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GIII BL0 AIRFOIL (giiia-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GIII BL0 AIRFOIL (giiia-il)
Reynolds number: 1,000,000
Max Cl/Cd: 72.01 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-giiia-il-1000000-n5.txt
Download as CSV file: xf-giiia-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GIII BL0 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -1.0345   0.09815   0.09607  -0.0027   1.0000   0.0034
 -16.000  -1.1787   0.06128   0.05870  -0.0260   1.0000   0.0033
 -15.750  -1.2066   0.05312   0.05033  -0.0309   1.0000   0.0032
 -15.500  -1.2240   0.04762   0.04465  -0.0331   1.0000   0.0033
 -15.250  -1.2355   0.04349   0.04036  -0.0339   1.0000   0.0033
 -15.000  -1.2442   0.04010   0.03681  -0.0337   1.0000   0.0033
 -14.750  -1.2487   0.03742   0.03397  -0.0328   1.0000   0.0033
 -14.500  -1.2512   0.03512   0.03153  -0.0314   1.0000   0.0033
 -14.250  -1.2512   0.03316   0.02943  -0.0297   1.0000   0.0034
 -14.000  -1.2489   0.03147   0.02761  -0.0278   1.0000   0.0034
 -13.750  -1.2449   0.02997   0.02598  -0.0257   1.0000   0.0034
 -13.500  -1.2411   0.02848   0.02436  -0.0233   1.0000   0.0034
 -13.250  -1.2393   0.02685   0.02255  -0.0204   1.0000   0.0036
 -13.000  -1.2334   0.02551   0.02107  -0.0177   1.0000   0.0037
 -12.750  -1.2240   0.02439   0.01984  -0.0154   1.0000   0.0038
 -12.500  -1.2116   0.02343   0.01878  -0.0134   1.0000   0.0039
 -12.250  -1.1963   0.02255   0.01780  -0.0118   1.0000   0.0040
 -12.000  -1.1797   0.02175   0.01691  -0.0104   1.0000   0.0042
 -11.750  -1.1622   0.02099   0.01607  -0.0091   1.0000   0.0043
 -11.500  -1.1440   0.02029   0.01529  -0.0078   1.0000   0.0045
 -11.250  -1.1252   0.01961   0.01454  -0.0066   1.0000   0.0046
 -11.000  -1.1061   0.01896   0.01381  -0.0054   1.0000   0.0048
 -10.750  -1.0867   0.01834   0.01311  -0.0042   1.0000   0.0050
 -10.500  -1.0670   0.01775   0.01245  -0.0029   1.0000   0.0051
 -10.250  -1.0472   0.01720   0.01182  -0.0017   1.0000   0.0053
 -10.000  -1.0273   0.01670   0.01125  -0.0004   1.0000   0.0054
  -9.750  -1.0091   0.01610   0.01058   0.0012   1.0000   0.0057
  -9.500  -0.9910   0.01558   0.01002   0.0029   1.0000   0.0061
  -9.250  -0.9726   0.01517   0.00959   0.0045   1.0000   0.0065
  -9.000  -0.9456   0.01473   0.00912   0.0043   0.9981   0.0070
  -8.750  -0.9161   0.01429   0.00864   0.0036   0.9956   0.0075
  -8.500  -0.8865   0.01386   0.00816   0.0029   0.9931   0.0079
  -8.250  -0.8576   0.01344   0.00768   0.0024   0.9896   0.0082
  -8.000  -0.8287   0.01292   0.00713   0.0018   0.9864   0.0091
  -7.750  -0.7994   0.01253   0.00673   0.0012   0.9821   0.0099
  -7.500  -0.7690   0.01217   0.00635   0.0004   0.9762   0.0106
  -7.250  -0.7392   0.01185   0.00599  -0.0002   0.9675   0.0113
  -7.000  -0.7110   0.01153   0.00562  -0.0004   0.9572   0.0121
  -6.750  -0.6851   0.01118   0.00523  -0.0001   0.9458   0.0135
  -6.500  -0.6601   0.01091   0.00493   0.0004   0.9344   0.0147
  -6.250  -0.6351   0.01066   0.00465   0.0010   0.9242   0.0158
  -6.000  -0.6096   0.01045   0.00439   0.0014   0.9163   0.0166
  -5.750  -0.5846   0.01017   0.00409   0.0019   0.9085   0.0193
  -5.500  -0.5591   0.00994   0.00384   0.0024   0.9020   0.0216
  -5.250  -0.5331   0.00975   0.00362   0.0027   0.8953   0.0234
  -5.000  -0.5075   0.00953   0.00338   0.0031   0.8890   0.0276
  -4.750  -0.4816   0.00932   0.00317   0.0035   0.8822   0.0313
  -4.250  -0.4295   0.00894   0.00278   0.0042   0.8688   0.0426
  -4.000  -0.4040   0.00874   0.00259   0.0046   0.8600   0.0539
  -3.750  -0.3786   0.00854   0.00241   0.0051   0.8484   0.0677
  -3.500  -0.3532   0.00833   0.00224   0.0055   0.8363   0.0853
  -3.250  -0.3278   0.00812   0.00208   0.0060   0.8245   0.1092
  -3.000  -0.3026   0.00791   0.00194   0.0065   0.8108   0.1369
  -2.750  -0.2771   0.00774   0.00181   0.0069   0.7940   0.1612
  -2.500  -0.2515   0.00763   0.00169   0.0074   0.7694   0.1799
  -2.250  -0.2276   0.00759   0.00155   0.0082   0.7197   0.2033
  -2.000  -0.2046   0.00750   0.00144   0.0091   0.6752   0.2439
  -1.750  -0.1829   0.00728   0.00132   0.0102   0.6320   0.3157
  -1.500  -0.1649   0.00670   0.00113   0.0119   0.5971   0.4584
  -1.250  -0.1455   0.00630   0.00105   0.0134   0.5698   0.5774
  -1.000  -0.1212   0.00622   0.00101   0.0141   0.5469   0.6171
  -0.750  -0.0963   0.00618   0.00099   0.0147   0.5256   0.6459
  -0.500  -0.0712   0.00615   0.00096   0.0153   0.5064   0.6712
  -0.250  -0.0459   0.00611   0.00095   0.0158   0.4895   0.6956
   0.000  -0.0207   0.00610   0.00094   0.0164   0.4702   0.7200
   0.250   0.0042   0.00608   0.00094   0.0170   0.4486   0.7461
   0.500   0.0284   0.00609   0.00095   0.0178   0.4192   0.7747
   0.750   0.0521   0.00617   0.00099   0.0186   0.3793   0.8049
   1.000   0.0765   0.00628   0.00106   0.0193   0.3445   0.8320
   1.250   0.1011   0.00647   0.00115   0.0200   0.2984   0.8542
   1.500   0.1258   0.00672   0.00126   0.0205   0.2501   0.8730
   1.750   0.1519   0.00689   0.00137   0.0209   0.2255   0.8880
   2.250   0.2058   0.00715   0.00153   0.0212   0.1967   0.9048
   2.500   0.2337   0.00726   0.00162   0.0211   0.1884   0.9108
   2.750   0.2609   0.00738   0.00172   0.0212   0.1811   0.9173
   3.000   0.2887   0.00748   0.00181   0.0212   0.1765   0.9226
   3.250   0.3168   0.00759   0.00191   0.0211   0.1723   0.9276
   3.500   0.3439   0.00771   0.00202   0.0212   0.1683   0.9331
   3.750   0.3720   0.00783   0.00214   0.0210   0.1648   0.9373
   4.000   0.4007   0.00793   0.00226   0.0208   0.1630   0.9413
   4.250   0.4281   0.00804   0.00239   0.0208   0.1609   0.9459
   4.500   0.4553   0.00817   0.00251   0.0209   0.1583   0.9500
   4.750   0.4847   0.00831   0.00266   0.0205   0.1557   0.9528
   5.000   0.5132   0.00846   0.00282   0.0202   0.1534   0.9561
   5.250   0.5400   0.00860   0.00298   0.0203   0.1499   0.9600
   5.500   0.5675   0.00871   0.00310   0.0203   0.1457   0.9632
   5.750   0.5974   0.00889   0.00326   0.0197   0.1399   0.9651
   6.000   0.6267   0.00904   0.00342   0.0192   0.1345   0.9674
   6.250   0.6549   0.00924   0.00358   0.0189   0.1242   0.9701
   6.500   0.6805   0.00945   0.00375   0.0192   0.1116   0.9737
   6.750   0.7041   0.01037   0.00431   0.0193   0.0482   0.9759
   7.000   0.7323   0.01097   0.00480   0.0188   0.0257   0.9778
   7.250   0.7630   0.01138   0.00520   0.0178   0.0185   0.9803
   7.500   0.7923   0.01178   0.00559   0.0171   0.0143   0.9838
   7.750   0.8235   0.01212   0.00595   0.0161   0.0126   0.9858
   8.000   0.8543   0.01253   0.00636   0.0150   0.0105   0.9868
   8.250   0.8837   0.01289   0.00675   0.0143   0.0093   0.9878
   8.500   0.9125   0.01326   0.00715   0.0136   0.0083   0.9889
   8.750   0.9403   0.01368   0.00759   0.0132   0.0074   0.9903
   9.000   0.9671   0.01418   0.00813   0.0129   0.0066   0.9919
   9.250   0.9937   0.01459   0.00859   0.0127   0.0063   0.9935
   9.500   1.0203   0.01504   0.00908   0.0124   0.0059   0.9947
   9.750   1.0480   0.01552   0.00961   0.0119   0.0055   0.9956
  10.000   1.0753   0.01603   0.01017   0.0113   0.0052   0.9966
  10.250   1.1019   0.01661   0.01080   0.0109   0.0048   0.9978
  10.500   1.1264   0.01743   0.01170   0.0107   0.0043   0.9991
  10.750   1.1518   0.01797   0.01229   0.0105   0.0042   1.0000
  11.000   1.1649   0.01846   0.01284   0.0129   0.0041   1.0000
  11.250   1.1771   0.01899   0.01344   0.0154   0.0040   1.0000
  11.500   1.1885   0.01956   0.01407   0.0180   0.0038   1.0000
  11.750   1.1994   0.02016   0.01475   0.0207   0.0037   1.0000
  12.000   1.2096   0.02080   0.01545   0.0233   0.0036   1.0000
  12.250   1.2192   0.02149   0.01622   0.0260   0.0035   1.0000
  12.500   1.2257   0.02217   0.01697   0.0292   0.0034   1.0000
  12.750   1.2323   0.02293   0.01781   0.0321   0.0033   1.0000
  13.000   1.2398   0.02382   0.01877   0.0344   0.0032   1.0000
  13.250   1.2474   0.02482   0.01985   0.0365   0.0031   1.0000
  13.500   1.2542   0.02597   0.02108   0.0383   0.0031   1.0000
  13.750   1.2598   0.02730   0.02251   0.0399   0.0030   1.0000
  14.000   1.2637   0.02887   0.02417   0.0413   0.0029   1.0000
  14.250   1.2656   0.03073   0.02613   0.0424   0.0028   1.0000
  14.500   1.2651   0.03299   0.02851   0.0432   0.0028   1.0000
  14.750   1.2614   0.03580   0.03145   0.0433   0.0027   1.0000
  15.000   1.2553   0.03926   0.03505   0.0427   0.0027   1.0000
  15.250   1.2460   0.04355   0.03948   0.0411   0.0026   1.0000
  15.500   1.2342   0.04862   0.04470   0.0386   0.0026   1.0000
  15.750   1.2190   0.05450   0.05074   0.0356   0.0026   1.0000
  16.000   1.2009   0.06107   0.05747   0.0321   0.0026   1.0000
  16.250   1.1811   0.06810   0.06464   0.0284   0.0026   1.0000
  16.500   1.1600   0.07554   0.07221   0.0247   0.0026   1.0000
  16.750   1.1366   0.08346   0.08027   0.0208   0.0026   1.0000
  17.000   1.1141   0.09132   0.08824   0.0171   0.0026   1.0000
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