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AH 94-156 (ah94156-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 94-156 (ah94156-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.43 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah94156-il-1000000-n5.txt
Download as CSV file: xf-ah94156-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 94-156                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.7164   0.05069   0.04742  -0.1043   0.7811   0.0059
 -14.750  -0.7420   0.04408   0.04061  -0.1083   0.7779   0.0059
 -14.500  -0.7694   0.03889   0.03521  -0.1095   0.7749   0.0059
 -14.250  -0.7756   0.03629   0.03248  -0.1092   0.7723   0.0059
 -14.000  -0.7855   0.03369   0.02973  -0.1081   0.7693   0.0059
 -13.750  -0.7795   0.03241   0.02835  -0.1071   0.7664   0.0060
 -13.500  -0.7830   0.03055   0.02633  -0.1052   0.7633   0.0060
 -13.250  -0.7865   0.02877   0.02438  -0.1030   0.7604   0.0060
 -13.000  -0.7835   0.02743   0.02293  -0.1010   0.7580   0.0061
 -12.750  -0.7800   0.02614   0.02152  -0.0988   0.7556   0.0061
 -12.500  -0.7855   0.02429   0.01949  -0.0955   0.7529   0.0063
 -12.250  -0.7796   0.02322   0.01830  -0.0931   0.7504   0.0063
 -12.000  -0.7722   0.02227   0.01724  -0.0908   0.7480   0.0064
 -11.750  -0.7625   0.02152   0.01638  -0.0885   0.7457   0.0065
 -11.500  -0.7512   0.02086   0.01563  -0.0863   0.7436   0.0066
 -11.250  -0.7357   0.02023   0.01494  -0.0848   0.7415   0.0067
 -11.000  -0.7175   0.01969   0.01433  -0.0837   0.7394   0.0069
 -10.750  -0.6993   0.01908   0.01364  -0.0826   0.7374   0.0070
 -10.500  -0.6810   0.01843   0.01289  -0.0815   0.7354   0.0070
 -10.250  -0.6604   0.01794   0.01233  -0.0807   0.7334   0.0073
 -10.000  -0.6403   0.01737   0.01166  -0.0798   0.7314   0.0074
  -9.750  -0.6195   0.01681   0.01101  -0.0790   0.7295   0.0075
  -9.500  -0.5976   0.01629   0.01043  -0.0783   0.7278   0.0077
  -9.250  -0.5756   0.01576   0.00983  -0.0777   0.7261   0.0079
  -9.000  -0.5528   0.01530   0.00929  -0.0771   0.7243   0.0080
  -8.750  -0.5293   0.01489   0.00882  -0.0767   0.7225   0.0082
  -8.500  -0.5058   0.01448   0.00834  -0.0762   0.7206   0.0083
  -8.250  -0.4826   0.01402   0.00781  -0.0757   0.7188   0.0085
  -8.000  -0.4595   0.01353   0.00727  -0.0752   0.7169   0.0089
  -7.750  -0.4348   0.01323   0.00693  -0.0749   0.7151   0.0092
  -7.500  -0.4097   0.01291   0.00658  -0.0747   0.7137   0.0095
  -7.250  -0.3843   0.01260   0.00625  -0.0745   0.7122   0.0099
  -7.000  -0.3590   0.01229   0.00591  -0.0743   0.7106   0.0102
  -6.750  -0.3335   0.01199   0.00557  -0.0741   0.7087   0.0106
  -6.500  -0.3078   0.01172   0.00526  -0.0739   0.7068   0.0109
  -6.250  -0.2819   0.01146   0.00495  -0.0738   0.7050   0.0111
  -6.000  -0.2566   0.01113   0.00460  -0.0735   0.7033   0.0118
  -5.750  -0.2306   0.01089   0.00433  -0.0734   0.7017   0.0124
  -5.500  -0.2042   0.01069   0.00410  -0.0734   0.6999   0.0131
  -5.250  -0.1774   0.01048   0.00388  -0.0734   0.6984   0.0139
  -5.000  -0.1505   0.01029   0.00368  -0.0734   0.6966   0.0147
  -4.750  -0.1239   0.01006   0.00346  -0.0734   0.6948   0.0159
  -4.500  -0.0969   0.00988   0.00327  -0.0734   0.6929   0.0172
  -4.250  -0.0697   0.00973   0.00309  -0.0735   0.6909   0.0184
  -4.000  -0.0428   0.00954   0.00292  -0.0735   0.6890   0.0209
  -3.750  -0.0156   0.00941   0.00277  -0.0736   0.6871   0.0233
  -3.500   0.0115   0.00926   0.00262  -0.0737   0.6852   0.0280
  -3.250   0.0389   0.00910   0.00250  -0.0738   0.6836   0.0345
  -3.000   0.0663   0.00894   0.00238  -0.0739   0.6818   0.0435
  -2.750   0.0936   0.00877   0.00227  -0.0741   0.6795   0.0581
  -2.500   0.1203   0.00856   0.00215  -0.0741   0.6771   0.0845
  -2.250   0.1470   0.00834   0.00205  -0.0742   0.6748   0.1193
  -2.000   0.1730   0.00807   0.00194  -0.0741   0.6724   0.1724
  -1.750   0.1984   0.00775   0.00184  -0.0741   0.6699   0.2429
  -1.500   0.2237   0.00737   0.00176  -0.0740   0.6671   0.3311
  -1.250   0.2484   0.00695   0.00166  -0.0738   0.6637   0.4305
  -1.000   0.2712   0.00637   0.00155  -0.0734   0.6606   0.5746
  -0.750   0.2924   0.00578   0.00150  -0.0724   0.6577   0.7308
  -0.500   0.3184   0.00585   0.00174  -0.0719   0.6550   0.7951
  -0.250   0.3476   0.00592   0.00179  -0.0722   0.6518   0.8098
   0.000   0.3764   0.00600   0.00186  -0.0725   0.6485   0.8184
   0.250   0.4052   0.00609   0.00191  -0.0729   0.6449   0.8266
   0.500   0.4334   0.00619   0.00198  -0.0730   0.6415   0.8313
   0.750   0.4620   0.00628   0.00208  -0.0732   0.6382   0.8357
   1.000   0.4907   0.00637   0.00215  -0.0735   0.6344   0.8401
   1.250   0.5193   0.00644   0.00219  -0.0739   0.6305   0.8434
   1.500   0.5470   0.00652   0.00226  -0.0740   0.6268   0.8459
   1.750   0.5752   0.00659   0.00234  -0.0742   0.6224   0.8482
   2.000   0.6032   0.00666   0.00240  -0.0744   0.6169   0.8504
   2.250   0.6309   0.00674   0.00245  -0.0745   0.6114   0.8522
   2.500   0.6593   0.00678   0.00249  -0.0749   0.6059   0.8536
   2.750   0.6871   0.00685   0.00253  -0.0751   0.5995   0.8548
   3.000   0.7150   0.00691   0.00258  -0.0754   0.5932   0.8559
   3.250   0.7423   0.00699   0.00263  -0.0756   0.5842   0.8567
   3.500   0.7695   0.00708   0.00269  -0.0757   0.5747   0.8575
   3.750   0.7962   0.00718   0.00276  -0.0758   0.5655   0.8581
   4.000   0.8223   0.00729   0.00283  -0.0757   0.5543   0.8587
   4.250   0.8470   0.00743   0.00293  -0.0754   0.5395   0.8593
   4.500   0.8713   0.00760   0.00305  -0.0751   0.5248   0.8600
   4.750   0.8957   0.00776   0.00317  -0.0747   0.5113   0.8605
   5.000   0.9188   0.00797   0.00333  -0.0741   0.4957   0.8611
   5.250   0.9408   0.00820   0.00351  -0.0733   0.4794   0.8617
   5.500   0.9621   0.00845   0.00371  -0.0724   0.4635   0.8624
   5.750   0.9830   0.00870   0.00391  -0.0715   0.4483   0.8631
   6.250   1.0224   0.00921   0.00434  -0.0691   0.4193   0.8642
   6.500   1.0411   0.00947   0.00456  -0.0678   0.4064   0.8648
   6.750   1.0530   0.00978   0.00482  -0.0650   0.3901   0.8656
   7.000   1.0616   0.01018   0.00516  -0.0618   0.3719   0.8668
   7.250   1.0699   0.01068   0.00558  -0.0586   0.3515   0.8677
   7.500   1.0778   0.01124   0.00607  -0.0556   0.3319   0.8685
   7.750   1.0842   0.01192   0.00666  -0.0525   0.3106   0.8694
   8.000   1.0926   0.01260   0.00726  -0.0499   0.2907   0.8701
   8.250   1.0963   0.01352   0.00806  -0.0467   0.2646   0.8709
   8.500   1.1043   0.01434   0.00879  -0.0443   0.2443   0.8715
   8.750   1.1091   0.01534   0.00966  -0.0416   0.2201   0.8722
   9.000   1.1122   0.01647   0.01065  -0.0387   0.1925   0.8728
   9.250   1.1148   0.01766   0.01170  -0.0359   0.1646   0.8737
   9.500   1.1218   0.01867   0.01262  -0.0338   0.1445   0.8745
   9.750   1.1266   0.01984   0.01368  -0.0315   0.1216   0.8752
  10.000   1.1311   0.02108   0.01480  -0.0292   0.1003   0.8758
  10.250   1.1366   0.02229   0.01592  -0.0272   0.0804   0.8764
  10.500   1.1443   0.02343   0.01699  -0.0255   0.0665   0.8770
  10.750   1.1534   0.02450   0.01803  -0.0240   0.0559   0.8775
  11.000   1.1629   0.02559   0.01909  -0.0226   0.0465   0.8781
  11.250   1.1710   0.02680   0.02027  -0.0212   0.0370   0.8786
  11.500   1.1817   0.02788   0.02134  -0.0200   0.0314   0.8791
  11.750   1.1908   0.02911   0.02254  -0.0188   0.0252   0.8796
  12.000   1.2014   0.03025   0.02369  -0.0178   0.0219   0.8802
  12.250   1.2120   0.03143   0.02489  -0.0169   0.0184   0.8807
  12.500   1.2220   0.03269   0.02616  -0.0159   0.0155   0.8812
  12.750   1.2327   0.03391   0.02740  -0.0151   0.0138   0.8817
  13.000   1.2427   0.03523   0.02874  -0.0143   0.0121   0.8822
  13.250   1.2529   0.03656   0.03010  -0.0136   0.0107   0.8827
  13.500   1.2622   0.03800   0.03158  -0.0128   0.0097   0.8833
  13.750   1.2729   0.03933   0.03296  -0.0122   0.0090   0.8837
  14.000   1.2817   0.04086   0.03453  -0.0116   0.0082   0.8842
  14.250   1.2902   0.04246   0.03617  -0.0110   0.0076   0.8847
  14.500   1.2989   0.04408   0.03784  -0.0105   0.0070   0.8852
  14.750   1.3077   0.04572   0.03953  -0.0101   0.0066   0.8857
  15.000   1.3154   0.04749   0.04135  -0.0097   0.0063   0.8861
  15.250   1.3223   0.04937   0.04328  -0.0093   0.0059   0.8866
  15.500   1.3287   0.05136   0.04532  -0.0090   0.0057   0.8871
  16.000   1.3402   0.05557   0.04968  -0.0086   0.0052   0.8884
  16.250   1.3461   0.05773   0.05191  -0.0085   0.0051   0.8890
  16.500   1.3516   0.05996   0.05421  -0.0085   0.0048   0.8896
  16.750   1.3561   0.06236   0.05669  -0.0086   0.0049   0.8902
  17.000   1.3597   0.06491   0.05931  -0.0087   0.0046   0.8907
  17.250   1.3629   0.06757   0.06205  -0.0089   0.0044   0.8913
  17.500   1.3655   0.07036   0.06491  -0.0093   0.0043   0.8918
  17.750   1.3671   0.07330   0.06794  -0.0098   0.0042   0.8924
  18.000   1.3681   0.07639   0.07112  -0.0103   0.0041   0.8929
  18.250   1.3690   0.07959   0.07439  -0.0110   0.0040   0.8935
  18.500   1.3639   0.08368   0.07858  -0.0119   0.0037   0.8940
  18.750   1.3650   0.08695   0.08194  -0.0129   0.0037   0.8946
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