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GOE 527 AIRFOIL (goe527-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 527 AIRFOIL (goe527-il)
Reynolds number: 1,000,000
Max Cl/Cd: 128.85 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe527-il-1000000.txt
Download as CSV file: xf-goe527-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 527 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7118   0.06691   0.06435  -0.0895   1.0000   0.0257
 -15.500  -0.7694   0.05521   0.05244  -0.0978   1.0000   0.0257
 -15.250  -0.8028   0.04761   0.04469  -0.1030   1.0000   0.0257
 -15.000  -0.8259   0.04179   0.03874  -0.1071   0.9998   0.0256
 -14.750  -0.8348   0.03328   0.02993  -0.1202   0.9949   0.0260
 -14.500  -0.8258   0.03012   0.02664  -0.1244   0.9872   0.0262
 -14.250  -0.8069   0.02814   0.02460  -0.1273   0.9813   0.0265
 -13.750  -0.7648   0.02549   0.02180  -0.1302   0.9617   0.0270
 -13.500  -0.7295   0.02419   0.02040  -0.1338   0.9549   0.0273
 -13.250  -0.6947   0.02295   0.01904  -0.1370   0.9432   0.0277
 -13.000  -0.6613   0.02192   0.01786  -0.1397   0.9275   0.0281
 -12.750  -0.6369   0.02124   0.01703  -0.1400   0.9084   0.0285
 -12.500  -0.6204   0.02060   0.01622  -0.1387   0.8895   0.0287
 -12.250  -0.6053   0.02003   0.01550  -0.1369   0.8726   0.0290
 -12.000  -0.5893   0.01952   0.01486  -0.1351   0.8571   0.0291
 -11.750  -0.5724   0.01905   0.01425  -0.1334   0.8430   0.0293
 -11.500  -0.5601   0.01807   0.01310  -0.1313   0.8291   0.0296
 -11.250  -0.5447   0.01726   0.01220  -0.1295   0.8169   0.0300
 -11.000  -0.5264   0.01671   0.01157  -0.1280   0.8060   0.0304
 -10.750  -0.5063   0.01629   0.01108  -0.1267   0.7949   0.0307
 -10.500  -0.4852   0.01589   0.01061  -0.1255   0.7849   0.0310
 -10.000  -0.4414   0.01519   0.00975  -0.1234   0.7651   0.0319
  -9.500  -0.3963   0.01447   0.00886  -0.1213   0.7476   0.0326
  -9.250  -0.3735   0.01413   0.00843  -0.1204   0.7390   0.0329
  -9.000  -0.3496   0.01382   0.00805  -0.1195   0.7314   0.0332
  -8.750  -0.3259   0.01351   0.00766  -0.1187   0.7230   0.0335
  -8.500  -0.3052   0.01290   0.00698  -0.1174   0.7153   0.0342
  -8.250  -0.2816   0.01254   0.00658  -0.1166   0.7073   0.0347
  -8.000  -0.2575   0.01230   0.00628  -0.1157   0.6993   0.0353
  -7.750  -0.2322   0.01204   0.00600  -0.1151   0.6923   0.0359
  -7.500  -0.2074   0.01182   0.00571  -0.1144   0.6846   0.0365
  -7.250  -0.1821   0.01159   0.00543  -0.1137   0.6774   0.0371
  -7.000  -0.1567   0.01139   0.00516  -0.1131   0.6694   0.0376
  -6.750  -0.1322   0.01113   0.00484  -0.1123   0.6616   0.0383
  -6.500  -0.1074   0.01082   0.00451  -0.1116   0.6539   0.0393
  -6.250  -0.0823   0.01065   0.00428  -0.1109   0.6460   0.0401
  -6.000  -0.0561   0.01048   0.00408  -0.1104   0.6388   0.0412
  -5.750  -0.0302   0.01034   0.00389  -0.1098   0.6307   0.0422
  -5.500  -0.0047   0.01015   0.00366  -0.1092   0.6231   0.0437
  -5.250   0.0212   0.00999   0.00348  -0.1087   0.6153   0.0456
  -5.000   0.0470   0.00989   0.00333  -0.1081   0.6079   0.0475
  -4.750   0.0733   0.00972   0.00316  -0.1076   0.6011   0.0504
  -4.500   0.0993   0.00962   0.00303  -0.1071   0.5937   0.0541
  -4.250   0.1256   0.00951   0.00293  -0.1066   0.5871   0.0596
  -4.000   0.1522   0.00942   0.00285  -0.1062   0.5805   0.0660
  -3.750   0.1783   0.00939   0.00280  -0.1057   0.5740   0.0716
  -3.500   0.2057   0.00936   0.00276  -0.1054   0.5687   0.0761
  -3.250   0.2325   0.00930   0.00272  -0.1050   0.5630   0.0811
  -3.000   0.2591   0.00932   0.00269  -0.1046   0.5570   0.0844
  -2.750   0.2858   0.00925   0.00263  -0.1042   0.5524   0.0884
  -2.500   0.3130   0.00921   0.00259  -0.1040   0.5478   0.0920
  -2.250   0.3399   0.00921   0.00256  -0.1036   0.5429   0.0947
  -2.000   0.3656   0.00920   0.00251  -0.1031   0.5376   0.0986
  -1.750   0.3929   0.00913   0.00246  -0.1028   0.5340   0.1028
  -1.500   0.4200   0.00910   0.00243  -0.1025   0.5296   0.1062
  -1.250   0.4463   0.00909   0.00239  -0.1021   0.5246   0.1101
  -1.000   0.4718   0.00908   0.00236  -0.1015   0.5190   0.1165
  -0.750   0.4991   0.00902   0.00233  -0.1013   0.5153   0.1233
  -0.500   0.5254   0.00895   0.00230  -0.1009   0.5110   0.1358
  -0.250   0.5500   0.00880   0.00229  -0.1002   0.5063   0.1857
   0.000   0.5738   0.00863   0.00232  -0.0994   0.5010   0.2605
   0.250   0.5989   0.00841   0.00233  -0.0989   0.4968   0.3359
   0.500   0.6232   0.00824   0.00236  -0.0982   0.4923   0.4142
   0.750   0.6470   0.00812   0.00242  -0.0974   0.4882   0.4866
   1.000   0.6701   0.00804   0.00249  -0.0964   0.4840   0.5564
   1.250   0.6936   0.00784   0.00255  -0.0955   0.4813   0.6385
   1.500   0.7133   0.00757   0.00262  -0.0937   0.4781   0.7585
   1.750   0.7383   0.00730   0.00282  -0.0927   0.4744   0.9356
   2.000   0.7906   0.00748   0.00296  -0.0979   0.4696   0.9692
   2.250   0.8351   0.00763   0.00307  -0.1014   0.4653   0.9808
   2.500   0.8811   0.00774   0.00315  -0.1052   0.4604   0.9871
   2.750   0.9238   0.00789   0.00325  -0.1084   0.4546   0.9941
   3.000   0.9663   0.00805   0.00334  -0.1117   0.4488   0.9982
   3.250   1.0040   0.00812   0.00341  -0.1138   0.4446   1.0000
   3.500   1.0245   0.00820   0.00347  -0.1123   0.4403   1.0000
   3.750   1.0435   0.00832   0.00355  -0.1106   0.4355   1.0000
   4.000   1.0630   0.00842   0.00363  -0.1089   0.4311   1.0000
   4.250   1.0838   0.00850   0.00370  -0.1075   0.4261   1.0000
   4.500   1.1023   0.00863   0.00379  -0.1056   0.4194   1.0000
   4.750   1.1213   0.00876   0.00390  -0.1039   0.4137   1.0000
   5.000   1.1416   0.00886   0.00399  -0.1024   0.4078   1.0000
   5.250   1.1598   0.00902   0.00411  -0.1005   0.4014   1.0000
   5.500   1.1796   0.00916   0.00424  -0.0990   0.3956   1.0000
   5.750   1.1977   0.00931   0.00436  -0.0971   0.3888   1.0000
   6.000   1.2118   0.00950   0.00451  -0.0944   0.3818   1.0000
   6.250   1.2294   0.00964   0.00465  -0.0924   0.3749   1.0000
   6.500   1.2434   0.00989   0.00484  -0.0898   0.3664   1.0000
   6.750   1.2617   0.01007   0.00502  -0.0881   0.3586   1.0000
   7.000   1.2765   0.01036   0.00525  -0.0858   0.3490   1.0000
   7.250   1.2932   0.01062   0.00549  -0.0839   0.3390   1.0000
   7.500   1.3085   0.01095   0.00577  -0.0818   0.3282   1.0000
   7.750   1.3223   0.01135   0.00611  -0.0795   0.3172   1.0000
   8.000   1.3385   0.01169   0.00642  -0.0777   0.3074   1.0000
   8.250   1.3531   0.01210   0.00680  -0.0756   0.2980   1.0000
   8.500   1.3669   0.01257   0.00722  -0.0736   0.2882   1.0000
   8.750   1.3827   0.01299   0.00763  -0.0719   0.2803   1.0000
   9.000   1.3961   0.01353   0.00813  -0.0699   0.2722   1.0000
   9.250   1.4116   0.01401   0.00860  -0.0684   0.2651   1.0000
   9.500   1.4254   0.01459   0.00916  -0.0666   0.2584   1.0000
   9.750   1.4399   0.01517   0.00973  -0.0651   0.2526   1.0000
  10.000   1.4559   0.01570   0.01027  -0.0638   0.2480   1.0000
  10.250   1.4694   0.01639   0.01095  -0.0623   0.2432   1.0000
  10.500   1.4830   0.01711   0.01167  -0.0609   0.2386   1.0000
  10.750   1.4996   0.01768   0.01228  -0.0599   0.2357   1.0000
  11.000   1.5145   0.01838   0.01299  -0.0588   0.2323   1.0000
  11.250   1.5276   0.01921   0.01383  -0.0575   0.2286   1.0000
  11.500   1.5385   0.02020   0.01483  -0.0562   0.2247   1.0000
  11.750   1.5539   0.02094   0.01561  -0.0553   0.2221   1.0000
  12.000   1.5686   0.02173   0.01644  -0.0544   0.2192   1.0000
  12.250   1.5809   0.02272   0.01745  -0.0534   0.2158   1.0000
  12.500   1.5883   0.02406   0.01878  -0.0521   0.2106   1.0000
  12.750   1.6008   0.02507   0.01983  -0.0512   0.2073   1.0000
  13.000   1.6139   0.02607   0.02087  -0.0504   0.2039   1.0000
  13.250   1.6226   0.02740   0.02222  -0.0494   0.1993   1.0000
  13.500   1.6273   0.02909   0.02391  -0.0482   0.1943   1.0000
  13.750   1.6403   0.03015   0.02502  -0.0476   0.1906   1.0000
  14.000   1.6491   0.03157   0.02646  -0.0468   0.1864   1.0000
  14.250   1.6518   0.03351   0.02840  -0.0458   0.1806   1.0000
  14.500   1.6609   0.03497   0.02991  -0.0451   0.1760   1.0000
  14.750   1.6638   0.03699   0.03193  -0.0442   0.1692   1.0000
  15.000   1.6663   0.03905   0.03400  -0.0434   0.1624   1.0000
  15.250   1.6646   0.04156   0.03650  -0.0425   0.1543   1.0000
  15.500   1.6653   0.04390   0.03886  -0.0417   0.1481   1.0000
  15.750   1.6592   0.04691   0.04185  -0.0409   0.1405   1.0000
  16.000   1.6575   0.04956   0.04453  -0.0402   0.1355   1.0000
  16.250   1.6526   0.05257   0.04755  -0.0396   0.1307   1.0000
  16.500   1.6510   0.05528   0.05029  -0.0392   0.1269   1.0000
  16.750   1.6492   0.05804   0.05310  -0.0388   0.1239   1.0000
  17.000   1.6458   0.06103   0.05612  -0.0384   0.1212   1.0000
  17.250   1.6427   0.06399   0.05911  -0.0381   0.1186   1.0000
  17.500   1.6417   0.06678   0.06196  -0.0380   0.1166   1.0000
  17.750   1.6436   0.06923   0.06447  -0.0378   0.1151   1.0000
  18.000   1.6425   0.07204   0.06734  -0.0378   0.1132   1.0000
  18.250   1.6408   0.07494   0.07029  -0.0377   0.1113   1.0000
  18.500   1.6348   0.07837   0.07375  -0.0378   0.1086   1.0000
  18.750   1.6269   0.08203   0.07746  -0.0378   0.1061   1.0000
  19.000   1.6314   0.08423   0.07973  -0.0379   0.1049   1.0000
  19.250   1.6321   0.08692   0.08248  -0.0381   0.1029   1.0000
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