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GOE 614 AIRFOIL (goe614-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 614 AIRFOIL (goe614-il)
Reynolds number: 500,000
Max Cl/Cd: 77.06 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe614-il-500000-n5.txt
Download as CSV file: xf-goe614-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 614 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.3819   0.09586   0.09271  -0.0963   0.9848   0.0240
 -15.250  -0.4287   0.08201   0.07860  -0.1069   0.9830   0.0239
 -15.000  -0.4531   0.07301   0.06941  -0.1147   0.9801   0.0239
 -14.750  -0.4714   0.06605   0.06229  -0.1206   0.9751   0.0239
 -14.500  -0.4799   0.05999   0.05608  -0.1269   0.9713   0.0239
 -14.250  -0.4880   0.05445   0.05038  -0.1326   0.9661   0.0240
 -14.000  -0.4920   0.04976   0.04554  -0.1375   0.9591   0.0240
 -13.750  -0.4894   0.04517   0.04079  -0.1435   0.9534   0.0241
 -13.500  -0.4832   0.04166   0.03716  -0.1478   0.9448   0.0241
 -13.250  -0.4712   0.03763   0.03293  -0.1550   0.9380   0.0242
 -13.000  -0.4535   0.03463   0.02982  -0.1599   0.9291   0.0243
 -12.750  -0.4245   0.03194   0.02701  -0.1660   0.9223   0.0245
 -12.500  -0.3992   0.02969   0.02463  -0.1710   0.9107   0.0245
 -12.250  -0.3762   0.02778   0.02260  -0.1748   0.8970   0.0247
 -12.000  -0.3581   0.02628   0.02096  -0.1767   0.8814   0.0248
 -11.750  -0.3459   0.02514   0.01968  -0.1766   0.8659   0.0249
 -11.500  -0.3377   0.02420   0.01861  -0.1751   0.8509   0.0251
 -11.250  -0.3315   0.02348   0.01777  -0.1726   0.8372   0.0251
 -11.000  -0.3243   0.02282   0.01702  -0.1701   0.8250   0.0253
 -10.750  -0.3125   0.02219   0.01628  -0.1683   0.8145   0.0255
 -10.500  -0.3002   0.02158   0.01557  -0.1664   0.8032   0.0257
 -10.250  -0.2863   0.02098   0.01488  -0.1646   0.7937   0.0259
 -10.000  -0.2716   0.02042   0.01422  -0.1629   0.7837   0.0260
  -9.750  -0.2559   0.01985   0.01357  -0.1612   0.7743   0.0261
  -9.500  -0.2395   0.01934   0.01296  -0.1596   0.7647   0.0263
  -9.250  -0.2224   0.01882   0.01237  -0.1580   0.7557   0.0264
  -9.000  -0.2048   0.01836   0.01182  -0.1565   0.7459   0.0266
  -8.750  -0.1867   0.01788   0.01127  -0.1550   0.7364   0.0267
  -8.500  -0.1682   0.01746   0.01076  -0.1535   0.7265   0.0269
  -8.250  -0.1489   0.01704   0.01027  -0.1522   0.7173   0.0270
  -8.000  -0.1298   0.01667   0.00980  -0.1507   0.7072   0.0272
  -7.750  -0.1100   0.01629   0.00935  -0.1493   0.6966   0.0273
  -7.500  -0.0905   0.01596   0.00894  -0.1479   0.6859   0.0275
  -7.250  -0.0701   0.01563   0.00853  -0.1466   0.6751   0.0276
  -7.000  -0.0496   0.01534   0.00816  -0.1452   0.6654   0.0278
  -6.750  -0.0289   0.01505   0.00779  -0.1439   0.6550   0.0279
  -6.500  -0.0078   0.01479   0.00746  -0.1427   0.6450   0.0280
  -6.250   0.0114   0.01443   0.00703  -0.1411   0.6342   0.0283
  -6.000   0.0322   0.01412   0.00665  -0.1398   0.6241   0.0285
  -5.500   0.0745   0.01360   0.00601  -0.1373   0.6050   0.0292
  -5.000   0.1187   0.01322   0.00551  -0.1350   0.5879   0.0300
  -4.750   0.1405   0.01307   0.00528  -0.1338   0.5791   0.0304
  -4.500   0.1633   0.01291   0.00507  -0.1328   0.5711   0.0307
  -4.250   0.1856   0.01278   0.00487  -0.1316   0.5627   0.0310
  -4.000   0.2082   0.01268   0.00470  -0.1305   0.5551   0.0314
  -3.750   0.2315   0.01257   0.00454  -0.1295   0.5478   0.0318
  -3.500   0.2537   0.01250   0.00440  -0.1283   0.5411   0.0322
  -3.250   0.2772   0.01239   0.00424  -0.1274   0.5351   0.0327
  -3.000   0.3002   0.01229   0.00410  -0.1263   0.5287   0.0335
  -2.750   0.3220   0.01224   0.00399  -0.1251   0.5224   0.0344
  -2.500   0.3452   0.01216   0.00388  -0.1241   0.5169   0.0355
  -2.250   0.3673   0.01211   0.00379  -0.1228   0.5106   0.0368
  -2.000   0.3878   0.01204   0.00369  -0.1213   0.5051   0.0405
  -1.750   0.4079   0.01174   0.00357  -0.1198   0.5002   0.0909
  -1.500   0.4295   0.01169   0.00353  -0.1185   0.4933   0.1043
  -1.250   0.4508   0.01166   0.00350  -0.1172   0.4881   0.1145
  -0.750   0.4934   0.01145   0.00348  -0.1147   0.4771   0.1735
  -0.500   0.5150   0.01145   0.00353  -0.1134   0.4720   0.1973
  -0.250   0.5358   0.01153   0.00357  -0.1120   0.4667   0.2089
   0.000   0.5594   0.01155   0.00362  -0.1111   0.4620   0.2205
   0.250   0.5817   0.01160   0.00368  -0.1100   0.4564   0.2299
   0.500   0.6023   0.01171   0.00376  -0.1086   0.4505   0.2393
   0.750   0.6240   0.01177   0.00384  -0.1074   0.4444   0.2543
   1.000   0.6457   0.01184   0.00393  -0.1062   0.4382   0.2671
   1.250   0.6664   0.01194   0.00404  -0.1049   0.4330   0.2824
   1.500   0.6879   0.01203   0.00414  -0.1037   0.4286   0.2952
   1.750   0.7100   0.01208   0.00425  -0.1026   0.4237   0.3159
   2.000   0.7307   0.01217   0.00438  -0.1013   0.4184   0.3376
   2.250   0.7501   0.01231   0.00453  -0.0998   0.4132   0.3568
   2.500   0.7722   0.01239   0.00466  -0.0988   0.4086   0.3783
   2.750   0.7931   0.01248   0.00481  -0.0975   0.4035   0.4022
   3.000   0.8130   0.01259   0.00498  -0.0961   0.3993   0.4285
   3.250   0.8324   0.01274   0.00516  -0.0947   0.3956   0.4522
   3.500   0.8540   0.01284   0.00532  -0.0936   0.3921   0.4754
   3.750   0.8750   0.01295   0.00549  -0.0924   0.3880   0.4985
   4.000   0.8941   0.01311   0.00570  -0.0909   0.3831   0.5236
   4.250   0.9109   0.01331   0.00594  -0.0891   0.3777   0.5539
   4.500   0.9305   0.01337   0.00615  -0.0877   0.3732   0.5997
   4.750   0.9465   0.01343   0.00641  -0.0856   0.3679   0.6664
   5.000   0.9576   0.01333   0.00668  -0.0825   0.3640   0.7999
   5.500   1.0727   0.01392   0.00744  -0.0962   0.3479   1.0000
   5.750   1.0912   0.01425   0.00773  -0.0948   0.3432   1.0000
   6.000   1.1108   0.01456   0.00802  -0.0937   0.3370   1.0000
   6.250   1.1281   0.01495   0.00838  -0.0922   0.3306   1.0000
   6.500   1.1463   0.01533   0.00873  -0.0909   0.3250   1.0000
   6.750   1.1636   0.01576   0.00913  -0.0896   0.3171   1.0000
   7.000   1.1795   0.01626   0.00959  -0.0880   0.3098   1.0000
   7.250   1.1961   0.01676   0.01006  -0.0866   0.3016   1.0000
   7.500   1.2109   0.01734   0.01060  -0.0851   0.2937   1.0000
   7.750   1.2255   0.01797   0.01119  -0.0835   0.2846   1.0000
   8.000   1.2396   0.01865   0.01184  -0.0820   0.2767   1.0000
   8.250   1.2531   0.01938   0.01253  -0.0805   0.2682   1.0000
   8.500   1.2663   0.02015   0.01328  -0.0790   0.2607   1.0000
   8.750   1.2792   0.02097   0.01407  -0.0775   0.2532   1.0000
   9.000   1.2921   0.02181   0.01490  -0.0761   0.2476   1.0000
   9.250   1.3045   0.02271   0.01579  -0.0747   0.2402   1.0000
   9.500   1.3152   0.02374   0.01680  -0.0733   0.2340   1.0000
   9.750   1.3277   0.02469   0.01775  -0.0720   0.2287   1.0000
  10.000   1.3400   0.02568   0.01875  -0.0708   0.2237   1.0000
  10.250   1.3498   0.02687   0.01993  -0.0695   0.2187   1.0000
  10.500   1.3614   0.02797   0.02104  -0.0684   0.2143   1.0000
  10.750   1.3723   0.02913   0.02223  -0.0673   0.2096   1.0000
  11.000   1.3821   0.03041   0.02351  -0.0662   0.2053   1.0000
  11.250   1.3901   0.03187   0.02498  -0.0650   0.2007   1.0000
  11.500   1.4010   0.03312   0.02627  -0.0641   0.1969   1.0000
  11.750   1.4050   0.03497   0.02810  -0.0628   0.1886   1.0000
  12.000   1.4116   0.03664   0.02980  -0.0618   0.1820   1.0000
  12.250   1.4126   0.03883   0.03197  -0.0606   0.1711   1.0000
  12.750   1.3750   0.04713   0.04006  -0.0569   0.1227   1.0000
  13.000   1.3717   0.05004   0.04299  -0.0560   0.1177   1.0000
  13.250   1.3745   0.05239   0.04539  -0.0554   0.1157   1.0000
  13.500   1.3766   0.05483   0.04789  -0.0549   0.1140   1.0000
  13.750   1.3794   0.05725   0.05037  -0.0544   0.1132   1.0000
  14.000   1.3792   0.06001   0.05318  -0.0540   0.1115   1.0000
  14.250   1.3810   0.06259   0.05582  -0.0536   0.1106   1.0000
  14.500   1.3791   0.06561   0.05891  -0.0533   0.1092   1.0000
  14.750   1.3789   0.06845   0.06181  -0.0530   0.1083   1.0000
  15.000   1.3775   0.07145   0.06487  -0.0527   0.1070   1.0000
  15.250   1.3745   0.07470   0.06819  -0.0526   0.1058   1.0000
  15.500   1.3742   0.07764   0.07118  -0.0525   0.1050   1.0000
  15.750   1.3765   0.08029   0.07391  -0.0524   0.1046   1.0000
  16.000   1.3785   0.08297   0.07666  -0.0524   0.1041   1.0000
  16.250   1.3794   0.08580   0.07957  -0.0524   0.1033   1.0000
  16.500   1.3814   0.08850   0.08234  -0.0525   0.1029   1.0000
  16.750   1.3811   0.09152   0.08544  -0.0526   0.1022   1.0000
  17.000   1.3818   0.09440   0.08838  -0.0527   0.1010   1.0000
  17.250   1.3809   0.09750   0.09155  -0.0530   0.1002   1.0000
  17.500   1.3807   0.10049   0.09460  -0.0532   0.0992   1.0000
  17.750   1.3788   0.10374   0.09790  -0.0535   0.0982   1.0000
  18.000   1.3781   0.10683   0.10105  -0.0539   0.0973   1.0000
  18.250   1.3761   0.11012   0.10440  -0.0543   0.0963   1.0000
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