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GOE 702 AIRFOIL (goe702-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 702 AIRFOIL (goe702-il)
Reynolds number: 1,000,000
Max Cl/Cd: 116.21 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe702-il-1000000-n5.txt
Download as CSV file: xf-goe702-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 702 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.7948   0.08729   0.08411  -0.0644   0.8709   0.0309
 -17.250  -0.8182   0.08056   0.07725  -0.0687   0.8581   0.0310
 -17.000  -0.8493   0.07307   0.06963  -0.0734   0.8464   0.0312
 -16.750  -0.8909   0.06490   0.06130  -0.0784   0.8337   0.0313
 -16.500  -0.9526   0.05498   0.05119  -0.0845   0.8198   0.0312
 -16.250  -1.1248   0.03093   0.02661  -0.1023   0.7969   0.0307
 -16.000  -1.1422   0.02815   0.02365  -0.1012   0.7793   0.0309
 -15.750  -1.1495   0.02658   0.02193  -0.0984   0.7650   0.0310
 -15.500  -1.1511   0.02548   0.02070  -0.0953   0.7521   0.0312
 -15.250  -1.1453   0.02455   0.01967  -0.0929   0.7421   0.0314
 -15.000  -1.1337   0.02372   0.01873  -0.0912   0.7326   0.0316
 -14.750  -1.1196   0.02294   0.01786  -0.0897   0.7251   0.0318
 -14.500  -1.1037   0.02223   0.01705  -0.0883   0.7171   0.0320
 -14.250  -1.0863   0.02159   0.01631  -0.0870   0.7100   0.0322
 -14.000  -1.0675   0.02097   0.01561  -0.0858   0.7040   0.0324
 -13.750  -1.0488   0.02032   0.01488  -0.0847   0.6979   0.0327
 -13.500  -1.0298   0.01966   0.01415  -0.0835   0.6924   0.0330
 -13.250  -1.0092   0.01907   0.01350  -0.0825   0.6879   0.0333
 -13.000  -0.9875   0.01854   0.01292  -0.0816   0.6836   0.0337
 -12.750  -0.9652   0.01805   0.01237  -0.0808   0.6791   0.0341
 -12.500  -0.9421   0.01761   0.01187  -0.0800   0.6743   0.0345
 -12.250  -0.9186   0.01720   0.01140  -0.0792   0.6691   0.0350
 -12.000  -0.8945   0.01680   0.01094  -0.0785   0.6646   0.0354
 -11.750  -0.8702   0.01641   0.01050  -0.0778   0.6592   0.0358
 -11.500  -0.8456   0.01606   0.01007  -0.0771   0.6538   0.0361
 -11.250  -0.8207   0.01572   0.00967  -0.0765   0.6487   0.0364
 -11.000  -0.7959   0.01532   0.00922  -0.0758   0.6446   0.0369
 -10.750  -0.7708   0.01493   0.00880  -0.0752   0.6407   0.0374
 -10.500  -0.7453   0.01459   0.00842  -0.0746   0.6368   0.0380
 -10.250  -0.7196   0.01429   0.00807  -0.0741   0.6321   0.0385
 -10.000  -0.6934   0.01400   0.00774  -0.0736   0.6276   0.0391
  -9.750  -0.6670   0.01372   0.00742  -0.0731   0.6232   0.0397
  -9.500  -0.6403   0.01346   0.00711  -0.0726   0.6187   0.0403
  -9.250  -0.6135   0.01324   0.00683  -0.0722   0.6142   0.0409
  -9.000  -0.5871   0.01295   0.00651  -0.0717   0.6101   0.0417
  -8.750  -0.5602   0.01268   0.00622  -0.0713   0.6068   0.0426
  -8.500  -0.5330   0.01244   0.00596  -0.0709   0.6030   0.0434
  -8.250  -0.5057   0.01222   0.00571  -0.0705   0.5991   0.0443
  -8.000  -0.4782   0.01203   0.00547  -0.0702   0.5952   0.0452
  -7.750  -0.4507   0.01185   0.00525  -0.0698   0.5909   0.0459
  -7.500  -0.4233   0.01161   0.00500  -0.0695   0.5873   0.0470
  -7.250  -0.3956   0.01140   0.00478  -0.0692   0.5826   0.0481
  -7.000  -0.3678   0.01122   0.00457  -0.0688   0.5775   0.0493
  -6.750  -0.3400   0.01107   0.00438  -0.0685   0.5727   0.0504
  -6.500  -0.3120   0.01090   0.00418  -0.0683   0.5683   0.0516
  -6.250  -0.2841   0.01071   0.00399  -0.0680   0.5626   0.0533
  -6.000  -0.2562   0.01057   0.00381  -0.0677   0.5552   0.0550
  -5.750  -0.2280   0.01044   0.00365  -0.0674   0.5487   0.0564
  -5.500  -0.2000   0.01029   0.00348  -0.0672   0.5408   0.0582
  -5.250  -0.1721   0.01017   0.00333  -0.0669   0.5326   0.0604
  -5.000  -0.1439   0.01006   0.00319  -0.0667   0.5222   0.0625
  -4.750  -0.1161   0.00996   0.00306  -0.0664   0.5092   0.0656
  -4.500  -0.0884   0.00991   0.00294  -0.0661   0.4919   0.0690
  -4.250  -0.0609   0.00987   0.00285  -0.0658   0.4737   0.0732
  -4.000  -0.0333   0.00985   0.00278  -0.0655   0.4585   0.0773
  -3.750  -0.0055   0.00983   0.00273  -0.0652   0.4457   0.0820
  -3.500   0.0225   0.00981   0.00267  -0.0650   0.4361   0.0861
  -3.000   0.0787   0.00979   0.00259  -0.0645   0.4191   0.0935
  -2.750   0.1067   0.00977   0.00255  -0.0643   0.4117   0.0970
  -2.500   0.1348   0.00976   0.00253  -0.0641   0.4057   0.1004
  -2.250   0.1633   0.00974   0.00249  -0.0640   0.4015   0.1029
  -2.000   0.1916   0.00972   0.00246  -0.0638   0.3971   0.1055
  -1.750   0.2197   0.00970   0.00243  -0.0636   0.3923   0.1089
  -1.500   0.2478   0.00971   0.00242  -0.0634   0.3874   0.1117
  -1.250   0.2763   0.00969   0.00240  -0.0633   0.3841   0.1144
  -1.000   0.3046   0.00968   0.00238  -0.0631   0.3801   0.1177
  -0.750   0.3327   0.00966   0.00237  -0.0629   0.3762   0.1216
  -0.500   0.3607   0.00968   0.00238  -0.0627   0.3724   0.1258
  -0.250   0.3886   0.00969   0.00239  -0.0625   0.3687   0.1310
   0.000   0.4168   0.00965   0.00239  -0.0624   0.3665   0.1398
   0.250   0.4448   0.00961   0.00239  -0.0622   0.3635   0.1513
   0.500   0.4726   0.00959   0.00240  -0.0620   0.3599   0.1646
   0.750   0.5000   0.00957   0.00243  -0.0618   0.3563   0.1844
   1.000   0.5272   0.00956   0.00248  -0.0615   0.3525   0.2082
   1.250   0.5548   0.00955   0.00253  -0.0613   0.3499   0.2287
   1.500   0.5828   0.00956   0.00258  -0.0612   0.3478   0.2446
   1.750   0.6106   0.00957   0.00263  -0.0610   0.3453   0.2585
   2.000   0.6383   0.00960   0.00269  -0.0608   0.3426   0.2701
   2.250   0.6659   0.00967   0.00276  -0.0606   0.3395   0.2802
   2.500   0.6930   0.00973   0.00284  -0.0604   0.3362   0.2922
   2.750   0.7203   0.00982   0.00293  -0.0602   0.3328   0.3010
   3.000   0.7479   0.00985   0.00300  -0.0600   0.3308   0.3111
   3.250   0.7754   0.00990   0.00308  -0.0598   0.3287   0.3200
   3.500   0.8027   0.00996   0.00316  -0.0596   0.3263   0.3305
   3.750   0.8296   0.01002   0.00326  -0.0593   0.3237   0.3454
   4.000   0.8561   0.01009   0.00337  -0.0590   0.3210   0.3663
   4.250   0.8823   0.01016   0.00349  -0.0587   0.3182   0.3875
   4.500   0.9083   0.01023   0.00362  -0.0583   0.3155   0.4116
   5.000   0.9602   0.01024   0.00386  -0.0575   0.3114   0.4938
   5.500   1.0485   0.00955   0.00432  -0.0645   0.3060   0.9808
   5.750   1.0839   0.00974   0.00448  -0.0662   0.3032   0.9890
   6.000   1.1153   0.00995   0.00466  -0.0670   0.3001   0.9957
   6.250   1.1507   0.01011   0.00482  -0.0687   0.2980   0.9990
   6.500   1.1807   0.01025   0.00497  -0.0692   0.2960   1.0000
   6.750   1.2039   0.01040   0.00512  -0.0683   0.2941   1.0000
   7.000   1.2268   0.01057   0.00528  -0.0674   0.2919   1.0000
   7.250   1.2492   0.01075   0.00546  -0.0665   0.2896   1.0000
   7.500   1.2711   0.01095   0.00565  -0.0654   0.2870   1.0000
   7.750   1.2924   0.01118   0.00587  -0.0643   0.2842   1.0000
   8.000   1.3144   0.01138   0.00607  -0.0633   0.2823   1.0000
   8.250   1.3368   0.01155   0.00626  -0.0624   0.2808   1.0000
   8.500   1.3586   0.01173   0.00646  -0.0614   0.2787   1.0000
   8.750   1.3797   0.01194   0.00668  -0.0603   0.2762   1.0000
   9.000   1.3990   0.01221   0.00694  -0.0590   0.2722   1.0000
   9.250   1.4158   0.01256   0.00725  -0.0573   0.2675   1.0000
   9.500   1.4344   0.01278   0.00750  -0.0558   0.2645   1.0000
   9.750   1.4493   0.01304   0.00778  -0.0537   0.2616   1.0000
  10.000   1.4636   0.01336   0.00811  -0.0516   0.2589   1.0000
  10.250   1.4769   0.01379   0.00854  -0.0496   0.2554   1.0000
  10.500   1.4904   0.01431   0.00906  -0.0479   0.2524   1.0000
  10.750   1.5076   0.01474   0.00953  -0.0468   0.2502   1.0000
  11.000   1.5246   0.01523   0.01004  -0.0458   0.2470   1.0000
  11.250   1.5404   0.01581   0.01064  -0.0447   0.2434   1.0000
  11.500   1.5547   0.01652   0.01135  -0.0436   0.2396   1.0000
  11.750   1.5694   0.01725   0.01209  -0.0427   0.2358   1.0000
  12.000   1.5857   0.01790   0.01277  -0.0419   0.2324   1.0000
  12.250   1.6000   0.01870   0.01358  -0.0410   0.2281   1.0000
  12.500   1.6103   0.01981   0.01468  -0.0400   0.2222   1.0000
  12.750   1.6248   0.02065   0.01555  -0.0392   0.2183   1.0000
  13.000   1.6366   0.02171   0.01663  -0.0384   0.2130   1.0000
  13.250   1.6451   0.02304   0.01795  -0.0375   0.2072   1.0000
  13.500   1.6554   0.02426   0.01918  -0.0367   0.2013   1.0000
  13.750   1.6607   0.02588   0.02080  -0.0358   0.1950   1.0000
  14.000   1.6689   0.02730   0.02223  -0.0350   0.1893   1.0000
  14.250   1.6709   0.02921   0.02414  -0.0341   0.1820   1.0000
  14.500   1.6695   0.03146   0.02637  -0.0331   0.1718   1.0000
  14.750   1.6648   0.03401   0.02891  -0.0321   0.1622   1.0000
  15.000   1.6578   0.03692   0.03179  -0.0312   0.1527   1.0000
  15.250   1.6485   0.04012   0.03498  -0.0304   0.1431   1.0000
  15.500   1.6372   0.04364   0.03849  -0.0298   0.1327   1.0000
  15.750   1.6226   0.04762   0.04246  -0.0293   0.1222   1.0000
  16.000   1.6044   0.05213   0.04696  -0.0291   0.1116   1.0000
  16.250   1.5898   0.05640   0.05126  -0.0290   0.1041   1.0000
  16.500   1.5720   0.06119   0.05608  -0.0291   0.0972   1.0000
  17.000   1.5356   0.07125   0.06622  -0.0300   0.0854   1.0000
  17.250   1.5213   0.07598   0.07100  -0.0305   0.0820   1.0000
  17.500   1.5088   0.08051   0.07560  -0.0311   0.0792   1.0000
  17.750   1.4978   0.08488   0.08002  -0.0318   0.0765   1.0000
  18.000   1.4870   0.08931   0.08450  -0.0325   0.0745   1.0000
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