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GOE 190 (MVA MK.18) AIRFOIL (goe190-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 190 (MVA MK.18) AIRFOIL (goe190-il)
Reynolds number: 500,000
Max Cl/Cd: 97 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe190-il-500000-n5.txt
Download as CSV file: xf-goe190-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 190 (MVA MK.18) AIRFOIL                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.6616   0.07165   0.06876  -0.0717   0.9947   0.0175
 -13.250  -0.6863   0.06322   0.06017  -0.0787   0.9928   0.0174
 -13.000  -0.6927   0.05802   0.05487  -0.0833   0.9903   0.0178
 -12.750  -0.6987   0.05291   0.04965  -0.0884   0.9874   0.0181
 -12.500  -0.7007   0.04838   0.04501  -0.0937   0.9847   0.0184
 -12.250  -0.7065   0.04429   0.04081  -0.0976   0.9800   0.0187
 -12.000  -0.6962   0.04010   0.03648  -0.1041   0.9759   0.0192
 -11.750  -0.6748   0.03609   0.03232  -0.1121   0.9735   0.0197
 -11.500  -0.6464   0.03291   0.02905  -0.1193   0.9721   0.0203
 -11.250  -0.6314   0.03064   0.02671  -0.1219   0.9683   0.0208
 -11.000  -0.6063   0.02848   0.02445  -0.1258   0.9654   0.0216
 -10.750  -0.5762   0.02639   0.02221  -0.1301   0.9633   0.0224
 -10.500  -0.5423   0.02452   0.02015  -0.1345   0.9616   0.0233
 -10.250  -0.5059   0.02279   0.01832  -0.1390   0.9602   0.0241
 -10.000  -0.4682   0.02146   0.01692  -0.1429   0.9591   0.0249
  -9.750  -0.4384   0.02049   0.01586  -0.1447   0.9570   0.0257
  -9.500  -0.4193   0.01971   0.01500  -0.1440   0.9522   0.0265
  -9.250  -0.3888   0.01891   0.01408  -0.1453   0.9497   0.0274
  -9.000  -0.3554   0.01816   0.01319  -0.1472   0.9477   0.0282
  -8.750  -0.3199   0.01727   0.01227  -0.1495   0.9459   0.0291
  -8.500  -0.2833   0.01669   0.01165  -0.1517   0.9443   0.0301
  -8.250  -0.2649   0.01625   0.01116  -0.1501   0.9386   0.0308
  -8.000  -0.2388   0.01574   0.01058  -0.1500   0.9339   0.0317
  -7.750  -0.2065   0.01519   0.00994  -0.1511   0.9304   0.0326
  -7.500  -0.1820   0.01475   0.00942  -0.1505   0.9244   0.0333
  -7.250  -0.1612   0.01419   0.00882  -0.1492   0.9157   0.0340
  -7.000  -0.1440   0.01372   0.00832  -0.1471   0.9026   0.0348
  -6.500  -0.0691   0.01268   0.00715  -0.1510   0.8696   0.0369
  -6.250  -0.0184   0.01213   0.00640  -0.1556   0.8381   0.0381
  -6.000   0.0156   0.01191   0.00590  -0.1567   0.8004   0.0392
  -5.750   0.0420   0.01180   0.00559  -0.1563   0.7757   0.0399
  -5.250   0.0927   0.01128   0.00483  -0.1553   0.7443   0.0422
  -5.000   0.1186   0.01112   0.00457  -0.1548   0.7322   0.0434
  -4.750   0.1446   0.01098   0.00433  -0.1543   0.7214   0.0447
  -4.500   0.1711   0.01082   0.00410  -0.1539   0.7115   0.0462
  -4.250   0.1974   0.01073   0.00391  -0.1534   0.7016   0.0476
  -4.000   0.2235   0.01052   0.00362  -0.1529   0.6907   0.0497
  -3.750   0.2497   0.01036   0.00341  -0.1525   0.6797   0.0521
  -3.500   0.2757   0.01026   0.00322  -0.1519   0.6666   0.0545
  -3.250   0.3011   0.01020   0.00306  -0.1512   0.6477   0.0569
  -3.000   0.3256   0.01013   0.00287  -0.1503   0.6228   0.0610
  -2.750   0.3496   0.01011   0.00271  -0.1494   0.5937   0.0665
  -2.500   0.3739   0.01009   0.00257  -0.1485   0.5723   0.0764
  -2.000   0.4232   0.00947   0.00226  -0.1474   0.5456   0.2309
  -1.750   0.4493   0.00952   0.00230  -0.1469   0.5369   0.2557
  -1.500   0.4759   0.00958   0.00233  -0.1464   0.5287   0.2684
  -1.250   0.5022   0.00968   0.00235  -0.1459   0.5216   0.2770
  -1.000   0.5292   0.00973   0.00240  -0.1455   0.5159   0.2854
  -0.750   0.5561   0.00982   0.00244  -0.1450   0.5105   0.2933
  -0.250   0.6096   0.00996   0.00255  -0.1442   0.5006   0.3049
   0.000   0.6365   0.01003   0.00257  -0.1438   0.4955   0.3089
   0.250   0.6629   0.01010   0.00265  -0.1433   0.4904   0.3145
   0.500   0.6895   0.01019   0.00272  -0.1428   0.4862   0.3194
   0.750   0.7166   0.01023   0.00276  -0.1425   0.4820   0.3220
   1.000   0.7433   0.01029   0.00280  -0.1420   0.4772   0.3243
   1.250   0.7695   0.01037   0.00285  -0.1415   0.4722   0.3266
   1.500   0.7959   0.01043   0.00292  -0.1411   0.4675   0.3292
   1.750   0.8226   0.01048   0.00299  -0.1406   0.4625   0.3320
   2.000   0.8488   0.01055   0.00307  -0.1401   0.4575   0.3353
   2.250   0.8745   0.01066   0.00315  -0.1395   0.4528   0.3386
   2.500   0.9011   0.01071   0.00322  -0.1391   0.4470   0.3416
   2.750   0.9266   0.01080   0.00330  -0.1385   0.4393   0.3444
   3.000   0.9521   0.01089   0.00340  -0.1379   0.4315   0.3475
   3.250   0.9773   0.01099   0.00350  -0.1372   0.4229   0.3509
   3.500   1.0026   0.01109   0.00362  -0.1365   0.4158   0.3544
   3.750   1.0276   0.01121   0.00372  -0.1358   0.4069   0.3580
   4.000   1.0521   0.01135   0.00384  -0.1351   0.3963   0.3613
   4.250   1.0759   0.01150   0.00399  -0.1342   0.3857   0.3652
   4.500   1.1001   0.01165   0.00415  -0.1333   0.3760   0.3697
   4.750   1.1241   0.01182   0.00431  -0.1325   0.3678   0.3742
   5.000   1.1478   0.01200   0.00449  -0.1316   0.3594   0.3782
   5.250   1.1714   0.01217   0.00468  -0.1307   0.3522   0.3824
   5.500   1.1946   0.01237   0.00488  -0.1297   0.3440   0.3870
   5.750   1.2175   0.01258   0.00509  -0.1287   0.3363   0.3916
   6.000   1.2402   0.01279   0.00532  -0.1276   0.3282   0.3960
   6.250   1.2620   0.01301   0.00556  -0.1264   0.3201   0.4008
   6.500   1.2834   0.01324   0.00580  -0.1251   0.3117   0.4065
   7.000   1.3248   0.01372   0.00631  -0.1223   0.2953   0.4165
   7.250   1.3451   0.01398   0.00659  -0.1208   0.2872   0.4217
   7.500   1.3650   0.01426   0.00688  -0.1193   0.2784   0.4268
   7.750   1.3848   0.01454   0.00719  -0.1178   0.2689   0.4316
   8.000   1.4032   0.01489   0.00754  -0.1161   0.2577   0.4371
   8.250   1.4221   0.01523   0.00788  -0.1145   0.2469   0.4428
   8.500   1.4400   0.01560   0.00826  -0.1127   0.2347   0.4484
   8.750   1.4566   0.01604   0.00868  -0.1108   0.2206   0.4541
   9.000   1.4721   0.01654   0.00915  -0.1087   0.2061   0.4596
   9.250   1.4848   0.01718   0.00972  -0.1063   0.1880   0.4644
   9.500   1.4979   0.01780   0.01030  -0.1039   0.1743   0.4701
   9.750   1.5104   0.01846   0.01094  -0.1015   0.1620   0.4760
  10.000   1.5226   0.01912   0.01159  -0.0991   0.1508   0.4825
  10.250   1.5343   0.01981   0.01228  -0.0967   0.1417   0.4892
  10.500   1.5471   0.02045   0.01295  -0.0945   0.1314   0.4960
  10.750   1.5575   0.02123   0.01372  -0.0920   0.1200   0.5033
  11.000   1.5651   0.02219   0.01465  -0.0894   0.1052   0.5106
  11.250   1.5714   0.02324   0.01567  -0.0866   0.0925   0.5206
  11.500   1.5774   0.02435   0.01678  -0.0839   0.0829   0.5326
  11.750   1.5835   0.02547   0.01796  -0.0815   0.0761   0.5541
  12.250   1.6307   0.02797   0.02107  -0.0845   0.0619   1.0000
  12.500   1.6340   0.02957   0.02267  -0.0823   0.0562   1.0000
  12.750   1.6400   0.03105   0.02420  -0.0805   0.0519   1.0000
  13.000   1.6425   0.03291   0.02609  -0.0787   0.0472   1.0000
  13.250   1.6454   0.03485   0.02806  -0.0772   0.0425   1.0000
  13.500   1.6460   0.03710   0.03035  -0.0757   0.0381   1.0000
  13.750   1.6448   0.03963   0.03291  -0.0745   0.0334   1.0000
  14.000   1.6437   0.04227   0.03561  -0.0735   0.0294   1.0000
  14.250   1.6406   0.04522   0.03861  -0.0726   0.0255   1.0000
  14.500   1.6365   0.04838   0.04182  -0.0719   0.0226   1.0000
  14.750   1.6312   0.05177   0.04528  -0.0714   0.0199   1.0000
  15.000   1.6267   0.05521   0.04879  -0.0711   0.0185   1.0000
  15.250   1.6214   0.05885   0.05252  -0.0710   0.0170   1.0000
  15.500   1.6156   0.06264   0.05640  -0.0711   0.0161   1.0000
  15.750   1.6089   0.06668   0.06053  -0.0714   0.0152   1.0000
  16.000   1.6037   0.07059   0.06454  -0.0717   0.0147   1.0000
  16.250   1.5970   0.07475   0.06881  -0.0722   0.0141   1.0000
  16.500   1.5897   0.07905   0.07320  -0.0728   0.0136   1.0000
  16.750   1.5814   0.08356   0.07782  -0.0736   0.0131   1.0000
  17.000   1.5722   0.08830   0.08266  -0.0745   0.0127   1.0000
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