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AH 82-150 A (ah82150a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 82-150 A (ah82150a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 129.95 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah82150a-il-1000000-n5.txt
Download as CSV file: xf-ah82150a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 82-150 A                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.8363   0.04696   0.04426  -0.1080   0.9360   0.0051
 -15.500  -0.8222   0.04055   0.03753  -0.1192   0.9167   0.0052
 -15.250  -0.8189   0.03648   0.03314  -0.1240   0.8882   0.0052
 -15.000  -0.8123   0.03470   0.03118  -0.1245   0.8685   0.0054
 -14.750  -0.8165   0.03233   0.02860  -0.1240   0.8528   0.0054
 -14.500  -0.8168   0.03046   0.02655  -0.1232   0.8407   0.0054
 -14.250  -0.8110   0.02910   0.02507  -0.1224   0.8314   0.0056
 -14.000  -0.8084   0.02757   0.02339  -0.1212   0.8235   0.0056
 -13.750  -0.8038   0.02620   0.02188  -0.1199   0.8161   0.0057
 -13.500  -0.7938   0.02525   0.02081  -0.1188   0.8099   0.0060
 -13.250  -0.7862   0.02414   0.01959  -0.1174   0.8037   0.0060
 -13.000  -0.7760   0.02324   0.01857  -0.1161   0.7980   0.0061
 -12.750  -0.7668   0.02226   0.01747  -0.1146   0.7932   0.0062
 -12.500  -0.7558   0.02143   0.01653  -0.1131   0.7885   0.0063
 -12.250  -0.7438   0.02070   0.01569  -0.1116   0.7841   0.0064
 -12.000  -0.7317   0.02001   0.01491  -0.1100   0.7802   0.0065
 -11.750  -0.7220   0.01924   0.01404  -0.1078   0.7759   0.0065
 -11.500  -0.7127   0.01848   0.01317  -0.1055   0.7717   0.0068
 -11.000  -0.6797   0.01717   0.01167  -0.1031   0.7652   0.0073
 -10.750  -0.6604   0.01664   0.01108  -0.1022   0.7620   0.0075
 -10.500  -0.6404   0.01615   0.01052  -0.1015   0.7588   0.0077
 -10.250  -0.6197   0.01571   0.01001  -0.1007   0.7557   0.0080
 -10.000  -0.5983   0.01528   0.00951  -0.1001   0.7529   0.0084
  -9.750  -0.5764   0.01484   0.00901  -0.0995   0.7500   0.0086
  -9.500  -0.5540   0.01443   0.00854  -0.0990   0.7472   0.0090
  -9.250  -0.5311   0.01405   0.00808  -0.0986   0.7445   0.0092
  -9.000  -0.5086   0.01362   0.00759  -0.0980   0.7418   0.0097
  -8.500  -0.4615   0.01291   0.00681  -0.0973   0.7369   0.0109
  -8.250  -0.4369   0.01262   0.00649  -0.0971   0.7342   0.0118
  -8.000  -0.4121   0.01234   0.00618  -0.0969   0.7316   0.0125
  -7.750  -0.3871   0.01209   0.00588  -0.0967   0.7292   0.0130
  -7.500  -0.3627   0.01176   0.00551  -0.0964   0.7268   0.0143
  -7.250  -0.3375   0.01152   0.00525  -0.0963   0.7244   0.0153
  -7.000  -0.3115   0.01128   0.00500  -0.0962   0.7222   0.0164
  -6.750  -0.2855   0.01106   0.00475  -0.0962   0.7197   0.0173
  -6.500  -0.2595   0.01084   0.00450  -0.0962   0.7174   0.0181
  -6.250  -0.2336   0.01059   0.00423  -0.0961   0.7150   0.0198
  -6.000  -0.2073   0.01041   0.00404  -0.0961   0.7126   0.0214
  -5.750  -0.1808   0.01026   0.00385  -0.0962   0.7103   0.0228
  -5.500  -0.1536   0.01010   0.00368  -0.0963   0.7083   0.0238
  -5.250  -0.1270   0.00986   0.00343  -0.0964   0.7060   0.0259
  -5.000  -0.1000   0.00968   0.00324  -0.0965   0.7036   0.0280
  -4.750  -0.0729   0.00952   0.00308  -0.0966   0.7012   0.0298
  -4.500  -0.0456   0.00939   0.00292  -0.0968   0.6989   0.0315
  -4.250  -0.0183   0.00926   0.00275  -0.0969   0.6968   0.0336
  -4.000   0.0091   0.00910   0.00260  -0.0971   0.6948   0.0372
  -3.750   0.0369   0.00895   0.00246  -0.0974   0.6925   0.0409
  -3.500   0.0647   0.00882   0.00234  -0.0976   0.6902   0.0461
  -3.250   0.0925   0.00868   0.00222  -0.0978   0.6879   0.0533
  -3.000   0.1201   0.00854   0.00210  -0.0981   0.6855   0.0654
  -2.750   0.1476   0.00838   0.00199  -0.0983   0.6832   0.0859
  -2.500   0.1749   0.00813   0.00188  -0.0986   0.6810   0.1271
  -2.250   0.2025   0.00785   0.00177  -0.0990   0.6788   0.1824
  -2.000   0.2303   0.00757   0.00168  -0.0995   0.6763   0.2418
  -1.750   0.2580   0.00725   0.00158  -0.0999   0.6736   0.3141
  -1.500   0.2852   0.00662   0.00140  -0.1006   0.6710   0.4643
  -1.250   0.3126   0.00601   0.00133  -0.1013   0.6684   0.6406
  -1.000   0.3414   0.00603   0.00144  -0.1016   0.6656   0.6866
  -0.750   0.3702   0.00611   0.00154  -0.1018   0.6621   0.7058
  -0.500   0.3992   0.00617   0.00155  -0.1022   0.6580   0.7125
  -0.250   0.4274   0.00622   0.00159  -0.1024   0.6539   0.7172
   0.000   0.4562   0.00627   0.00164  -0.1027   0.6501   0.7225
   0.250   0.4852   0.00631   0.00166  -0.1031   0.6462   0.7254
   0.500   0.5139   0.00634   0.00166  -0.1035   0.6425   0.7265
   0.750   0.5425   0.00639   0.00166  -0.1039   0.6390   0.7274
   1.000   0.5714   0.00640   0.00168  -0.1043   0.6354   0.7283
   1.250   0.6000   0.00642   0.00169  -0.1046   0.6312   0.7292
   1.500   0.6283   0.00645   0.00172  -0.1049   0.6269   0.7300
   1.750   0.6567   0.00649   0.00175  -0.1052   0.6226   0.7308
   2.000   0.6852   0.00652   0.00179  -0.1056   0.6179   0.7316
   2.250   0.7132   0.00657   0.00184  -0.1058   0.6126   0.7325
   2.500   0.7414   0.00662   0.00189  -0.1061   0.6078   0.7333
   2.750   0.7695   0.00667   0.00194  -0.1064   0.6020   0.7344
   3.250   0.8251   0.00680   0.00208  -0.1068   0.5900   0.7364
   3.500   0.8522   0.00689   0.00216  -0.1069   0.5828   0.7374
   3.750   0.8797   0.00697   0.00224  -0.1071   0.5745   0.7383
   4.000   0.9063   0.00708   0.00234  -0.1071   0.5652   0.7392
   4.250   0.9325   0.00720   0.00245  -0.1070   0.5539   0.7401
   4.500   0.9577   0.00737   0.00257  -0.1067   0.5383   0.7410
   4.750   0.9794   0.00769   0.00277  -0.1058   0.5065   0.7419
   5.000   0.9968   0.00821   0.00308  -0.1041   0.4603   0.7429
   5.250   1.0122   0.00880   0.00345  -0.1021   0.4128   0.7440
   5.500   1.0249   0.00950   0.00389  -0.0996   0.3603   0.7453
   5.750   1.0359   0.01022   0.00436  -0.0969   0.3089   0.7466
   6.000   1.0405   0.01113   0.00494  -0.0930   0.2458   0.7480
   6.250   1.0395   0.01198   0.00552  -0.0880   0.1927   0.7495
   6.500   1.0410   0.01285   0.00618  -0.0837   0.1478   0.7510
   6.750   1.0419   0.01381   0.00694  -0.0794   0.1043   0.7524
   7.000   1.0444   0.01479   0.00774  -0.0757   0.0680   0.7539
   7.500   1.0538   0.01683   0.00951  -0.0695   0.0141   0.7566
   7.750   1.0686   0.01743   0.01012  -0.0680   0.0112   0.7578
   8.000   1.0831   0.01806   0.01077  -0.0665   0.0096   0.7592
   8.250   1.0975   0.01872   0.01148  -0.0651   0.0085   0.7606
   8.500   1.1127   0.01936   0.01215  -0.0638   0.0080   0.7620
   8.750   1.1275   0.02005   0.01288  -0.0625   0.0076   0.7636
   9.000   1.1420   0.02076   0.01364  -0.0613   0.0072   0.7653
   9.250   1.1555   0.02156   0.01447  -0.0599   0.0068   0.7671
   9.500   1.1686   0.02241   0.01535  -0.0586   0.0064   0.7688
   9.750   1.1795   0.02343   0.01643  -0.0571   0.0059   0.7703
  10.000   1.1926   0.02432   0.01735  -0.0559   0.0057   0.7717
  10.250   1.2061   0.02519   0.01828  -0.0547   0.0055   0.7734
  10.500   1.2186   0.02615   0.01930  -0.0536   0.0054   0.7751
  10.750   1.2303   0.02719   0.02039  -0.0523   0.0051   0.7769
  11.000   1.2416   0.02827   0.02153  -0.0512   0.0050   0.7788
  11.250   1.2531   0.02937   0.02268  -0.0501   0.0049   0.7808
  11.500   1.2635   0.03057   0.02395  -0.0489   0.0047   0.7828
  11.750   1.2736   0.03183   0.02526  -0.0478   0.0045   0.7848
  12.250   1.2929   0.03451   0.02805  -0.0458   0.0042   0.7888
  12.500   1.3006   0.03605   0.02966  -0.0447   0.0041   0.7912
  12.750   1.3054   0.03791   0.03160  -0.0435   0.0039   0.7937
  13.000   1.3084   0.04000   0.03379  -0.0423   0.0038   0.7965
  13.250   1.3167   0.04166   0.03551  -0.0416   0.0037   0.7992
  13.500   1.3244   0.04341   0.03734  -0.0409   0.0037   0.8019
  13.750   1.3336   0.04504   0.03906  -0.0404   0.0036   0.8048
  14.000   1.3377   0.04723   0.04135  -0.0397   0.0036   0.8079
  14.250   1.3465   0.04900   0.04319  -0.0393   0.0035   0.8113
  14.500   1.3536   0.05100   0.04526  -0.0389   0.0034   0.8146
  14.750   1.3591   0.05320   0.04756  -0.0385   0.0033   0.8181
  15.000   1.3653   0.05535   0.04980  -0.0383   0.0032   0.8221
  15.250   1.3697   0.05778   0.05233  -0.0381   0.0031   0.8264
  15.750   1.3760   0.06312   0.05787  -0.0380   0.0030   0.8361
  16.000   1.3798   0.06580   0.06065  -0.0381   0.0029   0.8420
  16.250   1.3813   0.06882   0.06378  -0.0383   0.0029   0.8485
  16.500   1.3817   0.07205   0.06715  -0.0386   0.0028   0.8566
  16.750   1.3847   0.07497   0.07019  -0.0390   0.0028   0.8678
  17.000   1.3850   0.07825   0.07361  -0.0394   0.0027   0.8859
  17.250   1.3837   0.08128   0.07688  -0.0395   0.0027   1.0000
  17.500   1.3839   0.08484   0.08054  -0.0404   0.0026   1.0000
  17.750   1.3836   0.08857   0.08436  -0.0415   0.0026   1.0000
  18.000   1.3816   0.09264   0.08852  -0.0427   0.0026   1.0000
  18.250   1.3807   0.09659   0.09257  -0.0440   0.0025   1.0000
  18.500   1.3777   0.10095   0.09702  -0.0456   0.0025   1.0000
  18.750   1.3742   0.10543   0.10161  -0.0473   0.0025   1.0000
  19.000   1.3707   0.11001   0.10629  -0.0491   0.0024   1.0000
  19.250   1.3664   0.11479   0.11117  -0.0512   0.0024   1.0000
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