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GOE 563 AIRFOIL (goe563-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 563 AIRFOIL (goe563-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.61 at α=2.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe563-il-1000000.txt
Download as CSV file: xf-goe563-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 563 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -1.0430   0.03741   0.03500  -0.0761   1.0000   0.0104
 -13.750  -1.0551   0.03479   0.03225  -0.0748   1.0000   0.0105
 -13.500  -1.0674   0.03234   0.02965  -0.0719   1.0000   0.0106
 -13.250  -1.0671   0.03036   0.02751  -0.0699   1.0000   0.0108
 -13.000  -1.0600   0.02890   0.02592  -0.0682   1.0000   0.0110
 -12.750  -1.0510   0.02758   0.02448  -0.0664   1.0000   0.0113
 -12.500  -1.0419   0.02626   0.02302  -0.0644   1.0000   0.0115
 -12.250  -1.0318   0.02504   0.02166  -0.0624   1.0000   0.0118
 -12.000  -1.0207   0.02399   0.02047  -0.0603   1.0000   0.0120
 -11.750  -1.0090   0.02308   0.01943  -0.0580   1.0000   0.0122
 -11.500  -1.0066   0.02123   0.01737  -0.0547   1.0000   0.0127
 -11.250  -0.9940   0.02046   0.01653  -0.0525   1.0000   0.0131
 -11.000  -0.9772   0.02013   0.01617  -0.0507   1.0000   0.0135
 -10.750  -0.9515   0.01968   0.01568  -0.0508   0.9993   0.0140
 -10.500  -0.9206   0.01917   0.01510  -0.0519   0.9981   0.0146
 -10.250  -0.8897   0.01864   0.01446  -0.0530   0.9967   0.0152
 -10.000  -0.8577   0.01830   0.01404  -0.0542   0.9954   0.0156
  -9.750  -0.8286   0.01713   0.01276  -0.0554   0.9942   0.0167
  -9.500  -0.7988   0.01689   0.01250  -0.0561   0.9923   0.0173
  -9.250  -0.7681   0.01667   0.01225  -0.0569   0.9904   0.0180
  -9.000  -0.7369   0.01634   0.01186  -0.0579   0.9887   0.0188
  -8.750  -0.7051   0.01598   0.01141  -0.0590   0.9872   0.0194
  -8.500  -0.6750   0.01504   0.01033  -0.0600   0.9857   0.0204
  -8.250  -0.6424   0.01470   0.01000  -0.0613   0.9846   0.0213
  -8.000  -0.6090   0.01447   0.00976  -0.0627   0.9838   0.0221
  -7.750  -0.5783   0.01416   0.00939  -0.0635   0.9819   0.0230
  -7.500  -0.5494   0.01384   0.00901  -0.0638   0.9790   0.0239
  -7.250  -0.5172   0.01372   0.00885  -0.0648   0.9771   0.0246
  -7.000  -0.4874   0.01256   0.00756  -0.0657   0.9753   0.0258
  -6.750  -0.4552   0.01199   0.00697  -0.0669   0.9739   0.0268
  -6.500  -0.4225   0.01164   0.00659  -0.0680   0.9723   0.0278
  -6.250  -0.3898   0.01133   0.00626  -0.0692   0.9707   0.0289
  -6.000  -0.3624   0.01100   0.00589  -0.0691   0.9666   0.0298
  -5.750  -0.3340   0.01066   0.00551  -0.0692   0.9625   0.0305
  -5.500  -0.3041   0.01045   0.00526  -0.0696   0.9591   0.0311
  -5.250  -0.2762   0.00974   0.00447  -0.0697   0.9553   0.0322
  -5.000  -0.2527   0.00925   0.00394  -0.0687   0.9487   0.0333
  -4.750  -0.2257   0.00892   0.00358  -0.0684   0.9435   0.0344
  -4.500  -0.1991   0.00869   0.00332  -0.0681   0.9380   0.0355
  -4.250  -0.1734   0.00845   0.00305  -0.0675   0.9316   0.0366
  -4.000  -0.1461   0.00823   0.00278  -0.0673   0.9265   0.0376
  -3.750  -0.1202   0.00804   0.00257  -0.0667   0.9201   0.0386
  -3.500  -0.0934   0.00788   0.00238  -0.0664   0.9141   0.0392
  -3.250  -0.0672   0.00760   0.00205  -0.0659   0.9081   0.0423
  -3.000  -0.0409   0.00741   0.00187  -0.0654   0.9013   0.0458
  -2.750  -0.0137   0.00728   0.00170  -0.0651   0.8948   0.0493
  -2.500   0.0117   0.00699   0.00154  -0.0645   0.8857   0.0755
  -2.250   0.0382   0.00686   0.00145  -0.0641   0.8765   0.0990
  -2.000   0.0648   0.00675   0.00135  -0.0637   0.8669   0.1116
  -1.750   0.0913   0.00665   0.00126  -0.0633   0.8559   0.1221
  -1.500   0.1178   0.00655   0.00117  -0.0628   0.8446   0.1366
  -1.250   0.1438   0.00639   0.00110  -0.0624   0.8329   0.1730
  -1.000   0.1696   0.00619   0.00103  -0.0619   0.8217   0.2241
  -0.750   0.1932   0.00571   0.00097  -0.0612   0.8106   0.3705
  -0.500   0.2180   0.00544   0.00095  -0.0606   0.7994   0.4604
  -0.250   0.2425   0.00519   0.00093  -0.0598   0.7883   0.5469
   0.000   0.2646   0.00484   0.00094  -0.0586   0.7754   0.6763
   0.250   0.2830   0.00441   0.00098  -0.0562   0.7601   0.8328
   0.500   0.3085   0.00429   0.00104  -0.0553   0.7452   0.9145
   0.750   0.3466   0.00435   0.00110  -0.0573   0.7290   0.9540
   1.000   0.3859   0.00447   0.00113  -0.0597   0.7057   0.9709
   1.250   0.4241   0.00461   0.00118  -0.0619   0.6852   0.9811
   1.500   0.4616   0.00474   0.00122  -0.0639   0.6612   0.9870
   1.750   0.4965   0.00491   0.00126  -0.0654   0.6301   0.9922
   2.000   0.5356   0.00511   0.00132  -0.0679   0.5948   0.9971
   2.250   0.5703   0.00540   0.00138  -0.0696   0.5407   1.0000
   2.500   0.5907   0.00568   0.00146  -0.0680   0.4943   1.0000
   2.750   0.6115   0.00596   0.00157  -0.0666   0.4490   1.0000
   3.000   0.6317   0.00631   0.00169  -0.0651   0.3961   1.0000
   3.250   0.6519   0.00668   0.00185  -0.0636   0.3476   1.0000
   3.500   0.6733   0.00698   0.00199  -0.0623   0.3140   1.0000
   3.750   0.6959   0.00721   0.00214  -0.0612   0.2912   1.0000
   4.000   0.7185   0.00745   0.00228  -0.0601   0.2689   1.0000
   4.250   0.7409   0.00771   0.00244  -0.0590   0.2425   1.0000
   4.500   0.7632   0.00799   0.00260  -0.0579   0.2168   1.0000
   4.750   0.7850   0.00832   0.00280  -0.0567   0.1863   1.0000
   5.000   0.8058   0.00874   0.00303  -0.0554   0.1508   1.0000
   5.250   0.8273   0.00912   0.00328  -0.0542   0.1255   1.0000
   5.500   0.8495   0.00943   0.00352  -0.0531   0.1095   1.0000
   5.750   0.8721   0.00973   0.00377  -0.0521   0.0958   1.0000
   6.000   0.8933   0.01015   0.00405  -0.0509   0.0708   1.0000
   6.250   0.9124   0.01078   0.00447  -0.0493   0.0405   1.0000
   6.500   0.9349   0.01112   0.00481  -0.0483   0.0360   1.0000
   6.750   0.9564   0.01157   0.00526  -0.0470   0.0314   1.0000
   7.000   0.9797   0.01183   0.00555  -0.0462   0.0300   1.0000
   7.250   1.0023   0.01217   0.00589  -0.0452   0.0279   1.0000
   7.500   1.0232   0.01267   0.00641  -0.0440   0.0252   1.0000
   7.750   1.0454   0.01304   0.00682  -0.0430   0.0239   1.0000
   8.000   1.0682   0.01335   0.00716  -0.0421   0.0225   1.0000
   8.250   1.0902   0.01372   0.00754  -0.0411   0.0210   1.0000
   8.500   1.1087   0.01441   0.00826  -0.0395   0.0191   1.0000
   8.750   1.1315   0.01469   0.00858  -0.0386   0.0183   1.0000
   9.000   1.1532   0.01506   0.00897  -0.0376   0.0173   1.0000
   9.250   1.1743   0.01547   0.00941  -0.0365   0.0164   1.0000
   9.500   1.1922   0.01613   0.01010  -0.0350   0.0153   1.0000
   9.750   1.2098   0.01680   0.01084  -0.0333   0.0146   1.0000
  10.000   1.2302   0.01720   0.01129  -0.0321   0.0140   1.0000
  10.250   1.2502   0.01761   0.01173  -0.0309   0.0133   1.0000
  10.500   1.2686   0.01812   0.01227  -0.0295   0.0127   1.0000
  10.750   1.2859   0.01868   0.01287  -0.0279   0.0122   1.0000
  11.000   1.2943   0.01971   0.01396  -0.0249   0.0116   1.0000
  11.250   1.3029   0.02058   0.01494  -0.0219   0.0113   1.0000
  11.500   1.3175   0.02111   0.01552  -0.0199   0.0110   1.0000
  11.750   1.3300   0.02177   0.01626  -0.0176   0.0107   1.0000
  12.000   1.3410   0.02254   0.01711  -0.0153   0.0104   1.0000
  12.250   1.3525   0.02331   0.01794  -0.0132   0.0100   1.0000
  12.500   1.3623   0.02418   0.01889  -0.0110   0.0098   1.0000
  12.750   1.3722   0.02507   0.01983  -0.0089   0.0095   1.0000
  13.000   1.3801   0.02612   0.02096  -0.0068   0.0093   1.0000
  13.250   1.3858   0.02736   0.02228  -0.0046   0.0091   1.0000
  13.500   1.3785   0.02967   0.02472  -0.0015   0.0087   1.0000
  13.750   1.3763   0.03173   0.02691   0.0007   0.0085   1.0000
  14.000   1.3832   0.03310   0.02838   0.0020   0.0084   1.0000
  14.250   1.3847   0.03503   0.03042   0.0034   0.0084   1.0000
  14.500   1.3903   0.03668   0.03218   0.0044   0.0082   1.0000
  14.750   1.3877   0.03921   0.03484   0.0054   0.0081   1.0000
  15.000   1.3866   0.04175   0.03749   0.0059   0.0080   1.0000
  15.250   1.3861   0.04438   0.04023   0.0062   0.0078   1.0000
  15.500   1.3805   0.04774   0.04374   0.0060   0.0078   1.0000
  15.750   1.3756   0.05125   0.04737   0.0054   0.0077   1.0000
  16.000   1.3721   0.05479   0.05102   0.0045   0.0075   1.0000
  16.250   1.3578   0.06005   0.05643   0.0028   0.0076   1.0000
  16.500   1.3539   0.06417   0.06065   0.0010   0.0074   1.0000
  16.750   1.3412   0.06984   0.06646  -0.0016   0.0073   1.0000
  17.000   1.3252   0.07635   0.07311  -0.0048   0.0073   1.0000
  17.250   1.3017   0.08440   0.08133  -0.0089   0.0074   1.0000
  17.500   1.2829   0.09204   0.08912  -0.0130   0.0073   1.0000
  17.750   1.2624   0.10020   0.09741  -0.0174   0.0073   1.0000
  18.000   1.2405   0.10878   0.10613  -0.0221   0.0073   1.0000
  18.250   1.2161   0.11811   0.11560  -0.0273   0.0074   1.0000
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