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AH 95-160 (ah95160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: AH 95-160 (ah95160-il)
Reynolds number: 1,000,000
Max Cl/Cd: 173.08 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah95160-il-1000000.txt
Download as CSV file: xf-ah95160-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 95-160                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.7377   0.03856   0.03482  -0.1059   0.7069   0.0144
 -13.250  -0.7450   0.03408   0.03014  -0.1106   0.7042   0.0144
 -13.000  -0.7465   0.03157   0.02747  -0.1119   0.7011   0.0145
 -12.750  -0.7368   0.02973   0.02549  -0.1125   0.6990   0.0146
 -12.500  -0.7229   0.02817   0.02381  -0.1129   0.6974   0.0147
 -12.250  -0.7067   0.02675   0.02227  -0.1131   0.6955   0.0149
 -12.000  -0.6885   0.02547   0.02086  -0.1133   0.6936   0.0151
 -11.750  -0.6688   0.02429   0.01954  -0.1135   0.6917   0.0153
 -11.500  -0.6481   0.02316   0.01828  -0.1136   0.6897   0.0155
 -11.250  -0.6261   0.02216   0.01713  -0.1138   0.6878   0.0157
 -11.000  -0.6033   0.02123   0.01606  -0.1139   0.6855   0.0160
 -10.750  -0.5796   0.02042   0.01510  -0.1140   0.6829   0.0162
 -10.500  -0.5547   0.01967   0.01425  -0.1142   0.6816   0.0164
 -10.250  -0.5291   0.01904   0.01352  -0.1144   0.6802   0.0166
 -10.000  -0.5065   0.01771   0.01204  -0.1145   0.6787   0.0169
  -9.750  -0.4814   0.01687   0.01113  -0.1147   0.6771   0.0173
  -9.500  -0.4547   0.01634   0.01054  -0.1149   0.6754   0.0177
  -9.250  -0.4276   0.01590   0.01006  -0.1152   0.6738   0.0181
  -9.000  -0.4001   0.01548   0.00958  -0.1154   0.6721   0.0185
  -8.750  -0.3726   0.01506   0.00908  -0.1157   0.6703   0.0190
  -8.500  -0.3451   0.01466   0.00858  -0.1159   0.6683   0.0194
  -8.250  -0.3172   0.01434   0.00818  -0.1162   0.6659   0.0197
  -8.000  -0.2902   0.01362   0.00740  -0.1164   0.6650   0.0203
  -7.750  -0.2622   0.01316   0.00692  -0.1168   0.6639   0.0209
  -7.500  -0.2337   0.01284   0.00658  -0.1171   0.6625   0.0216
  -7.250  -0.2050   0.01253   0.00624  -0.1174   0.6610   0.0223
  -7.000  -0.1762   0.01226   0.00591  -0.1178   0.6594   0.0230
  -6.750  -0.1477   0.01185   0.00546  -0.1181   0.6577   0.0239
  -6.500  -0.1189   0.01155   0.00515  -0.1185   0.6563   0.0251
  -6.250  -0.0898   0.01135   0.00492  -0.1189   0.6548   0.0263
  -6.000  -0.0607   0.01113   0.00465  -0.1192   0.6533   0.0276
  -5.750  -0.0318   0.01087   0.00438  -0.1196   0.6515   0.0294
  -5.500  -0.0026   0.01076   0.00423  -0.1200   0.6493   0.0312
  -5.250   0.0268   0.01049   0.00397  -0.1205   0.6483   0.0336
  -5.000   0.0563   0.01032   0.00380  -0.1209   0.6471   0.0362
  -4.750   0.0858   0.01011   0.00362  -0.1213   0.6458   0.0397
  -4.500   0.1154   0.00996   0.00347  -0.1218   0.6444   0.0436
  -4.250   0.1450   0.00984   0.00336  -0.1223   0.6429   0.0478
  -4.000   0.1746   0.00968   0.00323  -0.1227   0.6414   0.0526
  -3.750   0.2043   0.00958   0.00311  -0.1232   0.6399   0.0570
  -3.500   0.2340   0.00947   0.00302  -0.1237   0.6383   0.0624
  -3.250   0.2637   0.00937   0.00292  -0.1241   0.6368   0.0676
  -3.000   0.2933   0.00932   0.00287  -0.1246   0.6351   0.0729
  -2.750   0.3229   0.00929   0.00283  -0.1251   0.6330   0.0789
  -2.500   0.3528   0.00920   0.00276  -0.1256   0.6321   0.0848
  -2.250   0.3826   0.00907   0.00268  -0.1261   0.6308   0.0933
  -2.000   0.4124   0.00897   0.00261  -0.1266   0.6294   0.1028
  -1.750   0.4423   0.00884   0.00254  -0.1272   0.6278   0.1190
  -1.500   0.4721   0.00867   0.00249  -0.1278   0.6262   0.1542
  -1.250   0.5020   0.00840   0.00244  -0.1285   0.6247   0.2265
  -1.000   0.5319   0.00804   0.00240  -0.1294   0.6232   0.3385
  -0.750   0.5618   0.00764   0.00239  -0.1302   0.6216   0.4768
  -0.500   0.5916   0.00740   0.00243  -0.1309   0.6199   0.5826
  -0.250   0.6212   0.00735   0.00250  -0.1314   0.6178   0.6441
   0.000   0.6509   0.00732   0.00256  -0.1319   0.6164   0.6829
   0.250   0.6804   0.00726   0.00260  -0.1324   0.6151   0.7168
   0.500   0.7099   0.00722   0.00265  -0.1328   0.6136   0.7437
   0.750   0.7393   0.00720   0.00269  -0.1332   0.6119   0.7709
   1.000   0.7685   0.00719   0.00273  -0.1335   0.6101   0.7929
   1.250   0.7973   0.00718   0.00278  -0.1337   0.6084   0.8192
   1.500   0.8251   0.00717   0.00285  -0.1337   0.6068   0.8507
   1.750   0.8526   0.00719   0.00291  -0.1337   0.6051   0.8775
   2.000   0.8800   0.00724   0.00298  -0.1336   0.6030   0.8955
   2.250   0.9070   0.00732   0.00307  -0.1334   0.6009   0.9110
   2.500   0.9332   0.00731   0.00312  -0.1331   0.5994   0.9255
   2.750   0.9588   0.00730   0.00316  -0.1326   0.5976   0.9399
   3.000   0.9834   0.00729   0.00318  -0.1320   0.5956   0.9559
   3.250   1.0093   0.00726   0.00318  -0.1316   0.5936   0.9760
   3.500   1.0423   0.00727   0.00318  -0.1329   0.5915   0.9998
   3.750   1.0728   0.00733   0.00323  -0.1337   0.5892   0.9998
   4.000   1.1030   0.00746   0.00331  -0.1344   0.5862   0.9998
   4.250   1.1329   0.00750   0.00338  -0.1351   0.5836   0.9998
   4.500   1.1626   0.00752   0.00343  -0.1357   0.5803   0.9998
   4.750   1.1920   0.00754   0.00345  -0.1363   0.5763   0.9998
   5.000   1.2209   0.00762   0.00349  -0.1368   0.5718   0.9998
   5.250   1.2498   0.00767   0.00357  -0.1373   0.5671   0.9998
   5.500   1.2787   0.00770   0.00362  -0.1377   0.5616   0.9998
   5.750   1.3066   0.00781   0.00370  -0.1380   0.5559   0.9998
   6.000   1.3353   0.00788   0.00380  -0.1385   0.5511   0.9998
   6.250   1.3635   0.00797   0.00391  -0.1388   0.5454   0.9998
   6.500   1.3907   0.00812   0.00403  -0.1390   0.5397   0.9998
   6.750   1.4189   0.00821   0.00417  -0.1394   0.5339   0.9998
   7.000   1.4458   0.00836   0.00431  -0.1395   0.5271   0.9998
   7.250   1.4729   0.00851   0.00448  -0.1397   0.5198   0.9998
   7.500   1.4984   0.00872   0.00467  -0.1397   0.5105   0.9998
   7.750   1.5240   0.00892   0.00487  -0.1396   0.4990   0.9998
   8.000   1.5477   0.00922   0.00513  -0.1393   0.4847   0.9998
   8.250   1.5694   0.00960   0.00546  -0.1386   0.4673   0.9998
   8.500   1.5883   0.01011   0.00589  -0.1374   0.4453   0.9998
   8.750   1.6018   0.01086   0.00650  -0.1355   0.4161   0.9998
   9.000   1.6061   0.01186   0.00734  -0.1320   0.3815   0.9998
   9.250   1.6030   0.01322   0.00852  -0.1276   0.3476   0.9998
   9.500   1.5992   0.01489   0.01006  -0.1238   0.3170   0.9998
   9.750   1.5949   0.01692   0.01195  -0.1206   0.2886   0.9998
  10.000   1.5904   0.01921   0.01412  -0.1178   0.2632   0.9998
  10.250   1.5879   0.02149   0.01631  -0.1155   0.2399   0.9998
  10.500   1.5841   0.02393   0.01866  -0.1132   0.2191   0.9998
  10.750   1.5816   0.02627   0.02092  -0.1110   0.2009   0.9998
  11.000   1.5803   0.02852   0.02311  -0.1089   0.1847   0.9998
  11.250   1.5790   0.03076   0.02530  -0.1069   0.1701   0.9998
  11.500   1.5778   0.03300   0.02750  -0.1049   0.1565   0.9998
  11.750   1.5774   0.03521   0.02966  -0.1031   0.1440   0.9998
  12.000   1.5788   0.03732   0.03173  -0.1014   0.1327   0.9998
  12.250   1.5818   0.03936   0.03375  -0.1000   0.1231   0.9998
  12.500   1.5852   0.04138   0.03575  -0.0986   0.1143   0.9998
  12.750   1.5868   0.04360   0.03793  -0.0972   0.1057   0.9998
  13.000   1.5923   0.04549   0.03982  -0.0961   0.0988   0.9998
  13.250   1.5956   0.04762   0.04194  -0.0949   0.0919   0.9998
  13.500   1.6009   0.04960   0.04392  -0.0938   0.0862   0.9998
  13.750   1.6055   0.05161   0.04593  -0.0928   0.0805   0.9998
  14.000   1.6101   0.05370   0.04802  -0.0918   0.0756   0.9998
  14.250   1.6146   0.05579   0.05011  -0.0908   0.0707   0.9998
  14.500   1.6201   0.05782   0.05216  -0.0900   0.0665   0.9998
  14.750   1.6228   0.06015   0.05448  -0.0890   0.0620   0.9998
  15.000   1.6297   0.06204   0.05640  -0.0883   0.0587   0.9998
  15.250   1.6318   0.06446   0.05883  -0.0874   0.0550   0.9998
  15.500   1.6372   0.06656   0.06096  -0.0867   0.0520   0.9998
  15.750   1.6414   0.06880   0.06322  -0.0860   0.0490   0.9998
  16.000   1.6432   0.07135   0.06578  -0.0853   0.0460   0.9998
  16.250   1.6491   0.07342   0.06790  -0.0848   0.0440   0.9998
  16.500   1.6512   0.07594   0.07044  -0.0842   0.0417   0.9998
  16.750   1.6529   0.07853   0.07305  -0.0836   0.0394   0.9998
  17.000   1.6580   0.08075   0.07533  -0.0832   0.0378   0.9998
  17.250   1.6597   0.08340   0.07802  -0.0827   0.0361   0.9998
  17.500   1.6602   0.08618   0.08082  -0.0823   0.0342   0.9998
  17.750   1.6632   0.08871   0.08341  -0.0820   0.0331   0.9998
  18.000   1.6661   0.09123   0.08598  -0.0817   0.0318   0.9998
  18.250   1.6667   0.09407   0.08886  -0.0815   0.0305   0.9998
  18.500   1.6646   0.09727   0.09210  -0.0813   0.0291   0.9998
  18.750   1.6678   0.09981   0.09471  -0.0812   0.0282   0.9998
  19.000   1.6695   0.10260   0.09757  -0.0813   0.0272   0.9998
  19.250   1.6704   0.10545   0.10046  -0.0813   0.0262   0.9998
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