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GOE 289 (MVA 289) AIRFOIL (goe289-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 289 (MVA 289) AIRFOIL (goe289-il)
Reynolds number: 200,000
Max Cl/Cd: 65.9 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe289-il-200000.txt
Download as CSV file: xf-goe289-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.1161   0.12218   0.11868  -0.0720   0.9758   0.0694
 -11.250  -0.1051   0.11804   0.11452  -0.0781   0.9719   0.0728
 -11.000  -0.1124   0.11277   0.10928  -0.0863   0.9652   0.0743
 -10.750  -0.0806   0.10910   0.10559  -0.0869   0.9614   0.0752
 -10.500  -0.0540   0.10555   0.10201  -0.0898   0.9583   0.0766
 -10.250  -0.0343   0.10210   0.09855  -0.0932   0.9532   0.0788
 -10.000  -0.0502   0.09664   0.09310  -0.1068   0.9445   0.0837
  -9.750  -0.0188   0.09198   0.08842  -0.1077   0.9424   0.0847
  -9.500   0.0111   0.08913   0.08554  -0.1090   0.9360   0.0860
  -9.250   0.0387   0.08569   0.08208  -0.1131   0.9305   0.0879
  -9.000   0.0642   0.08141   0.07774  -0.1202   0.9259   0.0915
  -8.750   0.0537   0.07386   0.07018  -0.1338   0.9112   0.0957
  -8.500  -0.0638   0.04689   0.04279  -0.1526   0.8812   0.0658
  -8.250  -0.0297   0.04647   0.04240  -0.1534   0.8743   0.0667
  -8.000  -0.1326   0.03237   0.02678  -0.1491   0.8522   0.0579
  -7.750  -0.1217   0.03006   0.02410  -0.1477   0.8427   0.0579
  -7.500  -0.1079   0.02819   0.02197  -0.1462   0.8335   0.0582
  -7.250  -0.0900   0.02641   0.01989  -0.1452   0.8251   0.0584
  -7.000  -0.0724   0.02491   0.01812  -0.1438   0.8163   0.0585
  -6.750  -0.0507   0.02358   0.01656  -0.1430   0.8081   0.0589
  -6.500  -0.0290   0.02251   0.01530  -0.1420   0.7998   0.0594
  -6.250  -0.0057   0.02155   0.01417  -0.1412   0.7914   0.0600
  -6.000   0.0182   0.02071   0.01318  -0.1405   0.7834   0.0610
  -5.750   0.0419   0.01994   0.01225  -0.1396   0.7748   0.0620
  -5.500   0.0673   0.01929   0.01144  -0.1391   0.7671   0.0636
  -5.250   0.0910   0.01878   0.01076  -0.1381   0.7581   0.0651
  -5.000   0.1161   0.01805   0.01002  -0.1377   0.7506   0.0673
  -4.750   0.1387   0.01762   0.00957  -0.1366   0.7414   0.0695
  -4.500   0.1655   0.01718   0.00900  -0.1362   0.7341   0.0724
  -4.250   0.1865   0.01674   0.00855  -0.1348   0.7247   0.0760
  -4.000   0.2143   0.01641   0.00812  -0.1347   0.7177   0.0820
  -3.750   0.2344   0.01609   0.00787  -0.1331   0.7082   0.0914
  -3.500   0.2611   0.01579   0.00758  -0.1327   0.7009   0.1182
  -3.250   0.2829   0.01567   0.00750  -0.1315   0.6919   0.1420
  -3.000   0.3093   0.01555   0.00729  -0.1312   0.6844   0.1578
  -2.750   0.3331   0.01552   0.00718  -0.1303   0.6762   0.1700
  -2.500   0.3577   0.01533   0.00700  -0.1296   0.6684   0.1833
  -2.250   0.3823   0.01521   0.00687  -0.1290   0.6612   0.1983
  -2.000   0.4054   0.01505   0.00675  -0.1280   0.6531   0.2135
  -1.750   0.4326   0.01490   0.00657  -0.1279   0.6469   0.2342
  -1.500   0.4529   0.01474   0.00656  -0.1264   0.6385   0.2618
  -1.250   0.4778   0.01457   0.00651  -0.1258   0.6318   0.3127
  -1.000   0.5002   0.01453   0.00660  -0.1247   0.6245   0.3693
  -0.750   0.5234   0.01446   0.00657  -0.1237   0.6173   0.4109
  -0.500   0.5492   0.01439   0.00649  -0.1232   0.6113   0.4447
  -0.250   0.5700   0.01431   0.00652  -0.1218   0.6035   0.4752
   0.000   0.5945   0.01418   0.00645  -0.1210   0.5971   0.5125
   0.250   0.6149   0.01406   0.00652  -0.1195   0.5900   0.5623
   0.500   0.6347   0.01383   0.00657  -0.1177   0.5832   0.6509
   0.750   0.7552   0.01346   0.00671  -0.1366   0.5736   0.9972
   1.000   0.7792   0.01361   0.00673  -0.1359   0.5665   1.0000
   1.250   0.8041   0.01379   0.00672  -0.1354   0.5604   1.0000
   1.500   0.8224   0.01395   0.00685  -0.1335   0.5530   1.0000
   1.750   0.8457   0.01412   0.00687  -0.1327   0.5467   1.0000
   2.000   0.8677   0.01434   0.00700  -0.1315   0.5403   1.0000
   2.250   0.8882   0.01453   0.00712  -0.1302   0.5336   1.0000
   2.500   0.9138   0.01475   0.00718  -0.1298   0.5280   1.0000
   2.750   0.9327   0.01497   0.00740  -0.1281   0.5213   1.0000
   3.000   0.9543   0.01517   0.00753  -0.1269   0.5149   1.0000
   3.250   0.9804   0.01544   0.00764  -0.1266   0.5093   1.0000
   3.500   0.9972   0.01565   0.00788  -0.1246   0.5024   1.0000
   3.750   1.0198   0.01587   0.00803  -0.1236   0.4966   1.0000
   4.000   1.0444   0.01617   0.00822  -0.1231   0.4912   1.0000
   4.250   1.0622   0.01642   0.00850  -0.1213   0.4850   1.0000
   4.500   1.0850   0.01667   0.00868  -0.1204   0.4796   1.0000
   4.750   1.1106   0.01699   0.00891  -0.1202   0.4746   1.0000
   5.000   1.1269   0.01726   0.00923  -0.1181   0.4687   1.0000
   5.250   1.1487   0.01752   0.00945  -0.1171   0.4635   1.0000
   5.500   1.1770   0.01786   0.00965  -0.1174   0.4588   1.0000
   5.750   1.1909   0.01816   0.01005  -0.1149   0.4535   1.0000
   6.000   1.2111   0.01846   0.01035  -0.1137   0.4486   1.0000
   6.250   1.2360   0.01877   0.01059  -0.1133   0.4444   1.0000
   6.500   1.2590   0.01917   0.01098  -0.1127   0.4403   1.0000
   6.750   1.2746   0.01954   0.01142  -0.1107   0.4357   1.0000
   7.000   1.2953   0.01987   0.01176  -0.1096   0.4314   1.0000
   7.250   1.3208   0.02021   0.01204  -0.1094   0.4278   1.0000
   7.500   1.3435   0.02065   0.01248  -0.1088   0.4239   1.0000
   7.750   1.3563   0.02106   0.01300  -0.1064   0.4198   1.0000
   8.000   1.3751   0.02145   0.01342  -0.1050   0.4159   1.0000
   8.250   1.3990   0.02182   0.01378  -0.1046   0.4126   1.0000
   8.500   1.4308   0.02229   0.01417  -0.1058   0.4095   1.0000
   8.750   1.4423   0.02282   0.01484  -0.1032   0.4064   1.0000
   9.000   1.4533   0.02333   0.01545  -0.1006   0.4032   1.0000
   9.250   1.4696   0.02379   0.01597  -0.0989   0.3999   1.0000
   9.500   1.4919   0.02420   0.01641  -0.0983   0.3969   1.0000
   9.750   1.5248   0.02462   0.01676  -0.0997   0.3937   1.0000
  10.000   1.5309   0.02520   0.01746  -0.0963   0.3902   1.0000
  10.250   1.5328   0.02573   0.01812  -0.0922   0.3862   1.0000
  10.500   1.5460   0.02607   0.01849  -0.0901   0.3819   1.0000
  10.750   1.5802   0.02617   0.01843  -0.0915   0.3764   1.0000
  11.000   1.5722   0.02692   0.01939  -0.0862   0.3730   1.0000
  11.250   1.5763   0.02759   0.02018  -0.0830   0.3691   1.0000
  11.500   1.5901   0.02797   0.02059  -0.0813   0.3647   1.0000
  11.750   1.6171   0.02818   0.02070  -0.0815   0.3599   1.0000
  12.000   1.6071   0.02925   0.02198  -0.0767   0.3560   1.0000
  12.250   1.6092   0.03005   0.02288  -0.0738   0.3514   1.0000
  12.500   1.6249   0.03041   0.02323  -0.0725   0.3467   1.0000
  12.750   1.6332   0.03121   0.02408  -0.0705   0.3423   1.0000
  13.000   1.6267   0.03258   0.02564  -0.0671   0.3379   1.0000
  13.250   1.6313   0.03347   0.02658  -0.0650   0.3330   1.0000
  13.500   1.6502   0.03384   0.02689  -0.0643   0.3279   1.0000
  13.750   1.6372   0.03586   0.02914  -0.0609   0.3237   1.0000
  14.000   1.6341   0.03743   0.03083  -0.0586   0.3184   1.0000
  14.250   1.6417   0.03832   0.03168  -0.0572   0.3117   1.0000
  14.500   1.6284   0.04092   0.03450  -0.0548   0.3068   1.0000
  14.750   1.6249   0.04286   0.03651  -0.0531   0.3000   1.0000
  15.000   1.6188   0.04527   0.03902  -0.0516   0.2935   1.0000
  15.250   1.6063   0.04837   0.04222  -0.0501   0.2848   1.0000
  15.500   1.5955   0.05164   0.04561  -0.0490   0.2769   1.0000
  15.750   1.5829   0.05521   0.04922  -0.0481   0.2661   1.0000
  16.000   1.5638   0.05985   0.05400  -0.0476   0.2548   1.0000
  16.250   1.5456   0.06462   0.05888  -0.0472   0.2427   1.0000
  16.500   1.5228   0.07009   0.06440  -0.0471   0.2266   1.0000
  16.750   1.4966   0.07615   0.07045  -0.0472   0.2065   1.0000
  17.000   1.4681   0.08263   0.07687  -0.0476   0.1852   1.0000
  17.250   1.4372   0.08961   0.08378  -0.0482   0.1641   1.0000
  17.500   1.4029   0.09723   0.09132  -0.0492   0.1435   1.0000
  17.750   1.3694   0.10499   0.09902  -0.0505   0.1232   1.0000
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