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GOE 195 AIRFOIL (goe195-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 195 AIRFOIL (goe195-il)
Reynolds number: 200,000
Max Cl/Cd: 84.03 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe195-il-200000-n5.txt
Download as CSV file: xf-goe195-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 195 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.2561   0.10262   0.09918  -0.0352   1.0000   0.0342
  -9.500  -0.2650   0.09977   0.09638  -0.0360   1.0000   0.0346
  -9.250  -0.2710   0.09683   0.09347  -0.0361   1.0000   0.0347
  -9.000  -0.2770   0.09394   0.09063  -0.0358   1.0000   0.0348
  -8.750  -0.2680   0.08999   0.08670  -0.0346   0.9992   0.0356
  -8.500  -0.2517   0.08654   0.08325  -0.0357   0.9969   0.0365
  -8.250  -0.2386   0.08270   0.07939  -0.0381   0.9944   0.0374
  -8.000  -0.2282   0.07879   0.07548  -0.0407   0.9906   0.0386
  -7.750  -0.2181   0.07454   0.07123  -0.0440   0.9868   0.0399
  -7.500  -0.2227   0.06874   0.06545  -0.0534   0.9773   0.0435
  -7.250  -0.2108   0.06322   0.05992  -0.0598   0.9713   0.0437
  -7.000  -0.1980   0.05953   0.05625  -0.0583   0.9675   0.0450
  -6.750  -0.2590   0.06804   0.06451  -0.0625   0.9756   0.0343
  -6.500  -0.2363   0.06387   0.06031  -0.0675   0.9701   0.0335
  -6.250  -0.2054   0.05759   0.05396  -0.0775   0.9645   0.0330
  -6.000  -0.1530   0.04036   0.03634  -0.1041   0.9567   0.0334
  -5.750  -0.1050   0.02978   0.02483  -0.1195   0.9514   0.0333
  -5.500  -0.0657   0.02591   0.02034  -0.1248   0.9481   0.0337
  -5.250  -0.0354   0.02413   0.01808  -0.1264   0.9406   0.0346
  -5.000  -0.0013   0.02200   0.01553  -0.1287   0.9358   0.0351
  -4.750   0.0313   0.02021   0.01343  -0.1302   0.9301   0.0353
  -4.500   0.0616   0.01880   0.01180  -0.1311   0.9223   0.0357
  -4.250   0.0954   0.01760   0.01040  -0.1325   0.9172   0.0361
  -4.000   0.1236   0.01670   0.00937  -0.1326   0.9075   0.0365
  -3.750   0.1559   0.01588   0.00845  -0.1335   0.9012   0.0373
  -3.500   0.1844   0.01527   0.00776  -0.1336   0.8912   0.0385
  -3.250   0.2146   0.01465   0.00706  -0.1339   0.8821   0.0393
  -3.000   0.2448   0.01405   0.00638  -0.1341   0.8725   0.0397
  -2.750   0.2737   0.01355   0.00583  -0.1342   0.8614   0.0402
  -2.500   0.3030   0.01311   0.00533  -0.1342   0.8501   0.0408
  -2.250   0.3323   0.01273   0.00488  -0.1343   0.8381   0.0415
  -2.000   0.3614   0.01242   0.00449  -0.1343   0.8247   0.0422
  -1.750   0.3903   0.01217   0.00414  -0.1342   0.8107   0.0430
  -1.500   0.4189   0.01197   0.00383  -0.1341   0.7965   0.0441
  -1.250   0.4473   0.01174   0.00352  -0.1340   0.7823   0.0471
  -1.000   0.4755   0.01161   0.00329  -0.1338   0.7677   0.0501
  -0.750   0.5034   0.01153   0.00310  -0.1335   0.7532   0.0531
  -0.500   0.5313   0.01140   0.00296  -0.1333   0.7391   0.0640
  -0.250   0.5589   0.01098   0.00299  -0.1334   0.7250   0.2067
   0.000   0.5862   0.01102   0.00304  -0.1331   0.7106   0.2477
   0.250   0.6134   0.01109   0.00308  -0.1327   0.6959   0.2737
   0.500   0.6404   0.01115   0.00313  -0.1324   0.6806   0.2969
   0.750   0.6673   0.01120   0.00316  -0.1320   0.6644   0.3155
   1.000   0.6941   0.01123   0.00321  -0.1317   0.6474   0.3355
   1.250   0.7207   0.01125   0.00325  -0.1313   0.6297   0.3577
   1.500   0.7467   0.01127   0.00332  -0.1308   0.6094   0.3926
   1.750   0.7724   0.01131   0.00342  -0.1303   0.5886   0.4457
   2.000   0.7976   0.01132   0.00354  -0.1296   0.5717   0.5305
   2.250   0.8228   0.01125   0.00365  -0.1290   0.5603   0.6424
   2.500   0.8470   0.01086   0.00369  -0.1278   0.5509   1.0000
   2.750   0.8739   0.01108   0.00383  -0.1275   0.5428   1.0000
   3.000   0.9004   0.01133   0.00399  -0.1271   0.5332   1.0000
   3.250   0.9268   0.01157   0.00418  -0.1267   0.5218   1.0000
   3.500   0.9530   0.01182   0.00437  -0.1263   0.5108   1.0000
   3.750   0.9792   0.01208   0.00458  -0.1259   0.5011   1.0000
   4.000   1.0057   0.01229   0.00480  -0.1256   0.4913   1.0000
   4.250   1.0316   0.01253   0.00503  -0.1251   0.4797   1.0000
   4.500   1.0572   0.01276   0.00524  -0.1246   0.4654   1.0000
   4.750   1.0824   0.01297   0.00547  -0.1240   0.4476   1.0000
   5.000   1.1073   0.01321   0.00568  -0.1234   0.4263   1.0000
   5.250   1.1319   0.01347   0.00591  -0.1227   0.4040   1.0000
   5.500   1.1555   0.01380   0.00617  -0.1219   0.3759   1.0000
   5.750   1.1777   0.01426   0.00650  -0.1209   0.3412   1.0000
   6.000   1.1990   0.01483   0.00691  -0.1198   0.3071   1.0000
   6.250   1.2198   0.01547   0.00740  -0.1187   0.2747   1.0000
   6.500   1.2407   0.01611   0.00794  -0.1176   0.2464   1.0000
   6.750   1.2617   0.01674   0.00849  -0.1165   0.2233   1.0000
   7.000   1.2821   0.01742   0.00907  -0.1154   0.1968   1.0000
   7.250   1.3012   0.01820   0.00972  -0.1141   0.1641   1.0000
   7.500   1.3190   0.01910   0.01045  -0.1127   0.1333   1.0000
   7.750   1.3364   0.01999   0.01123  -0.1112   0.1123   1.0000
   8.000   1.3540   0.02084   0.01203  -0.1097   0.0954   1.0000
   8.250   1.3716   0.02166   0.01282  -0.1082   0.0767   1.0000
   8.500   1.3863   0.02270   0.01372  -0.1063   0.0528   1.0000
   8.750   1.3996   0.02379   0.01474  -0.1042   0.0438   1.0000
   9.000   1.4131   0.02480   0.01579  -0.1021   0.0395   1.0000
   9.250   1.4253   0.02577   0.01686  -0.0998   0.0367   1.0000
   9.500   1.4338   0.02692   0.01808  -0.0970   0.0342   1.0000
   9.750   1.4400   0.02825   0.01950  -0.0941   0.0321   1.0000
  10.000   1.4495   0.02936   0.02075  -0.0917   0.0307   1.0000
  10.250   1.4573   0.03063   0.02217  -0.0892   0.0291   1.0000
  10.500   1.4633   0.03208   0.02373  -0.0868   0.0276   1.0000
  10.750   1.4664   0.03382   0.02555  -0.0843   0.0262   1.0000
  11.000   1.4639   0.03611   0.02793  -0.0815   0.0251   1.0000
  11.250   1.4705   0.03773   0.02969  -0.0797   0.0243   1.0000
  11.500   1.4752   0.03959   0.03170  -0.0779   0.0233   1.0000
  11.750   1.4787   0.04163   0.03387  -0.0763   0.0223   1.0000
  12.000   1.4817   0.04380   0.03617  -0.0749   0.0213   1.0000
  12.250   1.4838   0.04613   0.03860  -0.0737   0.0205   1.0000
  12.500   1.4838   0.04875   0.04131  -0.0726   0.0198   1.0000
  12.750   1.4807   0.05182   0.04444  -0.0716   0.0192   1.0000
  13.000   1.4828   0.05441   0.04722  -0.0707   0.0187   1.0000
  13.250   1.4831   0.05726   0.05022  -0.0700   0.0181   1.0000
  13.500   1.4827   0.06025   0.05337  -0.0694   0.0176   1.0000
  13.750   1.4817   0.06337   0.05663  -0.0689   0.0171   1.0000
  14.000   1.4801   0.06662   0.06003  -0.0687   0.0166   1.0000
  14.250   1.4782   0.07001   0.06356  -0.0688   0.0161   1.0000
  14.500   1.4758   0.07358   0.06724  -0.0690   0.0157   1.0000
  14.750   1.4729   0.07730   0.07107  -0.0695   0.0154   1.0000
  15.000   1.4690   0.08121   0.07507  -0.0701   0.0150   1.0000
  15.250   1.4637   0.08532   0.07926  -0.0707   0.0147   1.0000
  15.500   1.4587   0.08967   0.08382  -0.0716   0.0144   1.0000
  15.750   1.4527   0.09424   0.08859  -0.0727   0.0141   1.0000
  16.000   1.4457   0.09903   0.09357  -0.0739   0.0138   1.0000
  16.250   1.4379   0.10408   0.09881  -0.0755   0.0136   1.0000
  16.500   1.4292   0.10941   0.10433  -0.0774   0.0134   1.0000
  16.750   1.4197   0.11507   0.11017  -0.0797   0.0132   1.0000
  17.000   1.4095   0.12102   0.11631  -0.0824   0.0131   1.0000
  17.250   1.3986   0.12731   0.12278  -0.0855   0.0129   1.0000
  17.500   1.3870   0.13399   0.12964  -0.0890   0.0128   1.0000
  17.750   1.3746   0.14114   0.13698  -0.0931   0.0127   1.0000
  18.000   1.3612   0.14888   0.14490  -0.0979   0.0127   1.0000
  18.250   1.3461   0.15741   0.15362  -0.1033   0.0126   1.0000
  18.500   1.3279   0.16729   0.16370  -0.1099   0.0126   1.0000
  18.750   1.3030   0.18003   0.17665  -0.1187   0.0128   1.0000
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