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GOE 288 AIRFOIL (goe288-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 288 AIRFOIL (goe288-il)
Reynolds number: 1,000,000
Max Cl/Cd: 117.1 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe288-il-1000000.txt
Download as CSV file: xf-goe288-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 288 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.7330   0.08507   0.08242  -0.0700   1.0000   0.0278
 -16.000  -0.7622   0.07648   0.07368  -0.0758   1.0000   0.0279
 -15.750  -0.7815   0.06987   0.06695  -0.0804   1.0000   0.0279
 -15.500  -0.7974   0.06416   0.06114  -0.0844   1.0000   0.0280
 -15.250  -0.8115   0.05907   0.05595  -0.0880   1.0000   0.0280
 -15.000  -0.8232   0.05444   0.05123  -0.0912   1.0000   0.0281
 -14.750  -0.8336   0.05017   0.04688  -0.0940   1.0000   0.0282
 -14.500  -0.8438   0.04626   0.04289  -0.0964   1.0000   0.0282
 -14.250  -0.8578   0.04278   0.03935  -0.0974   1.0000   0.0283
 -14.000  -0.8673   0.03923   0.03573  -0.0994   0.9984   0.0284
 -13.750  -0.8508   0.03508   0.03147  -0.1069   0.9937   0.0285
 -13.500  -0.8286   0.03079   0.02705  -0.1160   0.9868   0.0287
 -13.250  -0.8000   0.02785   0.02396  -0.1230   0.9812   0.0290
 -13.000  -0.7783   0.02622   0.02223  -0.1253   0.9721   0.0292
 -12.750  -0.7553   0.02489   0.02080  -0.1269   0.9635   0.0294
 -12.500  -0.7340   0.02374   0.01955  -0.1276   0.9530   0.0296
 -12.250  -0.7131   0.02276   0.01847  -0.1278   0.9409   0.0298
 -12.000  -0.6912   0.02190   0.01750  -0.1278   0.9287   0.0299
 -11.750  -0.6685   0.02114   0.01663  -0.1278   0.9158   0.0300
 -11.500  -0.6451   0.02049   0.01586  -0.1277   0.9020   0.0302
 -11.250  -0.6253   0.01909   0.01435  -0.1276   0.8877   0.0305
 -11.000  -0.6025   0.01815   0.01332  -0.1276   0.8737   0.0308
 -10.750  -0.5781   0.01745   0.01253  -0.1276   0.8589   0.0311
 -10.500  -0.5528   0.01687   0.01186  -0.1276   0.8427   0.0314
 -10.250  -0.5270   0.01636   0.01125  -0.1276   0.8251   0.0317
 -10.000  -0.5008   0.01589   0.01068  -0.1276   0.8063   0.0320
  -9.750  -0.4743   0.01546   0.01014  -0.1277   0.7861   0.0324
  -9.500  -0.4476   0.01507   0.00963  -0.1277   0.7647   0.0327
  -9.250  -0.4206   0.01472   0.00915  -0.1277   0.7430   0.0331
  -9.000  -0.3932   0.01441   0.00872  -0.1278   0.7224   0.0335
  -8.750  -0.3655   0.01412   0.00831  -0.1279   0.7041   0.0339
  -8.500  -0.3376   0.01383   0.00791  -0.1280   0.6882   0.0342
  -8.250  -0.3095   0.01358   0.00756  -0.1281   0.6739   0.0344
  -8.000  -0.2818   0.01303   0.00691  -0.1284   0.6615   0.0350
  -7.750  -0.2535   0.01263   0.00643  -0.1286   0.6510   0.0356
  -7.500  -0.2248   0.01234   0.00608  -0.1288   0.6411   0.0362
  -7.250  -0.1958   0.01209   0.00577  -0.1291   0.6328   0.0368
  -7.000  -0.1667   0.01187   0.00549  -0.1293   0.6242   0.0374
  -6.750  -0.1375   0.01167   0.00522  -0.1295   0.6161   0.0381
  -6.500  -0.1081   0.01149   0.00497  -0.1298   0.6084   0.0388
  -6.250  -0.0790   0.01127   0.00467  -0.1300   0.6004   0.0396
  -6.000  -0.0494   0.01100   0.00438  -0.1303   0.5948   0.0410
  -5.750  -0.0198   0.01081   0.00417  -0.1306   0.5893   0.0425
  -5.500   0.0097   0.01069   0.00399  -0.1308   0.5837   0.0439
  -5.250   0.0393   0.01047   0.00375  -0.1311   0.5783   0.0467
  -5.000   0.0692   0.01027   0.00354  -0.1314   0.5730   0.0506
  -4.750   0.0988   0.01002   0.00331  -0.1317   0.5678   0.0616
  -4.500   0.1281   0.00972   0.00313  -0.1321   0.5626   0.0912
  -4.250   0.1581   0.00957   0.00303  -0.1325   0.5587   0.1065
  -4.000   0.1880   0.00945   0.00294  -0.1328   0.5539   0.1168
  -3.750   0.2177   0.00938   0.00285  -0.1330   0.5489   0.1252
  -3.500   0.2473   0.00935   0.00279  -0.1332   0.5439   0.1333
  -3.250   0.2772   0.00924   0.00272  -0.1336   0.5407   0.1437
  -3.000   0.3073   0.00914   0.00265  -0.1339   0.5374   0.1541
  -2.750   0.3371   0.00906   0.00258  -0.1342   0.5336   0.1666
  -2.500   0.3668   0.00895   0.00252  -0.1345   0.5297   0.1850
  -2.250   0.3962   0.00884   0.00248  -0.1348   0.5251   0.2164
  -2.000   0.4261   0.00871   0.00246  -0.1351   0.5219   0.2504
  -1.750   0.4560   0.00864   0.00246  -0.1355   0.5181   0.2750
  -1.500   0.4857   0.00862   0.00247  -0.1357   0.5141   0.2916
  -1.250   0.5152   0.00865   0.00248  -0.1359   0.5100   0.3048
  -1.000   0.5446   0.00870   0.00253  -0.1361   0.5057   0.3172
  -0.750   0.5746   0.00869   0.00254  -0.1364   0.5027   0.3264
  -0.500   0.6043   0.00870   0.00256  -0.1366   0.4986   0.3337
  -0.250   0.6338   0.00876   0.00258  -0.1368   0.4940   0.3392
   0.000   0.6628   0.00881   0.00262  -0.1369   0.4886   0.3467
   0.250   0.6926   0.00883   0.00265  -0.1372   0.4846   0.3532
   0.500   0.7221   0.00888   0.00267  -0.1374   0.4796   0.3575
   0.750   0.7512   0.00891   0.00270  -0.1375   0.4741   0.3638
   1.000   0.7802   0.00898   0.00276  -0.1377   0.4688   0.3695
   1.250   0.8097   0.00902   0.00279  -0.1379   0.4631   0.3748
   1.500   0.8385   0.00909   0.00284  -0.1380   0.4561   0.3807
   1.750   0.8673   0.00915   0.00291  -0.1381   0.4492   0.3886
   2.000   0.8960   0.00926   0.00298  -0.1382   0.4400   0.3956
   2.250   0.9243   0.00934   0.00305  -0.1383   0.4300   0.4027
   2.500   0.9521   0.00948   0.00314  -0.1383   0.4169   0.4083
   2.750   0.9794   0.00966   0.00324  -0.1382   0.4015   0.4131
   3.000   1.0064   0.00986   0.00337  -0.1381   0.3852   0.4181
   3.250   1.0330   0.01008   0.00353  -0.1379   0.3697   0.4245
   3.500   1.0598   0.01029   0.00369  -0.1377   0.3572   0.4311
   3.750   1.0863   0.01051   0.00386  -0.1375   0.3471   0.4377
   4.000   1.1129   0.01070   0.00404  -0.1373   0.3388   0.4457
   4.250   1.1395   0.01090   0.00422  -0.1372   0.3319   0.4536
   4.500   1.1665   0.01104   0.00439  -0.1370   0.3265   0.4648
   4.750   1.1926   0.01125   0.00459  -0.1368   0.3209   0.4784
   5.000   1.2189   0.01142   0.00480  -0.1366   0.3161   0.4972
   5.250   1.2459   0.01151   0.00497  -0.1365   0.3131   0.5257
   5.500   1.2724   0.01161   0.00518  -0.1364   0.3097   0.5734
   5.750   1.2983   0.01161   0.00545  -0.1363   0.3063   0.6883
   6.000   1.3170   0.01133   0.00571  -0.1343   0.3027   1.0000
   6.250   1.3423   0.01157   0.00593  -0.1340   0.2997   1.0000
   6.500   1.3688   0.01173   0.00611  -0.1338   0.2980   1.0000
   6.750   1.3947   0.01191   0.00630  -0.1335   0.2959   1.0000
   7.000   1.4199   0.01213   0.00651  -0.1331   0.2935   1.0000
   7.250   1.4443   0.01238   0.00676  -0.1326   0.2910   1.0000
   7.500   1.4676   0.01267   0.00703  -0.1319   0.2881   1.0000
   7.750   1.4888   0.01305   0.00738  -0.1309   0.2843   1.0000
   8.000   1.5133   0.01324   0.00760  -0.1304   0.2825   1.0000
   8.250   1.5375   0.01342   0.00781  -0.1299   0.2807   1.0000
   8.500   1.5606   0.01365   0.00806  -0.1292   0.2789   1.0000
   8.750   1.5819   0.01390   0.00833  -0.1281   0.2770   1.0000
   9.000   1.6016   0.01420   0.00864  -0.1268   0.2750   1.0000
   9.250   1.6203   0.01455   0.00900  -0.1253   0.2727   1.0000
   9.500   1.6376   0.01499   0.00943  -0.1237   0.2701   1.0000
   9.750   1.6539   0.01549   0.00994  -0.1220   0.2674   1.0000
  10.000   1.6761   0.01573   0.01023  -0.1213   0.2661   1.0000
  10.250   1.6978   0.01600   0.01054  -0.1205   0.2639   1.0000
  10.500   1.7181   0.01634   0.01091  -0.1195   0.2615   1.0000
  10.750   1.7368   0.01677   0.01136  -0.1184   0.2590   1.0000
  11.000   1.7534   0.01731   0.01190  -0.1170   0.2560   1.0000
  11.250   1.7671   0.01803   0.01261  -0.1152   0.2525   1.0000
  11.500   1.7859   0.01849   0.01313  -0.1142   0.2509   1.0000
  11.750   1.8054   0.01893   0.01362  -0.1134   0.2493   1.0000
  12.000   1.8242   0.01941   0.01415  -0.1125   0.2469   1.0000
  12.250   1.8410   0.02003   0.01479  -0.1114   0.2438   1.0000
  12.500   1.8553   0.02082   0.01559  -0.1101   0.2405   1.0000
  12.750   1.8658   0.02186   0.01664  -0.1084   0.2368   1.0000
  13.000   1.8844   0.02242   0.01727  -0.1077   0.2345   1.0000
  13.250   1.9007   0.02315   0.01804  -0.1068   0.2312   1.0000
  13.500   1.9133   0.02415   0.01906  -0.1056   0.2268   1.0000
  13.750   1.9210   0.02554   0.02045  -0.1040   0.2218   1.0000
  14.000   1.9363   0.02640   0.02137  -0.1032   0.2181   1.0000
  14.250   1.9460   0.02771   0.02270  -0.1020   0.2127   1.0000
  14.500   1.9511   0.02944   0.02444  -0.1006   0.2073   1.0000
  14.750   1.9606   0.03085   0.02589  -0.0996   0.2015   1.0000
  15.000   1.9603   0.03314   0.02816  -0.0980   0.1937   1.0000
  15.250   1.9604   0.03547   0.03050  -0.0967   0.1836   1.0000
  15.500   1.9522   0.03867   0.03367  -0.0952   0.1709   1.0000
  15.750   1.9346   0.04289   0.03785  -0.0935   0.1557   1.0000
  16.000   1.9108   0.04792   0.04282  -0.0919   0.1387   1.0000
  16.500   1.8479   0.06012   0.05494  -0.0893   0.1062   1.0000
  16.750   1.8237   0.06569   0.06052  -0.0886   0.0961   1.0000
  17.000   1.8038   0.07093   0.06578  -0.0882   0.0892   1.0000
  17.250   1.7894   0.07562   0.07053  -0.0880   0.0844   1.0000
  17.500   1.7734   0.08060   0.07556  -0.0879   0.0804   1.0000
  17.750   1.7609   0.08521   0.08023  -0.0880   0.0772   1.0000
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