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ONERA HOR20 AIRFOIL (hor20-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: ONERA HOR20 AIRFOIL (hor20-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.42 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hor20-il-1000000.txt
Download as CSV file: xf-hor20-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: ONERA HOR20 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1522   0.08405   0.08036  -0.0371   1.0000   0.0552
 -17.500  -1.1680   0.07861   0.07487  -0.0399   1.0000   0.0560
 -17.250  -1.1834   0.07325   0.06945  -0.0427   1.0000   0.0569
 -17.000  -1.1982   0.06807   0.06418  -0.0454   1.0000   0.0578
 -16.750  -1.2109   0.06322   0.05925  -0.0479   1.0000   0.0586
 -16.500  -1.2255   0.05833   0.05426  -0.0504   1.0000   0.0593
 -16.250  -1.2526   0.05221   0.04806  -0.0536   1.0000   0.0600
 -16.000  -1.2783   0.04632   0.04208  -0.0567   1.0000   0.0606
 -15.750  -1.3030   0.04054   0.03620  -0.0599   1.0000   0.0612
 -15.500  -1.3224   0.03525   0.03081  -0.0630   1.0000   0.0618
 -15.250  -1.3390   0.02981   0.02525  -0.0671   1.0000   0.0625
 -15.000  -1.3394   0.02466   0.01993  -0.0737   1.0000   0.0635
 -14.750  -1.3226   0.02334   0.01853  -0.0745   1.0000   0.0645
 -14.500  -1.3070   0.02193   0.01708  -0.0750   1.0000   0.0658
 -14.250  -1.2876   0.02093   0.01606  -0.0752   1.0000   0.0672
 -14.000  -1.2658   0.02016   0.01526  -0.0753   1.0000   0.0685
 -13.750  -1.2423   0.01955   0.01461  -0.0753   1.0000   0.0698
 -13.500  -1.2192   0.01888   0.01391  -0.0753   1.0000   0.0711
 -13.250  -1.1959   0.01820   0.01324  -0.0754   1.0000   0.0727
 -13.000  -1.1697   0.01765   0.01268  -0.0757   0.9965   0.0742
 -12.750  -1.1345   0.01718   0.01217  -0.0776   0.9776   0.0759
 -12.500  -1.1031   0.01666   0.01161  -0.0787   0.9601   0.0776
 -12.250  -1.0786   0.01620   0.01111  -0.0784   0.9397   0.0792
 -12.000  -1.0543   0.01583   0.01069  -0.0778   0.9173   0.0808
 -11.750  -1.0293   0.01554   0.01030  -0.0773   0.8950   0.0823
 -11.500  -1.0037   0.01521   0.00987  -0.0770   0.8730   0.0840
 -11.250  -0.9777   0.01483   0.00943  -0.0768   0.8525   0.0859
 -11.000  -0.9507   0.01454   0.00906  -0.0767   0.8337   0.0878
 -10.750  -0.9229   0.01431   0.00874  -0.0766   0.8165   0.0896
 -10.500  -0.8952   0.01398   0.00835  -0.0767   0.8025   0.0918
 -10.250  -0.8674   0.01369   0.00800  -0.0767   0.7890   0.0941
 -10.000  -0.8385   0.01344   0.00771  -0.0769   0.7782   0.0965
  -9.750  -0.8099   0.01321   0.00741  -0.0770   0.7659   0.0987
  -9.500  -0.7812   0.01289   0.00709  -0.0771   0.7558   0.1015
  -9.250  -0.7521   0.01267   0.00682  -0.0773   0.7450   0.1040
  -9.000  -0.7227   0.01248   0.00657  -0.0775   0.7353   0.1064
  -8.750  -0.6935   0.01219   0.00628  -0.0777   0.7255   0.1098
  -8.500  -0.6641   0.01202   0.00605  -0.0778   0.7142   0.1132
  -8.250  -0.6344   0.01179   0.00580  -0.0781   0.7053   0.1165
  -8.000  -0.6048   0.01157   0.00556  -0.0783   0.6952   0.1203
  -7.750  -0.5748   0.01143   0.00537  -0.0785   0.6857   0.1235
  -7.500  -0.5450   0.01119   0.00514  -0.0788   0.6759   0.1278
  -7.250  -0.5151   0.01105   0.00495  -0.0790   0.6646   0.1319
  -7.000  -0.4849   0.01087   0.00476  -0.0792   0.6562   0.1361
  -6.750  -0.4548   0.01071   0.00458  -0.0795   0.6458   0.1410
  -6.500  -0.4245   0.01060   0.00443  -0.0797   0.6361   0.1453
  -6.250  -0.3943   0.01042   0.00425  -0.0800   0.6259   0.1512
  -6.000  -0.3639   0.01035   0.00413  -0.0803   0.6155   0.1558
  -5.750  -0.3335   0.01017   0.00397  -0.0806   0.6067   0.1619
  -5.500  -0.3031   0.01010   0.00385  -0.0808   0.5959   0.1669
  -5.250  -0.2725   0.00998   0.00372  -0.0811   0.5867   0.1722
  -5.000  -0.2420   0.00989   0.00361  -0.0814   0.5767   0.1778
  -4.750  -0.2114   0.00984   0.00351  -0.0817   0.5677   0.1825
  -4.500  -0.1807   0.00972   0.00341  -0.0820   0.5599   0.1888
  -4.250  -0.1501   0.00969   0.00334  -0.0822   0.5511   0.1942
  -4.000  -0.1194   0.00962   0.00326  -0.0825   0.5437   0.2000
  -3.750  -0.0887   0.00955   0.00320  -0.0828   0.5363   0.2061
  -3.500  -0.0580   0.00956   0.00315  -0.0831   0.5284   0.2108
  -3.250  -0.0273   0.00948   0.00309  -0.0834   0.5225   0.2177
  -3.000   0.0036   0.00944   0.00305  -0.0836   0.5167   0.2231
  -2.750   0.0343   0.00947   0.00303  -0.0839   0.5100   0.2269
  -2.500   0.0648   0.00943   0.00298  -0.0842   0.5027   0.2339
  -2.250   0.0958   0.00938   0.00296  -0.0845   0.4983   0.2391
  -2.000   0.1266   0.00939   0.00294  -0.0847   0.4927   0.2430
  -1.750   0.1572   0.00938   0.00290  -0.0850   0.4867   0.2484
  -1.500   0.1878   0.00937   0.00289  -0.0852   0.4806   0.2541
  -1.250   0.2188   0.00933   0.00287  -0.0855   0.4767   0.2591
  -1.000   0.2496   0.00935   0.00286  -0.0858   0.4715   0.2625
  -0.750   0.2802   0.00930   0.00282  -0.0861   0.4660   0.2698
  -0.500   0.3107   0.00932   0.00283  -0.0863   0.4598   0.2756
  -0.250   0.3416   0.00930   0.00282  -0.0866   0.4559   0.2803
   0.000   0.3724   0.00928   0.00280  -0.0869   0.4506   0.2869
   0.250   0.4029   0.00928   0.00281  -0.0871   0.4450   0.2946
   0.500   0.4332   0.00933   0.00284  -0.0873   0.4390   0.3009
   0.750   0.4640   0.00928   0.00285  -0.0876   0.4351   0.3114
   1.000   0.4946   0.00929   0.00287  -0.0879   0.4300   0.3210
   1.250   0.5249   0.00931   0.00291  -0.0881   0.4244   0.3336
   1.500   0.5551   0.00939   0.00297  -0.0883   0.4186   0.3440
   1.750   0.5858   0.00937   0.00301  -0.0885   0.4151   0.3567
   2.000   0.6162   0.00940   0.00306  -0.0888   0.4104   0.3669
   2.250   0.6463   0.00946   0.00313  -0.0889   0.4049   0.3783
   2.500   0.6762   0.00957   0.00321  -0.0891   0.3985   0.3861
   2.750   0.7067   0.00958   0.00327  -0.0893   0.3946   0.3972
   3.000   0.7368   0.00965   0.00334  -0.0895   0.3893   0.4057
   3.250   0.7666   0.00975   0.00343  -0.0896   0.3833   0.4128
   3.500   0.7964   0.00984   0.00353  -0.0897   0.3779   0.4209
   3.750   0.8266   0.00990   0.00361  -0.0899   0.3733   0.4281
   4.000   0.8563   0.01001   0.00370  -0.0900   0.3679   0.4335
   4.250   0.8855   0.01013   0.00381  -0.0901   0.3619   0.4409
   4.500   0.9154   0.01021   0.00392  -0.0902   0.3577   0.4475
   4.750   0.9451   0.01031   0.00402  -0.0903   0.3529   0.4531
   5.000   0.9742   0.01045   0.00413  -0.0904   0.3468   0.4590
   5.250   1.0031   0.01058   0.00427  -0.0904   0.3406   0.4655
   5.500   1.0326   0.01067   0.00438  -0.0905   0.3356   0.4714
   5.750   1.0614   0.01083   0.00452  -0.0905   0.3296   0.4764
   6.000   1.0897   0.01101   0.00468  -0.0904   0.3229   0.4828
   6.250   1.1188   0.01110   0.00481  -0.0905   0.3181   0.4897
   6.500   1.1471   0.01128   0.00497  -0.0904   0.3118   0.4957
   6.750   1.1749   0.01150   0.00515  -0.0902   0.3054   0.5004
   7.000   1.2035   0.01161   0.00530  -0.0902   0.3002   0.5075
   7.250   1.2310   0.01181   0.00549  -0.0901   0.2934   0.5143
   7.500   1.2584   0.01202   0.00569  -0.0899   0.2873   0.5212
   7.750   1.2862   0.01218   0.00587  -0.0897   0.2821   0.5294
   8.000   1.3130   0.01240   0.00609  -0.0895   0.2763   0.5385
   8.250   1.3396   0.01263   0.00632  -0.0892   0.2709   0.5460
   8.500   1.3667   0.01279   0.00653  -0.0890   0.2661   0.5584
   8.750   1.3925   0.01304   0.00680  -0.0886   0.2604   0.5742
   9.000   1.4181   0.01327   0.00708  -0.0882   0.2550   0.5990
   9.250   1.4444   0.01336   0.00734  -0.0879   0.2507   0.6553
   9.500   1.4637   0.01302   0.00765  -0.0861   0.2460   1.0000
   9.750   1.4872   0.01342   0.00800  -0.0854   0.2402   1.0000
  10.000   1.5129   0.01365   0.00824  -0.0850   0.2366   1.0000
  10.250   1.5368   0.01397   0.00854  -0.0843   0.2316   1.0000
  10.500   1.5582   0.01441   0.00894  -0.0833   0.2257   1.0000
  10.750   1.5817   0.01470   0.00924  -0.0825   0.2217   1.0000
  11.000   1.6033   0.01507   0.00960  -0.0815   0.2170   1.0000
  11.250   1.6217   0.01556   0.01006  -0.0801   0.2118   1.0000
  11.500   1.6408   0.01595   0.01046  -0.0787   0.2075   1.0000
  11.750   1.6560   0.01644   0.01094  -0.0767   0.2025   1.0000
  12.000   1.6684   0.01713   0.01161  -0.0745   0.1973   1.0000
  12.250   1.6849   0.01769   0.01218  -0.0730   0.1934   1.0000
  12.500   1.6995   0.01838   0.01288  -0.0714   0.1887   1.0000
  12.750   1.7107   0.01934   0.01382  -0.0696   0.1836   1.0000
  13.000   1.7258   0.02011   0.01462  -0.0683   0.1798   1.0000
  13.250   1.7383   0.02110   0.01561  -0.0670   0.1754   1.0000
  13.500   1.7472   0.02242   0.01692  -0.0655   0.1706   1.0000
  13.750   1.7607   0.02346   0.01800  -0.0645   0.1674   1.0000
  14.000   1.7716   0.02475   0.01931  -0.0634   0.1636   1.0000
  14.250   1.7788   0.02639   0.02096  -0.0623   0.1598   1.0000
  14.500   1.7878   0.02795   0.02255  -0.0614   0.1566   1.0000
  14.750   1.7965   0.02955   0.02418  -0.0606   0.1532   1.0000
  15.000   1.8007   0.03159   0.02625  -0.0597   0.1495   1.0000
  15.250   1.8033   0.03383   0.02850  -0.0589   0.1460   1.0000
  15.500   1.8102   0.03567   0.03040  -0.0582   0.1431   1.0000
  15.750   1.8123   0.03800   0.03276  -0.0575   0.1398   1.0000
  16.000   1.8095   0.04085   0.03564  -0.0568   0.1366   1.0000
  16.250   1.8100   0.04342   0.03827  -0.0563   0.1341   1.0000
  16.500   1.8103   0.04606   0.04096  -0.0558   0.1314   1.0000
  16.750   1.8073   0.04910   0.04404  -0.0554   0.1287   1.0000
  17.000   1.8002   0.05265   0.04763  -0.0551   0.1259   1.0000
  17.250   1.7982   0.05572   0.05077  -0.0549   0.1238   1.0000
  17.500   1.7955   0.05892   0.05402  -0.0549   0.1215   1.0000
  17.750   1.7897   0.06249   0.05764  -0.0548   0.1190   1.0000
  18.000   1.7797   0.06657   0.06177  -0.0550   0.1165   1.0000
  18.250   1.7737   0.07026   0.06552  -0.0551   0.1145   1.0000
  18.500   1.7710   0.07355   0.06887  -0.0553   0.1122   1.0000
  18.750   1.7623   0.07762   0.07299  -0.0556   0.1098   1.0000
  19.000   1.7494   0.08223   0.07766  -0.0561   0.1074   1.0000
  19.250   1.7448   0.08583   0.08131  -0.0565   0.1053   1.0000
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