -0.0083   0.01141   0.00479  -0.1325   0.5966   0.0253
  -5.750   0.0163   0.01126   0.00458  -0.1318   0.5864   0.0255
  -5.500   0.0399   0.01105   0.00430  -0.1309   0.5765   0.0258
  -5.250   0.0636   0.01087   0.00404  -0.1301   0.5664   0.0261
  -5.000   0.0882   0.01070   0.00383  -0.1294   0.5583   0.0265
  -4.750   0.1129   0.01058   0.00366  -0.1287   0.5503   0.0269
  -4.500   0.1379   0.01046   0.00350  -0.1281   0.5435   0.0272
  -4.250   0.1631   0.01037   0.00336  -0.1275   0.5360   0.0276
  -4.000   0.1879   0.01029   0.00324  -0.1268   0.5290   0.0281
  -3.750   0.2135   0.01020   0.00311  -0.1263   0.5228   0.0286
  -3.500   0.2387   0.01013   0.00301  -0.1257   0.5167   0.0291
  -3.250   0.2639   0.01008   0.00291  -0.1251   0.5109   0.0295
  -3.000   0.2894   0.01001   0.00281  -0.1246   0.5049   0.0299
  -2.750   0.3142   0.00994   0.00270  -0.1239   0.4988   0.0310
  -2.500   0.3393   0.00988   0.00262  -0.1233   0.4935   0.0319
  -2.250   0.3649   0.00982   0.00255  -0.1227   0.4886   0.0331
  -2.000   0.3900   0.00979   0.00249  -0.1221   0.4833   0.0346
  -1.750   0.4145   0.00976   0.00244  -0.1214   0.4780   0.0382
  -1.500   0.4382   0.00953   0.00235  -0.1206   0.4732   0.0742
  -1.250   0.4625   0.00948   0.00233  -0.1199   0.4670   0.0905
  -1.000   0.4865   0.00947   0.00233  -0.1191   0.4615   0.1029
  -0.750   0.5118   0.00945   0.00232  -0.1185   0.4569   0.1121
  -0.500   0.5365   0.00944   0.00233  -0.1179   0.4518   0.1212
  -0.250   0.5603   0.00945   0.00234  -0.1171   0.4464   0.1306
   0.000   0.5848   0.00946   0.00235  -0.1163   0.4420   0.1402
   0.250   0.6091   0.00945   0.00237  -0.1156   0.4370   0.1509
   0.500   0.6324   0.00949   0.00239  -0.1147   0.4310   0.1613
   0.750   0.6547   0.00948   0.00242  -0.1136   0.4255   0.1822
   1.000   0.6759   0.00939   0.00245  -0.1123   0.4203   0.2289
   1.250   0.6959   0.00934   0.00251  -0.1107   0.4146   0.2796
   1.500   0.7169   0.00934   0.00259  -0.1094   0.4099   0.3128
   1.750   0.7394   0.00937   0.00265  -0.1083   0.4052   0.3345
   2.000   0.7611   0.00943   0.00273  -0.1071   0.4000   0.3535
   2.250   0.7820   0.00953   0.00283  -0.1057   0.3948   0.3681
   2.500   0.8044   0.00960   0.00292  -0.1046   0.3906   0.3810
   2.750   0.8262   0.00969   0.00302  -0.1035   0.3854   0.3923
   3.250   0.8684   0.00991   0.00326  -0.1009   0.3753   0.4212
   3.500   0.8891   0.00998   0.00339  -0.0996   0.3702   0.4462
   3.750   0.9083   0.01004   0.00355  -0.0980   0.3657   0.4924
   4.000   0.9242   0.00995   0.00376  -0.0958   0.3616   0.6198
   4.250   0.9367   0.00973   0.00395  -0.0927   0.3586   0.7690
   5.000   1.1061   0.01017   0.00470  -0.1124   0.3439   1.0000
   5.250   1.1273   0.01033   0.00485  -0.1112   0.3410   1.0000
   5.500   1.1482   0.01051   0.00502  -0.1101   0.3376   1.0000
   5.750   1.1683   0.01072   0.00522  -0.1088   0.3340   1.0000
   6.000   1.1878   0.01096   0.00543  -0.1074   0.3303   1.0000
   6.250   1.2092   0.01115   0.00563  -0.1064   0.3278   1.0000
   6.500   1.2305   0.01135   0.00583  -0.1054   0.3252   1.0000
   6.750   1.2513   0.01157   0.00605  -0.1043   0.3225   1.0000
   7.000   1.2717   0.01181   0.00630  -0.1032   0.3199   1.0000
   7.250   1.2915   0.01209   0.00657  -0.1021   0.3172   1.0000
   7.500   1.3107   0.01240   0.00687  -0.1008   0.3144   1.0000
   7.750   1.3316   0.01265   0.00713  -0.0999   0.3121   1.0000
   8.000   1.3518   0.01293   0.00742  -0.0989   0.3083   1.0000
   8.250   1.3703   0.01329   0.00777  -0.0977   0.3034   1.0000
   8.500   1.3870   0.01374   0.00820  -0.0962   0.2983   1.0000
   8.750   1.4071   0.01406   0.00853  -0.0953   0.2945   1.0000
   9.000   1.4257   0.01444   0.00892  -0.0942   0.2896   1.0000
   9.250   1.4420   0.01495   0.00941  -0.0929   0.2845   1.0000
   9.500   1.4599   0.01540   0.00986  -0.0917   0.2800   1.0000
   9.750   1.4783   0.01583   0.01031  -0.0907   0.2764   1.0000
  10.000   1.4951   0.01634   0.01083  -0.0896   0.2721   1.0000
  10.250   1.5096   0.01699   0.01147  -0.0881   0.2670   1.0000
  10.500   1.5272   0.01749   0.01200  -0.0871   0.2628   1.0000
  10.750   1.5397   0.01829   0.01277  -0.0856   0.2543   1.0000
  11.000   1.5541   0.01900   0.01348  -0.0843   0.2482   1.0000
  11.250   1.5627   0.02005   0.01449  -0.0825   0.2371   1.0000
  11.500   1.5722   0.02111   0.01552  -0.0808   0.2262   1.0000
  11.750   1.5741   0.02268   0.01701  -0.0785   0.2099   1.0000
  12.000   1.5638   0.02514   0.01933  -0.0752   0.1831   1.0000
  12.250   1.5294   0.02961   0.02355  -0.0705   0.1386   1.0000
  12.500   1.5030   0.03387   0.02766  -0.0671   0.1048   1.0000
  12.750   1.4841   0.03778   0.03149  -0.0647   0.0824   1.0000
  13.000   1.4786   0.04067   0.03437  -0.0633   0.0716   1.0000
  13.250   1.4677   0.04417   0.03785  -0.0618   0.0570   1.0000
  13.500   1.4436   0.04916   0.04276  -0.0602   0.0344   1.0000
  13.750   1.4384   0.05239   0.04602  -0.0594   0.0288   1.0000
  14.000   1.4347   0.05554   0.04922  -0.0588   0.0251   1.0000
  14.250   1.4329   0.05854   0.05227  -0.0583   0.0232   1.0000
  14.500   1.4312   0.06158   0.05536  -0.0580   0.0214   1.0000
  14.750   1.4297   0.06464   0.05848  -0.0577   0.0202   1.0000
  15.000   1.4279   0.06776   0.06166  -0.0574   0.0191   1.0000
  15.250   1.4257   0.07097   0.06493  -0.0572   0.0184   1.0000
  15.500   1.4229   0.07429   0.06832  -0.0571   0.0177   1.0000
  15.750   1.4192   0.07776   0.07184  -0.0571   0.0168   1.0000
  16.000   1.4154   0.08128   0.07542  -0.0571   0.0163   1.0000
  16.250   1.4122   0.08474   0.07895  -0.0572   0.0158   1.0000
  16.500   1.4092   0.08818   0.08247  -0.0573   0.0153   1.0000
  16.750   1.4050   0.09184   0.08619  -0.0575   0.0149   1.0000
  17.000   1.4005   0.09559   0.09001  -0.0578   0.0145   1.0000
  17.250   1.3969   0.09919   0.09366  -0.0581   0.0141   1.0000
  17.500   1.3918   0.10304   0.09758  -0.0586   0.0139   1.0000
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