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AH 82-150 F (ah82150f-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AH 82-150 F (ah82150f-il)
Reynolds number: 1,000,000
Max Cl/Cd: 133.8 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah82150f-il-1000000-n5.txt
Download as CSV file: xf-ah82150f-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 82-150 F                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.6033   0.04625   0.04317  -0.1350   0.7844   0.0042
 -14.250  -0.6098   0.04260   0.03942  -0.1370   0.7835   0.0043
 -14.000  -0.6567   0.03616   0.03270  -0.1369   0.7823   0.0042
 -13.750  -0.6604   0.03413   0.03056  -0.1358   0.7813   0.0042
 -13.500  -0.6792   0.03115   0.02736  -0.1330   0.7802   0.0042
 -13.250  -0.6812   0.02948   0.02556  -0.1309   0.7793   0.0043
 -13.000  -0.6789   0.02812   0.02407  -0.1288   0.7784   0.0044
 -12.750  -0.6786   0.02667   0.02245  -0.1263   0.7774   0.0044
 -12.500  -0.6757   0.02539   0.02102  -0.1239   0.7764   0.0044
 -12.250  -0.6671   0.02447   0.01999  -0.1219   0.7757   0.0045
 -12.000  -0.6592   0.02349   0.01890  -0.1197   0.7751   0.0046
 -11.750  -0.6538   0.02235   0.01761  -0.1170   0.7743   0.0046
 -11.500  -0.6457   0.02140   0.01655  -0.1145   0.7735   0.0046
 -11.250  -0.6349   0.02070   0.01574  -0.1122   0.7726   0.0047
 -11.000  -0.6250   0.01980   0.01471  -0.1098   0.7718   0.0047
 -10.750  -0.6151   0.01857   0.01330  -0.1075   0.7711   0.0049
 -10.500  -0.5991   0.01778   0.01239  -0.1060   0.7704   0.0051
 -10.250  -0.5816   0.01704   0.01156  -0.1048   0.7697   0.0054
 -10.000  -0.5619   0.01647   0.01090  -0.1039   0.7690   0.0056
  -9.750  -0.5409   0.01600   0.01036  -0.1031   0.7684   0.0058
  -9.500  -0.5196   0.01553   0.00983  -0.1024   0.7678   0.0060
  -9.250  -0.4972   0.01515   0.00939  -0.1019   0.7672   0.0063
  -9.000  -0.4752   0.01470   0.00887  -0.1013   0.7666   0.0065
  -8.750  -0.4530   0.01424   0.00833  -0.1007   0.7660   0.0068
  -8.500  -0.4301   0.01385   0.00788  -0.1002   0.7654   0.0070
  -8.250  -0.4070   0.01347   0.00743  -0.0997   0.7648   0.0072
  -8.000  -0.3833   0.01314   0.00702  -0.0993   0.7643   0.0073
  -7.750  -0.3606   0.01269   0.00650  -0.0987   0.7637   0.0077
  -7.500  -0.3373   0.01229   0.00605  -0.0982   0.7630   0.0083
  -7.250  -0.3130   0.01201   0.00573  -0.0979   0.7622   0.0088
  -7.000  -0.2886   0.01172   0.00543  -0.0976   0.7617   0.0095
  -6.750  -0.2638   0.01146   0.00514  -0.0974   0.7612   0.0102
  -6.500  -0.2387   0.01123   0.00489  -0.0972   0.7607   0.0109
  -6.250  -0.2140   0.01096   0.00460  -0.0969   0.7602   0.0128
  -6.000  -0.1887   0.01075   0.00440  -0.0968   0.7597   0.0147
  -5.750  -0.1629   0.01057   0.00421  -0.0967   0.7592   0.0160
  -5.500  -0.1375   0.01036   0.00400  -0.0966   0.7586   0.0185
  -5.250  -0.1117   0.01018   0.00383  -0.0965   0.7580   0.0207
  -5.000  -0.0854   0.01004   0.00367  -0.0965   0.7574   0.0225
  -4.750  -0.0593   0.00988   0.00350  -0.0965   0.7569   0.0245
  -4.500  -0.0332   0.00972   0.00335  -0.0965   0.7562   0.0276
  -4.250  -0.0067   0.00959   0.00324  -0.0965   0.7555   0.0313
  -4.000   0.0199   0.00947   0.00310  -0.0966   0.7548   0.0338
  -3.750   0.0464   0.00932   0.00296  -0.0966   0.7541   0.0384
  -3.500   0.0731   0.00920   0.00285  -0.0967   0.7536   0.0428
  -3.250   0.0999   0.00909   0.00274  -0.0969   0.7530   0.0482
  -3.000   0.1267   0.00897   0.00265  -0.0970   0.7524   0.0554
  -2.750   0.1534   0.00883   0.00255  -0.0971   0.7518   0.0678
  -2.500   0.1795   0.00865   0.00246  -0.0971   0.7511   0.0949
  -2.250   0.2050   0.00842   0.00237  -0.0970   0.7504   0.1382
  -2.000   0.2299   0.00815   0.00229  -0.0969   0.7497   0.2000
  -1.750   0.2541   0.00783   0.00221  -0.0967   0.7486   0.2828
  -1.500   0.2776   0.00747   0.00214  -0.0963   0.7471   0.3665
  -1.250   0.3018   0.00715   0.00206  -0.0960   0.7451   0.4391
  -1.000   0.3247   0.00669   0.00195  -0.0955   0.7429   0.5484
  -0.750   0.3414   0.00597   0.00206  -0.0935   0.7407   0.7977
  -0.500   0.3695   0.00607   0.00217  -0.0937   0.7386   0.8223
  -0.250   0.3982   0.00612   0.00218  -0.0940   0.7364   0.8296
   0.000   0.4272   0.00616   0.00216  -0.0945   0.7345   0.8332
   0.250   0.4550   0.00619   0.00223  -0.0947   0.7326   0.8363
   0.500   0.4829   0.00625   0.00230  -0.0949   0.7307   0.8400
   0.750   0.5111   0.00634   0.00239  -0.0952   0.7286   0.8466
   1.000   0.5380   0.00642   0.00250  -0.0951   0.7264   0.8512
   1.250   0.5661   0.00645   0.00253  -0.0953   0.7243   0.8534
   1.500   0.5948   0.00644   0.00251  -0.0958   0.7223   0.8541
   1.750   0.6233   0.00644   0.00251  -0.0963   0.7201   0.8546
   2.000   0.6515   0.00643   0.00253  -0.0967   0.7172   0.8552
   2.250   0.6797   0.00643   0.00253  -0.0971   0.7139   0.8557
   2.500   0.7079   0.00642   0.00253  -0.0975   0.7105   0.8563
   2.750   0.7360   0.00641   0.00252  -0.0979   0.7072   0.8568
   3.000   0.7638   0.00642   0.00257  -0.0983   0.7025   0.8575
   3.250   0.7912   0.00642   0.00257  -0.0985   0.6967   0.8581
   3.500   0.8185   0.00643   0.00260  -0.0987   0.6897   0.8586
   3.750   0.8448   0.00645   0.00261  -0.0987   0.6802   0.8591
   4.000   0.8697   0.00650   0.00264  -0.0984   0.6651   0.8596
   4.250   0.8798   0.00687   0.00275  -0.0950   0.6144   0.8604
   4.500   0.8875   0.00733   0.00304  -0.0912   0.5747   0.8613
   4.750   0.8958   0.00772   0.00331  -0.0876   0.5454   0.8622
   5.000   0.8937   0.00815   0.00362  -0.0818   0.5147   0.8634
   5.250   0.8888   0.00880   0.00412  -0.0757   0.4795   0.8649
   5.500   0.8860   0.00953   0.00471  -0.0704   0.4465   0.8664
   5.750   0.8877   0.01026   0.00532  -0.0661   0.4170   0.8676
   6.000   0.8913   0.01102   0.00596  -0.0623   0.3875   0.8687
   6.250   0.8910   0.01200   0.00675  -0.0581   0.3467   0.8700
   6.500   0.8879   0.01316   0.00765  -0.0536   0.2943   0.8712
   6.750   0.8847   0.01442   0.00859  -0.0492   0.2339   0.8724
   7.000   0.8782   0.01591   0.00968  -0.0445   0.1591   0.8735
   7.250   0.8714   0.01754   0.01087  -0.0400   0.0753   0.8744
   7.500   0.8716   0.01892   0.01194  -0.0365   0.0132   0.8753
   7.750   0.8890   0.01942   0.01245  -0.0355   0.0109   0.8761
   8.000   0.9055   0.01998   0.01302  -0.0344   0.0087   0.8769
   8.250   0.9232   0.02049   0.01356  -0.0335   0.0078   0.8775
   8.500   0.9404   0.02102   0.01413  -0.0325   0.0073   0.8782
   8.750   0.9570   0.02160   0.01474  -0.0315   0.0068   0.8788
   9.000   0.9725   0.02226   0.01543  -0.0303   0.0062   0.8795
   9.250   0.9873   0.02298   0.01618  -0.0291   0.0055   0.8802
   9.500   1.0014   0.02375   0.01701  -0.0279   0.0053   0.8809
   9.750   1.0183   0.02436   0.01764  -0.0270   0.0050   0.8816
  10.000   1.0333   0.02510   0.01842  -0.0260   0.0048   0.8823
  10.250   1.0474   0.02591   0.01929  -0.0248   0.0046   0.8830
  10.500   1.0627   0.02665   0.02006  -0.0239   0.0043   0.8838
  10.750   1.0765   0.02751   0.02096  -0.0228   0.0041   0.8845
  11.000   1.0910   0.02833   0.02182  -0.0219   0.0038   0.8853
  11.250   1.1030   0.02935   0.02288  -0.0207   0.0036   0.8860
  11.500   1.1135   0.03049   0.02406  -0.0194   0.0033   0.8868
  11.750   1.1224   0.03178   0.02542  -0.0180   0.0032   0.8875
  12.000   1.1301   0.03321   0.02692  -0.0165   0.0031   0.8882
  12.500   1.1552   0.03534   0.02918  -0.0147   0.0029   0.8897
  12.750   1.1640   0.03674   0.03065  -0.0136   0.0029   0.8906
  13.000   1.1711   0.03830   0.03230  -0.0124   0.0028   0.8915
  13.250   1.1785   0.03990   0.03398  -0.0112   0.0027   0.8925
  13.500   1.1915   0.04102   0.03515  -0.0106   0.0025   0.8936
  13.750   1.1960   0.04293   0.03716  -0.0094   0.0025   0.8947
  14.000   1.2053   0.04445   0.03875  -0.0087   0.0023   0.8958
  14.250   1.2087   0.04660   0.04099  -0.0077   0.0024   0.8969
  14.500   1.2159   0.04842   0.04289  -0.0070   0.0023   0.8979
  14.750   1.2234   0.05025   0.04481  -0.0065   0.0022   0.8989
  15.000   1.2289   0.05233   0.04697  -0.0059   0.0021   0.9000
  15.250   1.2350   0.05440   0.04913  -0.0055   0.0021   0.9010
  15.500   1.2375   0.05693   0.05176  -0.0050   0.0021   0.9019
  16.000   1.2492   0.06139   0.05637  -0.0047   0.0019   0.9042
  16.250   1.2511   0.06412   0.05921  -0.0046   0.0019   0.9054
  16.500   1.2550   0.06671   0.06188  -0.0047   0.0018   0.9068
  16.750   1.2515   0.07027   0.06560  -0.0047   0.0019   0.9080
  17.000   1.2543   0.07315   0.06857  -0.0051   0.0018   0.9095
  17.250   1.2532   0.07660   0.07215  -0.0055   0.0019   0.9109
  17.500   1.2516   0.08021   0.07587  -0.0061   0.0018   0.9123
  17.750   1.2483   0.08414   0.07992  -0.0069   0.0018   0.9137
  18.000   1.2446   0.08825   0.08416  -0.0080   0.0017   0.9150
  18.500   1.2366   0.09680   0.09300  -0.0105   0.0017   0.9182
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