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GOE 234 (MVA CA5) AIRFOIL (goe234-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 234 (MVA CA5) AIRFOIL (goe234-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.05 at α=2.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe234-il-1000000-n5.txt
Download as CSV file: xf-goe234-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 234 (MVA CA5) 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.5303   0.07523   0.07273  -0.0993   0.9196   0.0192
 -14.000  -0.5372   0.07049   0.06788  -0.1027   0.9073   0.0195
 -13.750  -0.5414   0.06621   0.06347  -0.1059   0.8898   0.0197
 -13.500  -0.5433   0.06234   0.05944  -0.1089   0.8705   0.0200
 -13.250  -0.5427   0.05877   0.05573  -0.1119   0.8545   0.0202
 -13.000  -0.5394   0.05569   0.05252  -0.1146   0.8432   0.0205
 -12.750  -0.5318   0.05269   0.04942  -0.1180   0.8353   0.0207
 -12.500  -0.5189   0.04981   0.04643  -0.1220   0.8282   0.0210
 -12.250  -0.5024   0.04720   0.04373  -0.1261   0.8229   0.0212
 -12.000  -0.4836   0.04456   0.04101  -0.1307   0.8178   0.0215
 -11.750  -0.4622   0.04200   0.03839  -0.1356   0.8129   0.0219
 -11.250  -0.4119   0.03767   0.03395  -0.1448   0.8048   0.0227
 -11.000  -0.3837   0.03583   0.03205  -0.1491   0.8011   0.0231
 -10.750  -0.3541   0.03402   0.03018  -0.1536   0.7973   0.0235
 -10.500  -0.3232   0.03232   0.02840  -0.1580   0.7935   0.0240
 -10.250  -0.2914   0.03085   0.02684  -0.1621   0.7898   0.0244
 -10.000  -0.2582   0.02942   0.02534  -0.1663   0.7870   0.0248
  -9.750  -0.2240   0.02801   0.02386  -0.1706   0.7837   0.0251
  -9.500  -0.1885   0.02667   0.02247  -0.1750   0.7800   0.0255
  -9.250  -0.1525   0.02540   0.02115  -0.1794   0.7763   0.0261
  -9.000  -0.1166   0.02428   0.01997  -0.1834   0.7728   0.0266
  -8.750  -0.0803   0.02321   0.01885  -0.1873   0.7694   0.0270
  -8.500  -0.0436   0.02217   0.01777  -0.1911   0.7659   0.0276
  -8.250  -0.0073   0.02128   0.01682  -0.1946   0.7621   0.0281
  -8.000   0.0291   0.02045   0.01593  -0.1979   0.7581   0.0286
  -7.750   0.0655   0.01967   0.01507  -0.2011   0.7538   0.0290
  -7.500   0.1021   0.01889   0.01423  -0.2043   0.7499   0.0293
  -7.250   0.1398   0.01807   0.01335  -0.2078   0.7453   0.0297
  -7.000   0.1789   0.01714   0.01237  -0.2118   0.7406   0.0306
  -6.750   0.2158   0.01642   0.01158  -0.2149   0.7355   0.0313
  -6.500   0.2524   0.01573   0.01084  -0.2178   0.7306   0.0320
  -6.250   0.2888   0.01506   0.01010  -0.2206   0.7241   0.0326
  -6.000   0.3246   0.01444   0.00939  -0.2232   0.7178   0.0333
  -5.750   0.3600   0.01386   0.00875  -0.2255   0.7118   0.0339
  -5.500   0.3948   0.01333   0.00813  -0.2277   0.7042   0.0345
  -5.250   0.4312   0.01263   0.00734  -0.2304   0.6966   0.0357
  -5.000   0.4656   0.01212   0.00677  -0.2324   0.6875   0.0370
  -4.750   0.4992   0.01167   0.00624  -0.2341   0.6793   0.0384
  -4.500   0.5322   0.01129   0.00577  -0.2355   0.6709   0.0397
  -4.250   0.5653   0.01087   0.00526  -0.2371   0.6629   0.0413
  -4.000   0.5979   0.01049   0.00483  -0.2384   0.6540   0.0435
  -3.750   0.6295   0.01023   0.00448  -0.2394   0.6447   0.0458
  -3.500   0.6607   0.01002   0.00419  -0.2402   0.6347   0.0484
  -3.250   0.6916   0.00987   0.00399  -0.2410   0.6257   0.0519
  -3.000   0.7220   0.00979   0.00383  -0.2415   0.6171   0.0554
  -2.750   0.7526   0.00967   0.00368  -0.2421   0.6089   0.0602
  -2.500   0.7827   0.00963   0.00356  -0.2426   0.5997   0.0645
  -2.250   0.8130   0.00954   0.00344  -0.2431   0.5925   0.0712
  -2.000   0.8434   0.00944   0.00330  -0.2436   0.5850   0.0831
  -1.750   0.8753   0.00907   0.00302  -0.2448   0.5774   0.1552
  -1.500   0.9065   0.00874   0.00280  -0.2458   0.5670   0.2333
  -1.250   0.9354   0.00882   0.00285  -0.2460   0.5555   0.2542
  -1.000   0.9639   0.00893   0.00292  -0.2460   0.5442   0.2655
  -0.750   0.9929   0.00900   0.00296  -0.2461   0.5378   0.2707
  -0.500   1.0218   0.00908   0.00303  -0.2462   0.5315   0.2758
  -0.250   1.0503   0.00919   0.00309  -0.2462   0.5248   0.2794
   0.000   1.0791   0.00927   0.00314  -0.2463   0.5181   0.2825
   0.250   1.1074   0.00939   0.00323  -0.2463   0.5099   0.2866
   0.500   1.1358   0.00950   0.00333  -0.2463   0.5029   0.2898
   0.750   1.1640   0.00962   0.00342  -0.2463   0.4950   0.2933
   1.000   1.1920   0.00975   0.00351  -0.2463   0.4880   0.2948
   1.250   1.2202   0.00986   0.00359  -0.2462   0.4799   0.2961
   1.500   1.2478   0.01001   0.00369  -0.2462   0.4716   0.2975
   1.750   1.2756   0.01014   0.00379  -0.2461   0.4625   0.2986
   2.000   1.3029   0.01031   0.00391  -0.2459   0.4529   0.3004
   2.250   1.3300   0.01048   0.00405  -0.2458   0.4415   0.3019
   2.500   1.3569   0.01068   0.00421  -0.2456   0.4298   0.3035
   2.750   1.3831   0.01092   0.00440  -0.2452   0.4162   0.3057
   3.000   1.4081   0.01125   0.00463  -0.2447   0.3959   0.3079
   3.250   1.4317   0.01170   0.00493  -0.2440   0.3703   0.3094
   3.500   1.4555   0.01210   0.00521  -0.2433   0.3477   0.3107
   3.750   1.4794   0.01246   0.00548  -0.2426   0.3303   0.3118
   4.000   1.5031   0.01283   0.00577  -0.2418   0.3149   0.3129
   4.250   1.5266   0.01319   0.00605  -0.2411   0.3009   0.3138
   4.500   1.5492   0.01358   0.00637  -0.2401   0.2859   0.3147
   5.000   1.5944   0.01430   0.00700  -0.2383   0.2613   0.3177
   5.250   1.6165   0.01466   0.00732  -0.2373   0.2532   0.3191
   5.500   1.6394   0.01493   0.00760  -0.2364   0.2478   0.3205
   5.750   1.6613   0.01523   0.00790  -0.2353   0.2422   0.3219
   6.250   1.7017   0.01594   0.00859  -0.2326   0.2293   0.3247
   6.500   1.7191   0.01639   0.00901  -0.2307   0.2213   0.3262
   6.750   1.7360   0.01677   0.00940  -0.2287   0.2162   0.3276
   7.000   1.7514   0.01714   0.00978  -0.2264   0.2130   0.3287
   7.250   1.7683   0.01757   0.01023  -0.2245   0.2093   0.3296
   7.500   1.7840   0.01811   0.01077  -0.2224   0.2041   0.3306
   7.750   1.8009   0.01861   0.01129  -0.2207   0.1988   0.3322
   8.000   1.8165   0.01919   0.01188  -0.2187   0.1920   0.3336
   8.250   1.8306   0.01989   0.01257  -0.2166   0.1849   0.3349
   8.500   1.8428   0.02072   0.01336  -0.2143   0.1731   0.3361
   8.750   1.8376   0.02268   0.01507  -0.2095   0.1337   0.3370
   9.000   1.8267   0.02516   0.01735  -0.2043   0.0992   0.3377
   9.250   1.8279   0.02694   0.01906  -0.2010   0.0824   0.3388
   9.500   1.8205   0.02947   0.02143  -0.1968   0.0522   0.3396
   9.750   1.8189   0.03167   0.02357  -0.1935   0.0354   0.3407
  10.000   1.8274   0.03311   0.02505  -0.1915   0.0322   0.3421
  10.250   1.8366   0.03451   0.02648  -0.1897   0.0306   0.3434
  10.500   1.8450   0.03601   0.02803  -0.1878   0.0292   0.3444
  10.750   1.8533   0.03755   0.02961  -0.1860   0.0279   0.3453
  11.000   1.8631   0.03897   0.03108  -0.1844   0.0273   0.3461
  11.250   1.8714   0.04056   0.03274  -0.1827   0.0266   0.3475
  11.500   1.8793   0.04220   0.03444  -0.1811   0.0258   0.3488
  11.750   1.8860   0.04401   0.03631  -0.1794   0.0251   0.3501
  12.000   1.8921   0.04591   0.03827  -0.1778   0.0243   0.3513
  12.250   1.8972   0.04796   0.04038  -0.1762   0.0235   0.3524
  12.500   1.9033   0.04995   0.04244  -0.1747   0.0230   0.3537
  12.750   1.9102   0.05185   0.04441  -0.1734   0.0225   0.3551
  13.000   1.9155   0.05398   0.04660  -0.1720   0.0220   0.3565
  13.250   1.9204   0.05617   0.04886  -0.1707   0.0214   0.3579
  13.500   1.9245   0.05851   0.05126  -0.1694   0.0208   0.3591
  13.750   1.9273   0.06105   0.05386  -0.1682   0.0201   0.3602
  14.000   1.9289   0.06374   0.05662  -0.1670   0.0195   0.3610
  14.250   1.9315   0.06634   0.05929  -0.1660   0.0189   0.3618
  14.500   1.9341   0.06902   0.06204  -0.1650   0.0185   0.3632
  14.750   1.9361   0.07177   0.06487  -0.1641   0.0179   0.3645
  15.000   1.9373   0.07465   0.06783  -0.1632   0.0174   0.3656
  15.250   1.9371   0.07777   0.07102  -0.1624   0.0168   0.3668
  15.500   1.9363   0.08095   0.07427  -0.1616   0.0163   0.3680
  15.750   1.9343   0.08430   0.07770  -0.1609   0.0157   0.3692
  16.000   1.9326   0.08767   0.08115  -0.1604   0.0154   0.3704
  16.250   1.9311   0.09103   0.08459  -0.1599   0.0149   0.3718
  16.500   1.9288   0.09452   0.08816  -0.1594   0.0143   0.3732
  16.750   1.9251   0.09826   0.09198  -0.1591   0.0138   0.3744
  17.000   1.9211   0.10202   0.09581  -0.1589   0.0133   0.3755
  17.250   1.9164   0.10590   0.09977  -0.1588   0.0129   0.3764
  17.500   1.9109   0.10998   0.10393  -0.1589   0.0126   0.3771
  17.750   1.9066   0.11389   0.10794  -0.1590   0.0123   0.3784
  18.000   1.9023   0.11783   0.11198  -0.1593   0.0120   0.3796
  18.250   1.8965   0.12205   0.11629  -0.1598   0.0116   0.3808
  18.500   1.8909   0.12627   0.12059  -0.1604   0.0113   0.3819
  18.750   1.8854   0.13043   0.12483  -0.1611   0.0110   0.3831
  19.000   1.8787   0.13488   0.12937  -0.1621   0.0107   0.3842
  19.250   1.8720   0.13938   0.13396  -0.1632   0.0104   0.3854
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