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GOE 531 AIRFOIL (goe531-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 531 AIRFOIL (goe531-il)
Reynolds number: 1,000,000
Max Cl/Cd: 100.82 at α=2°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe531-il-1000000.txt
Download as CSV file: xf-goe531-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 531 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500   0.6560   0.09170   0.08761  -0.2468   0.6809   0.0300
 -11.250   0.6658   0.09013   0.08604  -0.2474   0.6799   0.0305
 -11.000   0.6752   0.08854   0.08445  -0.2480   0.6790   0.0307
 -10.750   0.6843   0.08695   0.08286  -0.2486   0.6779   0.0313
 -10.500   0.6929   0.08536   0.08126  -0.2491   0.6768   0.0316
 -10.250   0.7011   0.08380   0.07970  -0.2496   0.6755   0.0318
 -10.000   0.7086   0.08230   0.07818  -0.2502   0.6741   0.0319
  -9.750   0.7168   0.08083   0.07670  -0.2509   0.6723   0.0320
  -9.500   0.7270   0.07934   0.07520  -0.2519   0.6706   0.0320
  -9.250   0.7332   0.07790   0.07378  -0.2522   0.6700   0.0321
  -9.000   0.7390   0.07649   0.07239  -0.2522   0.6695   0.0321
  -8.750   0.7441   0.07506   0.07100  -0.2522   0.6689   0.0321
  -8.500   0.7527   0.07306   0.06902  -0.2519   0.6682   0.0323
  -8.250   0.7624   0.07163   0.06761  -0.2516   0.6674   0.0323
  -8.000   0.7721   0.07036   0.06635  -0.2513   0.6666   0.0324
  -7.750   0.7807   0.06917   0.06519  -0.2508   0.6655   0.0326
  -7.500   0.7892   0.06808   0.06411  -0.2504   0.6645   0.0328
  -7.250   0.7965   0.06697   0.06302  -0.2497   0.6634   0.0329
  -7.000   0.8036   0.06593   0.06199  -0.2490   0.6623   0.0332
  -6.750   0.8095   0.06486   0.06094  -0.2482   0.6612   0.0334
  -6.500   0.8147   0.06383   0.05993  -0.2471   0.6602   0.0339
  -6.250   0.8183   0.06281   0.05893  -0.2458   0.6591   0.0343
  -6.000   0.8205   0.06181   0.05794  -0.2442   0.6579   0.0347
  -5.750   0.8206   0.06084   0.05698  -0.2423   0.6565   0.0353
  -5.500   0.8133   0.05995   0.05611  -0.2394   0.6547   0.0359
  -5.250   0.8108   0.05895   0.05511  -0.2389   0.6525   0.0362
  -5.000   0.8080   0.05798   0.05419  -0.2367   0.6519   0.0362
  -4.750   0.8049   0.05704   0.05329  -0.2341   0.6512   0.0362
  -4.500   0.7967   0.05629   0.05259  -0.2300   0.6503   0.0362
  -4.250   0.7931   0.05532   0.05166  -0.2271   0.6493   0.0363
  -4.000   0.7901   0.05383   0.05021  -0.2240   0.6482   0.0365
  -3.750   0.7915   0.05290   0.04931  -0.2215   0.6470   0.0366
  -3.500   0.7952   0.05203   0.04846  -0.2193   0.6458   0.0367
  -3.250   0.8007   0.05108   0.04753  -0.2177   0.6446   0.0368
  -3.000   0.8064   0.05016   0.04662  -0.2161   0.6433   0.0370
  -2.750   0.8841   0.02220   0.01783  -0.2629   0.6420   0.0331
  -2.500   0.9169   0.01910   0.01446  -0.2678   0.6408   0.0334
  -2.250   0.9449   0.01743   0.01259  -0.2698   0.6395   0.0335
  -2.000   0.9731   0.01626   0.01125  -0.2714   0.6381   0.0338
  -1.750   1.0039   0.01531   0.01014  -0.2731   0.6365   0.0340
  -1.500   1.0351   0.01458   0.00927  -0.2748   0.6350   0.0343
  -1.250   1.0535   0.01408   0.00869  -0.2736   0.6344   0.0345
  -1.000   1.0723   0.01370   0.00824  -0.2723   0.6336   0.0346
  -0.750   1.0908   0.01351   0.00801  -0.2709   0.6327   0.0349
  -0.500   1.1093   0.01339   0.00785  -0.2694   0.6316   0.0350
  -0.250   1.1287   0.01329   0.00771  -0.2681   0.6304   0.0352
   0.000   1.1487   0.01322   0.00760  -0.2669   0.6291   0.0355
   0.250   1.1690   0.01318   0.00753  -0.2658   0.6278   0.0357
   0.500   1.1884   0.01316   0.00746  -0.2644   0.6264   0.0360
   0.750   1.2085   0.01317   0.00744  -0.2633   0.6251   0.0362
   1.000   1.2291   0.01316   0.00740  -0.2622   0.6239   0.0367
   1.250   1.2513   0.01314   0.00734  -0.2614   0.6225   0.0381
   1.500   1.2753   0.01317   0.00734  -0.2610   0.6211   0.0391
   1.750   1.3033   0.01318   0.00730  -0.2613   0.6194   0.0419
   2.000   1.3318   0.01321   0.00740  -0.2618   0.6178   0.0613
   2.250   1.3456   0.01349   0.00772  -0.2595   0.6170   0.0676
   2.500   1.3594   0.01378   0.00806  -0.2572   0.6159   0.0707
   2.750   1.3756   0.01403   0.00832  -0.2554   0.6147   0.0726
   3.000   1.3923   0.01424   0.00854  -0.2538   0.6133   0.0746
   3.250   1.4086   0.01448   0.00881  -0.2521   0.6118   0.0764
   3.500   1.4264   0.01469   0.00904  -0.2506   0.6103   0.0780
   3.750   1.4448   0.01489   0.00923  -0.2493   0.6088   0.0792
   4.000   1.4631   0.01511   0.00945  -0.2480   0.6073   0.0803
   4.250   1.4822   0.01527   0.00960  -0.2468   0.6058   0.0816
   4.500   1.5039   0.01541   0.00975  -0.2461   0.6042   0.0835
   4.750   1.5314   0.01547   0.00980  -0.2465   0.6023   0.0852
   5.000   1.5497   0.01575   0.01009  -0.2453   0.6005   0.0871
   5.250   1.5585   0.01623   0.01061  -0.2424   0.5991   0.0883
   5.500   1.5695   0.01668   0.01110  -0.2400   0.5975   0.0889
   5.750   1.5807   0.01711   0.01156  -0.2376   0.5955   0.0912
   6.000   1.5957   0.01747   0.01195  -0.2359   0.5936   0.0922
   6.250   1.6114   0.01783   0.01233  -0.2343   0.5917   0.0935
   6.500   1.6260   0.01825   0.01276  -0.2326   0.5899   0.0949
   6.750   1.6446   0.01854   0.01305  -0.2315   0.5879   0.0963
   7.000   1.6689   0.01866   0.01316  -0.2314   0.5860   0.0977
   7.250   1.6898   0.01890   0.01341  -0.2307   0.5839   0.1016
   7.500   1.6960   0.01968   0.01426  -0.2278   0.5824   0.1039
   7.750   1.6932   0.02087   0.01551  -0.2235   0.5788   0.1071
   8.000   1.7063   0.02145   0.01615  -0.2217   0.5768   0.1180
   8.250   1.7158   0.02219   0.01699  -0.2194   0.5741   0.1610
   8.500   1.7315   0.02268   0.01752  -0.2181   0.5718   0.1857
   8.750   1.7533   0.02289   0.01773  -0.2176   0.5695   0.1999
   9.000   1.7712   0.02331   0.01818  -0.2167   0.5671   0.2090
   9.250   1.7668   0.02493   0.01987  -0.2126   0.5643   0.2131
   9.500   1.7722   0.02608   0.02109  -0.2100   0.5614   0.2199
   9.750   1.7799   0.02714   0.02218  -0.2078   0.5587   0.2259
  10.000   1.7918   0.02795   0.02300  -0.2061   0.5561   0.2305
  10.250   1.8100   0.02836   0.02343  -0.2053   0.5538   0.2386
  10.500   1.8361   0.02829   0.02334  -0.2056   0.5511   0.2452
  10.750   1.8265   0.03052   0.02566  -0.2013   0.5482   0.2473
  11.000   1.8280   0.03209   0.02729  -0.1985   0.5451   0.2512
  11.250   1.8292   0.03371   0.02896  -0.1957   0.5411   0.2566
  11.500   1.8429   0.03445   0.02970  -0.1944   0.5377   0.2623
  11.750   1.8670   0.03444   0.02966  -0.1944   0.5344   0.2681
  12.000   1.8487   0.03754   0.03289  -0.1895   0.5301   0.2717
  12.250   1.8488   0.03936   0.03476  -0.1868   0.5258   0.2761
  12.500   1.8589   0.04040   0.03581  -0.1852   0.5219   0.2820
  12.750   1.8781   0.04074   0.03613  -0.1847   0.5183   0.2897
  13.000   1.8645   0.04370   0.03919  -0.1806   0.5134   0.2925
  13.250   1.8588   0.04606   0.04159  -0.1775   0.5072   0.2964
  13.500   1.8702   0.04701   0.04254  -0.1762   0.5030   0.3015
  13.750   1.8703   0.04896   0.04454  -0.1738   0.4976   0.3068
  14.000   1.8650   0.05139   0.04704  -0.1708   0.4919   0.3121
  14.250   1.8715   0.05278   0.04840  -0.1691   0.4853   0.3186
  14.500   1.8690   0.05503   0.05073  -0.1666   0.4784   0.3260
  14.750   1.8635   0.05750   0.05320  -0.1638   0.4698   0.3321
  15.000   1.8635   0.05956   0.05530  -0.1616   0.4615   0.3433
  15.250   1.8522   0.06261   0.05834  -0.1584   0.4490   0.3544
  15.500   1.8378   0.06599   0.06168  -0.1549   0.4297   0.3676
  15.750   1.7921   0.07231   0.06781  -0.1488   0.3925   0.3633
  16.000   1.7343   0.08017   0.07541  -0.1422   0.3522   0.3533
  16.250   1.8057   0.09568   0.09155  -0.1684   0.3103   1.0000
  16.500   1.8025   0.09845   0.09430  -0.1666   0.3009   1.0000
  16.750   1.7993   0.10123   0.09706  -0.1649   0.2929   1.0000
  17.000   1.8032   0.10320   0.09903  -0.1637   0.2851   1.0000
  17.250   1.8013   0.10584   0.10162  -0.1621   0.2756   1.0000
  17.500   1.8006   0.10838   0.10417  -0.1607   0.2660   1.0000
  17.750   1.7990   0.11101   0.10675  -0.1593   0.2540   1.0000
  18.000   1.7942   0.11400   0.10965  -0.1578   0.2363   1.0000
  18.250   1.7780   0.11833   0.11382  -0.1558   0.2098   1.0000
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