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HSNLF(1)-0213 AIRFOIL (hsnlf213-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HSNLF(1)-0213 AIRFOIL (hsnlf213-il)
Reynolds number: 500,000
Max Cl/Cd: 59.78 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hsnlf213-il-500000-n5.txt
Download as CSV file: xf-hsnlf213-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HSNLF(1)-0213 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.9660   0.05596   0.05256  -0.0280   0.7843   0.0071
 -13.000  -1.0011   0.04902   0.04527  -0.0286   0.7823   0.0071
 -12.750  -1.0235   0.04401   0.03993  -0.0277   0.7802   0.0072
 -12.500  -1.0365   0.04017   0.03577  -0.0263   0.7782   0.0073
 -12.250  -1.0432   0.03702   0.03230  -0.0246   0.7762   0.0075
 -12.000  -1.0440   0.03443   0.02940  -0.0228   0.7744   0.0076
 -11.750  -1.0395   0.03231   0.02700  -0.0211   0.7726   0.0078
 -11.500  -1.0319   0.03066   0.02511  -0.0193   0.7709   0.0079
 -11.250  -1.0209   0.02912   0.02342  -0.0179   0.7690   0.0081
 -11.000  -1.0050   0.02803   0.02220  -0.0169   0.7670   0.0083
 -10.750  -0.9869   0.02715   0.02123  -0.0162   0.7652   0.0084
 -10.500  -0.9672   0.02641   0.02039  -0.0156   0.7634   0.0087
 -10.250  -0.9469   0.02567   0.01955  -0.0150   0.7619   0.0090
 -10.000  -0.9262   0.02486   0.01861  -0.0145   0.7605   0.0093
  -9.750  -0.9049   0.02402   0.01760  -0.0139   0.7592   0.0098
  -9.500  -0.8829   0.02320   0.01659  -0.0134   0.7579   0.0102
  -9.250  -0.8610   0.02226   0.01552  -0.0130   0.7566   0.0106
  -9.000  -0.8386   0.02147   0.01467  -0.0126   0.7553   0.0110
  -8.750  -0.8152   0.02084   0.01398  -0.0123   0.7539   0.0113
  -8.500  -0.7916   0.02016   0.01322  -0.0120   0.7525   0.0116
  -8.250  -0.7678   0.01947   0.01245  -0.0116   0.7510   0.0120
  -8.000  -0.7438   0.01879   0.01168  -0.0113   0.7495   0.0124
  -7.750  -0.7197   0.01813   0.01092  -0.0110   0.7480   0.0128
  -7.500  -0.6953   0.01751   0.01021  -0.0106   0.7468   0.0132
  -7.250  -0.6707   0.01694   0.00955  -0.0103   0.7457   0.0135
  -7.000  -0.6466   0.01633   0.00892  -0.0100   0.7445   0.0142
  -6.750  -0.6211   0.01594   0.00849  -0.0099   0.7435   0.0148
  -6.500  -0.5955   0.01554   0.00805  -0.0098   0.7424   0.0156
  -6.250  -0.5698   0.01510   0.00757  -0.0097   0.7413   0.0164
  -6.000  -0.5438   0.01470   0.00712  -0.0095   0.7401   0.0171
  -5.750  -0.5186   0.01419   0.00661  -0.0094   0.7387   0.0180
  -5.500  -0.4923   0.01383   0.00623  -0.0093   0.7373   0.0191
  -5.250  -0.4658   0.01350   0.00588  -0.0093   0.7359   0.0204
  -5.000  -0.4390   0.01321   0.00555  -0.0093   0.7347   0.0216
  -4.750  -0.4126   0.01286   0.00521  -0.0093   0.7336   0.0237
  -4.500  -0.3855   0.01260   0.00492  -0.0094   0.7325   0.0259
  -4.250  -0.3586   0.01231   0.00463  -0.0094   0.7314   0.0284
  -4.000  -0.3314   0.01207   0.00439  -0.0095   0.7303   0.0320
  -3.750  -0.3042   0.01182   0.00414  -0.0095   0.7292   0.0372
  -3.500  -0.2769   0.01158   0.00393  -0.0096   0.7281   0.0456
  -3.250  -0.2496   0.01134   0.00374  -0.0097   0.7270   0.0609
  -3.000  -0.2223   0.01104   0.00356  -0.0099   0.7259   0.0856
  -2.750  -0.1959   0.01062   0.00337  -0.0100   0.7247   0.1374
  -2.500  -0.1706   0.01001   0.00315  -0.0101   0.7234   0.2362
  -2.250  -0.1467   0.00918   0.00287  -0.0101   0.7219   0.3788
  -2.000  -0.1276   0.00778   0.00257  -0.0093   0.7204   0.6416
  -1.750  -0.0993   0.00825   0.00318  -0.0090   0.7191   0.7298
  -1.500  -0.0707   0.00862   0.00354  -0.0089   0.7178   0.7498
  -1.250  -0.0428   0.00889   0.00384  -0.0085   0.7165   0.7644
  -1.000  -0.0152   0.00909   0.00405  -0.0082   0.7152   0.7760
  -0.750   0.0136   0.00915   0.00409  -0.0083   0.7141   0.7800
  -0.500   0.0430   0.00915   0.00405  -0.0087   0.7130   0.7819
  -0.250   0.0725   0.00916   0.00401  -0.0091   0.7116   0.7831
   0.000   0.1022   0.00914   0.00398  -0.0097   0.7099   0.7839
   0.250   0.1319   0.00911   0.00394  -0.0102   0.7077   0.7844
   0.500   0.1615   0.00907   0.00389  -0.0107   0.7051   0.7847
   0.750   0.1911   0.00902   0.00382  -0.0112   0.7020   0.7852
   1.000   0.2205   0.00897   0.00373  -0.0116   0.6988   0.7857
   1.250   0.2499   0.00894   0.00367  -0.0120   0.6959   0.7860
   1.500   0.2796   0.00890   0.00366  -0.0125   0.6918   0.7862
   2.000   0.3383   0.00874   0.00347  -0.0133   0.6819   0.7866
   2.250   0.3677   0.00867   0.00345  -0.0137   0.6745   0.7869
   2.500   0.3968   0.00857   0.00333  -0.0140   0.6658   0.7873
   2.750   0.4261   0.00849   0.00328  -0.0144   0.6537   0.7876
   3.000   0.4553   0.00845   0.00325  -0.0148   0.6409   0.7878
   3.250   0.4841   0.00841   0.00317  -0.0150   0.6195   0.7879
   3.500   0.5111   0.00855   0.00307  -0.0150   0.5599   0.7881
   3.750   0.5356   0.00913   0.00328  -0.0149   0.4773   0.7883
   4.000   0.5598   0.00980   0.00362  -0.0149   0.4032   0.7885
   4.250   0.5829   0.01058   0.00402  -0.0148   0.3198   0.7888
   4.500   0.6061   0.01131   0.00441  -0.0147   0.2462   0.7892
   4.750   0.6300   0.01191   0.00476  -0.0147   0.1935   0.7895
   5.000   0.6546   0.01241   0.00508  -0.0147   0.1541   0.7896
   5.250   0.6796   0.01285   0.00538  -0.0147   0.1266   0.7898
   5.500   0.7045   0.01326   0.00570  -0.0147   0.1051   0.7899
   5.750   0.7295   0.01365   0.00601  -0.0147   0.0875   0.7900
   6.000   0.7543   0.01404   0.00634  -0.0147   0.0733   0.7902
   6.250   0.7791   0.01442   0.00668  -0.0146   0.0626   0.7904
   6.500   0.8036   0.01481   0.00703  -0.0145   0.0549   0.7907
   6.750   0.8281   0.01518   0.00739  -0.0144   0.0494   0.7910
   7.000   0.8522   0.01557   0.00778  -0.0143   0.0451   0.7912
   7.250   0.8763   0.01595   0.00818  -0.0142   0.0419   0.7914
   7.500   0.8994   0.01640   0.00862  -0.0139   0.0387   0.7915
   7.750   0.9224   0.01683   0.00908  -0.0136   0.0364   0.7916
   8.000   0.9453   0.01725   0.00954  -0.0133   0.0346   0.7918
   8.250   0.9674   0.01771   0.01003  -0.0130   0.0330   0.7919
   8.500   0.9885   0.01824   0.01057  -0.0125   0.0316   0.7921
   8.750   1.0076   0.01888   0.01124  -0.0118   0.0302   0.7922
   9.000   1.0255   0.01943   0.01185  -0.0109   0.0295   0.7924
   9.250   1.0438   0.02002   0.01250  -0.0101   0.0288   0.7926
   9.500   1.0628   0.02067   0.01321  -0.0096   0.0280   0.7928
   9.750   1.0816   0.02135   0.01394  -0.0091   0.0271   0.7930
  10.000   1.0998   0.02207   0.01471  -0.0086   0.0263   0.7932
  10.250   1.1169   0.02287   0.01555  -0.0080   0.0257   0.7933
  10.500   1.1328   0.02376   0.01648  -0.0073   0.0250   0.7935
  10.750   1.1467   0.02481   0.01758  -0.0065   0.0244   0.7937
  11.000   1.1598   0.02592   0.01876  -0.0055   0.0239   0.7939
  11.250   1.1753   0.02683   0.01975  -0.0048   0.0236   0.7941
  11.500   1.1900   0.02780   0.02081  -0.0041   0.0232   0.7943
  11.750   1.2044   0.02879   0.02189  -0.0034   0.0228   0.7946
  12.000   1.2183   0.02983   0.02301  -0.0026   0.0223   0.7949
  12.250   1.2316   0.03091   0.02416  -0.0019   0.0218   0.7953
  12.500   1.2442   0.03206   0.02539  -0.0012   0.0213   0.7956
  12.750   1.2559   0.03328   0.02669  -0.0004   0.0210   0.7958
  13.000   1.2669   0.03456   0.02806   0.0003   0.0206   0.7960
  13.250   1.2772   0.03592   0.02950   0.0011   0.0203   0.7962
  13.500   1.2861   0.03740   0.03106   0.0019   0.0200   0.7964
  13.750   1.2934   0.03904   0.03277   0.0027   0.0197   0.7966
  14.000   1.2987   0.04090   0.03471   0.0035   0.0193   0.7968
  14.250   1.3007   0.04309   0.03699   0.0045   0.0190   0.7970
  14.500   1.3072   0.04488   0.03890   0.0051   0.0188   0.7972
  14.750   1.3133   0.04674   0.04090   0.0056   0.0186   0.7974
  15.000   1.3185   0.04872   0.04301   0.0060   0.0183   0.7976
  15.250   1.3230   0.05083   0.04525   0.0063   0.0180   0.7978
  15.500   1.3267   0.05311   0.04766   0.0064   0.0177   0.7980
  15.750   1.3296   0.05557   0.05024   0.0064   0.0174   0.7982
  16.000   1.3308   0.05830   0.05309   0.0062   0.0171   0.7985
  16.250   1.3323   0.06110   0.05600   0.0059   0.0168   0.7987
  16.500   1.3334   0.06406   0.05907   0.0053   0.0165   0.7989
  16.750   1.3332   0.06730   0.06242   0.0045   0.0162   0.7992
  17.000   1.3315   0.07085   0.06608   0.0034   0.0160   0.7994
  17.250   1.3291   0.07462   0.06996   0.0021   0.0158   0.7996
  17.500   1.3242   0.07888   0.07434   0.0006   0.0156   0.7998
  17.750   1.3174   0.08358   0.07915  -0.0013   0.0154   0.8001
  18.000   1.3075   0.08889   0.08460  -0.0035   0.0153   0.8003
  18.250   1.2957   0.09465   0.09048  -0.0061   0.0151   0.8004
  18.500   1.2814   0.10100   0.09696  -0.0091   0.0150   0.8006
  18.750   1.2651   0.10788   0.10398  -0.0126   0.0149   0.8007
  19.000   1.2486   0.11501   0.11127  -0.0163   0.0148   0.8009
  19.250   1.2306   0.12268   0.11910  -0.0204   0.0148   0.8010
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