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GOE 433 AIRFOIL (goe433-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: GOE 433 AIRFOIL (goe433-il)
Reynolds number: 100,000
Max Cl/Cd: 48.24 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe433-il-100000.txt
Download as CSV file: xf-goe433-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 433 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.2297   0.12526   0.11987  -0.0414   1.0000   0.1747
 -10.750  -0.2612   0.12616   0.12089  -0.0393   1.0000   0.1794
 -10.500  -0.3339   0.12953   0.12446  -0.0372   1.0000   0.1808
 -10.250  -0.3115   0.12523   0.12018  -0.0339   1.0000   0.1818
 -10.000  -0.3024   0.12332   0.11832  -0.0305   1.0000   0.1831
  -9.750  -0.2718   0.11993   0.11490  -0.0324   0.9966   0.1869
  -9.500  -0.2964   0.11793   0.11292  -0.0438   0.9876   0.1970
  -9.250  -0.2530   0.11193   0.10688  -0.0453   0.9842   0.1989
  -9.000  -0.2101   0.10786   0.10275  -0.0481   0.9805   0.2025
  -8.750  -0.2283   0.10576   0.10066  -0.0586   0.9687   0.2139
  -8.500  -0.1821   0.10011   0.09497  -0.0604   0.9664   0.2164
  -8.250  -0.1373   0.09632   0.09112  -0.0637   0.9639   0.2209
  -8.000  -0.2867   0.06517   0.05976  -0.0992   0.9327   0.1648
  -7.750  -0.3074   0.05262   0.04684  -0.1127   0.9169   0.1631
  -7.500  -0.3135   0.04243   0.03565  -0.1242   0.9024   0.1649
  -7.250  -0.2738   0.04073   0.03404  -0.1269   0.8978   0.1685
  -7.000  -0.2452   0.03951   0.03276  -0.1282   0.8897   0.1719
  -6.750  -0.2171   0.03689   0.02976  -0.1314   0.8815   0.1763
  -6.500  -0.1785   0.03395   0.02626  -0.1361   0.8771   0.1820
  -6.250  -0.1585   0.03339   0.02578  -0.1352   0.8665   0.1855
  -6.000  -0.1230   0.03227   0.02454  -0.1370   0.8608   0.1910
  -5.750  -0.0836   0.03052   0.02238  -0.1399   0.8569   0.1984
  -5.500  -0.0659   0.03029   0.02225  -0.1386   0.8456   0.2028
  -5.250  -0.0303   0.02933   0.02112  -0.1400   0.8402   0.2106
  -5.000  -0.0004   0.02855   0.02026  -0.1405   0.8337   0.2181
  -4.750   0.0242   0.02829   0.01999  -0.1402   0.8248   0.2259
  -4.500   0.0588   0.02742   0.01900  -0.1412   0.8197   0.2356
  -4.250   0.0846   0.02727   0.01884  -0.1409   0.8122   0.2453
  -4.000   0.1113   0.02691   0.01847  -0.1409   0.8043   0.2551
  -3.750   0.1454   0.02641   0.01780  -0.1416   0.7994   0.2679
  -3.500   0.1691   0.02634   0.01789  -0.1409   0.7916   0.2775
  -3.250   0.1969   0.02610   0.01754  -0.1410   0.7841   0.2902
  -3.000   0.2294   0.02567   0.01714  -0.1412   0.7792   0.3039
  -2.750   0.2527   0.02571   0.01727  -0.1407   0.7711   0.3158
  -2.500   0.2806   0.02553   0.01708  -0.1406   0.7638   0.3312
  -2.250   0.3135   0.02512   0.01666  -0.1408   0.7591   0.3494
  -2.000   0.3358   0.02541   0.01703  -0.1401   0.7504   0.3661
  -1.750   0.3637   0.02535   0.01708  -0.1397   0.7435   0.3843
  -1.500   0.3967   0.02505   0.01679  -0.1396   0.7390   0.4055
  -1.250   0.4170   0.02557   0.01745  -0.1385   0.7294   0.4222
  -1.000   0.4463   0.02555   0.01745  -0.1381   0.7231   0.4423
  -0.750   0.4795   0.02532   0.01720  -0.1379   0.7189   0.4630
  -0.500   0.4981   0.02594   0.01794  -0.1367   0.7084   0.4787
  -0.250   0.5286   0.02576   0.01775  -0.1363   0.7027   0.4980
   0.000   0.5579   0.02571   0.01768  -0.1359   0.6969   0.5163
   0.250   0.5798   0.02610   0.01813  -0.1350   0.6876   0.5333
   0.500   0.6116   0.02579   0.01779  -0.1348   0.6825   0.5524
   0.750   0.6352   0.02609   0.01813  -0.1340   0.6742   0.5701
   1.000   0.6619   0.02610   0.01815  -0.1335   0.6667   0.5886
   1.250   0.6944   0.02574   0.01776  -0.1333   0.6622   0.6084
   1.500   0.7129   0.02639   0.01851  -0.1320   0.6527   0.6268
   1.750   0.7401   0.02630   0.01846  -0.1313   0.6462   0.6471
   2.000   0.7726   0.02594   0.01805  -0.1309   0.6418   0.6676
   2.250   0.7877   0.02678   0.01905  -0.1294   0.6314   0.6831
   2.500   0.8163   0.02668   0.01896  -0.1290   0.6257   0.7000
   2.750   0.8496   0.02641   0.01863  -0.1289   0.6216   0.7176
   3.000   0.8615   0.02748   0.01989  -0.1273   0.6108   0.7320
   3.250   0.8916   0.02735   0.01973  -0.1270   0.6054   0.7497
   3.500   0.9195   0.02751   0.01989  -0.1267   0.6001   0.7678
   3.750   0.9334   0.02855   0.02108  -0.1252   0.5908   0.7850
   4.000   0.9622   0.02843   0.02097  -0.1248   0.5856   0.8057
   4.250   0.9914   0.02832   0.02086  -0.1243   0.5811   0.8295
   4.500   0.9972   0.02964   0.02243  -0.1219   0.5713   0.8574
   4.750   1.0222   0.02935   0.02228  -0.1207   0.5664   0.9211
   5.000   1.0706   0.02900   0.02175  -0.1240   0.5622   1.0000
   5.250   1.0818   0.03069   0.02357  -0.1235   0.5511   1.0000
   5.500   1.1255   0.03000   0.02269  -0.1253   0.5455   1.0000
   5.750   1.1441   0.03084   0.02354  -0.1245   0.5361   1.0000
   6.000   1.1802   0.03016   0.02273  -0.1250   0.5282   1.0000
   6.250   1.2097   0.02998   0.02248  -0.1249   0.5200   1.0000
   6.500   1.2355   0.02989   0.02234  -0.1242   0.5107   1.0000
   6.750   1.2722   0.02924   0.02153  -0.1247   0.5038   1.0000
   7.000   1.2868   0.02990   0.02229  -0.1230   0.4941   1.0000
   7.250   1.3277   0.02903   0.02123  -0.1240   0.4878   1.0000
   7.500   1.3370   0.03005   0.02240  -0.1218   0.4784   1.0000
   7.750   1.3699   0.02970   0.02197  -0.1219   0.4716   1.0000
   8.000   1.3886   0.03023   0.02254  -0.1206   0.4636   1.0000
   8.250   1.4127   0.03029   0.02259  -0.1198   0.4552   1.0000
   8.500   1.4380   0.03034   0.02261  -0.1191   0.4468   1.0000
   8.750   1.4570   0.03058   0.02287  -0.1177   0.4373   1.0000
   9.000   1.4799   0.03074   0.02299  -0.1167   0.4284   1.0000
   9.250   1.4975   0.03110   0.02338  -0.1152   0.4190   1.0000
   9.500   1.5176   0.03146   0.02373  -0.1140   0.4103   1.0000
   9.750   1.5321   0.03198   0.02429  -0.1121   0.4009   1.0000
  10.000   1.5487   0.03247   0.02480  -0.1105   0.3919   1.0000
  10.250   1.5590   0.03306   0.02543  -0.1080   0.3823   1.0000
  10.500   1.5675   0.03379   0.02619  -0.1054   0.3730   1.0000
  10.750   1.5785   0.03433   0.02671  -0.1032   0.3627   1.0000
  11.000   1.5756   0.03564   0.02813  -0.0998   0.3525   1.0000
  11.250   1.5943   0.03589   0.02825  -0.0984   0.3423   1.0000
  11.500   1.5810   0.03800   0.03056  -0.0947   0.3319   1.0000
  11.750   1.5894   0.03898   0.03151  -0.0928   0.3221   1.0000
  12.000   1.5857   0.04084   0.03345  -0.0903   0.3118   1.0000
  12.250   1.5856   0.04264   0.03528  -0.0883   0.3019   1.0000
  12.500   1.5903   0.04405   0.03666  -0.0866   0.2921   1.0000
  12.750   1.5806   0.04682   0.03955  -0.0847   0.2818   1.0000
  13.000   1.5847   0.04842   0.04107  -0.0832   0.2722   1.0000
  13.250   1.5759   0.05142   0.04419  -0.0817   0.2628   1.0000
  13.500   1.5764   0.05358   0.04632  -0.0805   0.2539   1.0000
  13.750   1.5711   0.05643   0.04922  -0.0794   0.2451   1.0000
  14.000   1.5692   0.05904   0.05185  -0.0784   0.2367   1.0000
  14.250   1.5664   0.06179   0.05462  -0.0776   0.2281   1.0000
  14.500   1.5607   0.06503   0.05791  -0.0770   0.2196   1.0000
  14.750   1.5626   0.06730   0.06008  -0.0762   0.2107   1.0000
  15.000   1.5502   0.07159   0.06450  -0.0760   0.2018   1.0000
  15.250   1.5500   0.07422   0.06701  -0.0754   0.1924   1.0000
  15.500   1.5414   0.07808   0.07091  -0.0752   0.1827   1.0000
  15.750   1.5350   0.08174   0.07456  -0.0750   0.1729   1.0000
  16.000   1.5389   0.08391   0.07655  -0.0742   0.1633   1.0000
  16.250   1.5336   0.08755   0.08023  -0.0741   0.1551   1.0000
  16.500   1.5390   0.08972   0.08231  -0.0733   0.1483   1.0000
  16.750   1.5383   0.09288   0.08554  -0.0732   0.1428   1.0000
  17.000   1.5622   0.09247   0.08487  -0.0716   0.1378   1.0000
  17.250   1.5501   0.09738   0.09006  -0.0724   0.1347   1.0000
  17.500   1.5476   0.10095   0.09377  -0.0728   0.1316   1.0000
  17.750   1.5566   0.10280   0.09563  -0.0724   0.1287   1.0000
  18.000   1.5872   0.10160   0.09424  -0.0705   0.1259   1.0000
  18.250   1.5793   0.10605   0.09890  -0.0714   0.1244   1.0000
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