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GIII BL0 AIRFOIL (giiia-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GIII BL0 AIRFOIL (giiia-il)
Reynolds number: 500,000
Max Cl/Cd: 62.81 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-giiia-il-500000-n5.txt
Download as CSV file: xf-giiia-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.9553   0.08258   0.08004  -0.0110   1.0000   0.0054
 -14.250  -1.0032   0.06456   0.06174  -0.0243   1.0000   0.0053
 -14.000  -1.0295   0.05596   0.05291  -0.0300   1.0000   0.0053
 -13.750  -1.0492   0.04994   0.04667  -0.0328   1.0000   0.0053
 -13.500  -1.0645   0.04535   0.04186  -0.0337   1.0000   0.0053
 -13.250  -1.0757   0.04174   0.03803  -0.0332   1.0000   0.0053
 -13.000  -1.0837   0.03878   0.03485  -0.0319   1.0000   0.0054
 -12.750  -1.0879   0.03633   0.03219  -0.0300   1.0000   0.0054
 -12.500  -1.0889   0.03426   0.02992  -0.0278   1.0000   0.0055
 -12.250  -1.0935   0.03197   0.02743  -0.0248   1.0000   0.0056
 -12.000  -1.0920   0.03023   0.02552  -0.0220   1.0000   0.0057
 -11.750  -1.0858   0.02887   0.02402  -0.0194   1.0000   0.0059
 -11.500  -1.0760   0.02774   0.02277  -0.0172   1.0000   0.0061
 -11.250  -1.0627   0.02673   0.02165  -0.0155   1.0000   0.0063
 -11.000  -1.0477   0.02582   0.02062  -0.0140   1.0000   0.0065
 -10.750  -1.0317   0.02493   0.01963  -0.0125   1.0000   0.0068
 -10.500  -1.0152   0.02405   0.01860  -0.0110   1.0000   0.0071
 -10.250  -0.9985   0.02311   0.01753  -0.0095   1.0000   0.0075
 -10.000  -0.9814   0.02221   0.01649  -0.0080   1.0000   0.0078
  -9.750  -0.9637   0.02137   0.01551  -0.0065   1.0000   0.0080
  -9.500  -0.9480   0.02033   0.01435  -0.0047   1.0000   0.0084
  -9.250  -0.9315   0.01946   0.01340  -0.0029   1.0000   0.0088
  -9.000  -0.9135   0.01885   0.01274  -0.0014   1.0000   0.0092
  -8.750  -0.8957   0.01829   0.01212   0.0003   1.0000   0.0097
  -8.500  -0.8786   0.01775   0.01151   0.0022   1.0000   0.0102
  -8.250  -0.8621   0.01723   0.01090   0.0042   1.0000   0.0108
  -8.000  -0.8459   0.01679   0.01038   0.0063   1.0000   0.0114
  -7.750  -0.8196   0.01612   0.00964   0.0062   0.9977   0.0122
  -7.500  -0.7903   0.01550   0.00899   0.0054   0.9950   0.0134
  -7.250  -0.7609   0.01502   0.00847   0.0048   0.9920   0.0144
  -7.000  -0.7313   0.01453   0.00793   0.0041   0.9889   0.0155
  -6.750  -0.6992   0.01410   0.00742   0.0029   0.9861   0.0165
  -6.500  -0.6683   0.01349   0.00678   0.0019   0.9807   0.0186
  -6.250  -0.6344   0.01304   0.00632   0.0004   0.9746   0.0207
  -6.000  -0.6042   0.01266   0.00588  -0.0003   0.9659   0.0226
  -5.750  -0.5746   0.01227   0.00545  -0.0008   0.9591   0.0252
  -5.500  -0.5470   0.01188   0.00506  -0.0009   0.9519   0.0290
  -5.250  -0.5191   0.01159   0.00472  -0.0010   0.9459   0.0321
  -5.000  -0.4930   0.01127   0.00440  -0.0007   0.9388   0.0375
  -4.750  -0.4661   0.01099   0.00411  -0.0006   0.9329   0.0443
  -4.500  -0.4410   0.01069   0.00385  -0.0001   0.9258   0.0552
  -4.000  -0.3909   0.01009   0.00336   0.0009   0.9119   0.0916
  -3.500  -0.3414   0.00950   0.00297   0.0020   0.8979   0.1488
  -3.250  -0.3163   0.00926   0.00278   0.0025   0.8900   0.1757
  -3.000  -0.2915   0.00904   0.00261   0.0032   0.8789   0.2004
  -2.750  -0.2674   0.00877   0.00243   0.0039   0.8664   0.2363
  -2.500  -0.2449   0.00835   0.00223   0.0049   0.8531   0.3009
  -2.250  -0.2312   0.00729   0.00191   0.0074   0.8393   0.4976
  -2.000  -0.2114   0.00688   0.00179   0.0091   0.8241   0.5916
  -1.750  -0.1888   0.00667   0.00170   0.0103   0.8078   0.6419
  -1.500  -0.1651   0.00653   0.00161   0.0114   0.7877   0.6767
  -1.250  -0.1413   0.00643   0.00152   0.0124   0.7566   0.7063
  -1.000  -0.1187   0.00643   0.00142   0.0138   0.7096   0.7336
  -0.750  -0.0960   0.00649   0.00138   0.0150   0.6660   0.7601
  -0.250  -0.0475   0.00663   0.00141   0.0168   0.5991   0.8131
   0.000  -0.0217   0.00672   0.00146   0.0173   0.5725   0.8367
   0.250   0.0050   0.00682   0.00152   0.0177   0.5502   0.8573
   0.500   0.0317   0.00694   0.00158   0.0180   0.5278   0.8742
   0.750   0.0588   0.00708   0.00165   0.0183   0.5047   0.8889
   1.000   0.0867   0.00724   0.00174   0.0183   0.4813   0.9004
   1.250   0.1142   0.00739   0.00180   0.0184   0.4579   0.9089
   1.500   0.1421   0.00756   0.00187   0.0184   0.4290   0.9153
   1.750   0.1679   0.00779   0.00194   0.0187   0.3854   0.9219
   2.000   0.1960   0.00811   0.00206   0.0185   0.3395   0.9265
   2.250   0.2205   0.00846   0.00218   0.0190   0.2815   0.9329
   2.500   0.2484   0.00879   0.00234   0.0188   0.2437   0.9372
   2.750   0.2776   0.00904   0.00249   0.0184   0.2229   0.9410
   3.250   0.3322   0.00941   0.00276   0.0184   0.2003   0.9502
   3.500   0.3635   0.00961   0.00293   0.0175   0.1927   0.9527
   3.750   0.3938   0.00977   0.00309   0.0169   0.1871   0.9556
   4.000   0.4217   0.00996   0.00325   0.0168   0.1823   0.9595
   4.250   0.4491   0.01013   0.00343   0.0168   0.1787   0.9632
   4.500   0.4814   0.01030   0.00362   0.0156   0.1756   0.9649
   4.750   0.5133   0.01048   0.00382   0.0146   0.1723   0.9667
   5.000   0.5444   0.01068   0.00404   0.0137   0.1689   0.9688
   5.250   0.5732   0.01091   0.00427   0.0133   0.1662   0.9718
   5.500   0.6009   0.01108   0.00449   0.0132   0.1636   0.9749
   5.750   0.6337   0.01124   0.00465   0.0118   0.1562   0.9761
   6.000   0.6656   0.01147   0.00489   0.0107   0.1496   0.9776
   6.250   0.6974   0.01161   0.00507   0.0096   0.1422   0.9795
   6.500   0.7281   0.01182   0.00527   0.0087   0.1324   0.9820
   6.750   0.7575   0.01206   0.00548   0.0081   0.1155   0.9853
   7.000   0.7865   0.01316   0.00614   0.0068   0.0434   0.9874
   7.250   0.8171   0.01384   0.00675   0.0056   0.0256   0.9897
   7.500   0.8464   0.01435   0.00727   0.0049   0.0191   0.9920
   7.750   0.8736   0.01487   0.00781   0.0045   0.0156   0.9941
   8.000   0.9024   0.01537   0.00838   0.0038   0.0136   0.9954
   8.250   0.9308   0.01586   0.00894   0.0032   0.0122   0.9967
   8.500   0.9584   0.01645   0.00959   0.0027   0.0109   0.9982
   8.750   0.9849   0.01720   0.01042   0.0023   0.0096   0.9997
   9.000   1.0039   0.01768   0.01097   0.0036   0.0090   1.0000
   9.250   1.0192   0.01820   0.01156   0.0056   0.0084   1.0000
   9.500   1.0335   0.01877   0.01219   0.0078   0.0080   1.0000
   9.750   1.0470   0.01937   0.01286   0.0101   0.0076   1.0000
  10.000   1.0588   0.02004   0.01360   0.0127   0.0072   1.0000
  10.250   1.0675   0.02091   0.01456   0.0156   0.0068   1.0000
  10.500   1.0748   0.02181   0.01555   0.0188   0.0066   1.0000
  10.750   1.0841   0.02255   0.01640   0.0216   0.0064   1.0000
  11.000   1.0919   0.02337   0.01732   0.0246   0.0063   1.0000
  11.250   1.0976   0.02426   0.01830   0.0278   0.0061   1.0000
  11.500   1.1001   0.02515   0.01929   0.0314   0.0059   1.0000
  11.750   1.1038   0.02616   0.02040   0.0345   0.0057   1.0000
  12.000   1.1087   0.02729   0.02163   0.0369   0.0055   1.0000
  12.250   1.1138   0.02855   0.02299   0.0389   0.0053   1.0000
  12.500   1.1190   0.02993   0.02446   0.0406   0.0052   1.0000
  12.750   1.1234   0.03148   0.02612   0.0419   0.0050   1.0000
  13.000   1.1268   0.03326   0.02800   0.0428   0.0049   1.0000
  13.250   1.1286   0.03535   0.03022   0.0434   0.0047   1.0000
  13.500   1.1274   0.03794   0.03292   0.0435   0.0046   1.0000
  13.750   1.1233   0.04117   0.03628   0.0430   0.0045   1.0000
  14.000   1.1163   0.04509   0.04035   0.0417   0.0045   1.0000
  14.250   1.1071   0.04967   0.04508   0.0397   0.0044   1.0000
  14.500   1.0958   0.05480   0.05036   0.0372   0.0044   1.0000
  14.750   1.0823   0.06045   0.05616   0.0344   0.0043   1.0000
  15.000   1.0705   0.06602   0.06186   0.0316   0.0043   1.0000
  15.250   1.0578   0.07191   0.06788   0.0286   0.0043   1.0000
  15.500   1.0439   0.07808   0.07419   0.0255   0.0043   1.0000
  15.750   1.0297   0.08449   0.08072   0.0222   0.0043   1.0000
  16.000   1.0151   0.09103   0.08738   0.0190   0.0043   1.0000
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