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AH 95-160 (ah95160-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AH 95-160 (ah95160-il)
Reynolds number: 500,000
Max Cl/Cd: 128.07 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ah95160-il-500000-n5.txt
Download as CSV file: xf-ah95160-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.6762   0.04627   0.04188  -0.0980   0.6998   0.0139
 -13.000  -0.6961   0.03798   0.03329  -0.1078   0.6980   0.0139
 -12.750  -0.7011   0.03431   0.02944  -0.1110   0.6958   0.0140
 -12.500  -0.6974   0.03209   0.02707  -0.1118   0.6937   0.0141
 -12.250  -0.6857   0.03033   0.02516  -0.1124   0.6914   0.0143
 -12.000  -0.6706   0.02885   0.02352  -0.1127   0.6892   0.0144
 -11.750  -0.6532   0.02754   0.02207  -0.1130   0.6870   0.0146
 -11.500  -0.6340   0.02636   0.02074  -0.1132   0.6850   0.0148
 -11.000  -0.5919   0.02426   0.01835  -0.1136   0.6815   0.0154
 -10.750  -0.5695   0.02326   0.01721  -0.1138   0.6798   0.0157
 -10.500  -0.5463   0.02232   0.01612  -0.1139   0.6781   0.0161
 -10.250  -0.5225   0.02143   0.01507  -0.1141   0.6763   0.0164
 -10.000  -0.4980   0.02062   0.01411  -0.1143   0.6745   0.0166
  -9.750  -0.4738   0.01975   0.01314  -0.1144   0.6726   0.0169
  -9.500  -0.4484   0.01907   0.01239  -0.1146   0.6708   0.0172
  -9.250  -0.4224   0.01849   0.01172  -0.1148   0.6690   0.0176
  -9.000  -0.3961   0.01796   0.01109  -0.1150   0.6673   0.0180
  -8.750  -0.3694   0.01744   0.01048  -0.1153   0.6658   0.0184
  -8.500  -0.3424   0.01692   0.00988  -0.1155   0.6644   0.0189
  -8.250  -0.3151   0.01643   0.00931  -0.1158   0.6629   0.0194
  -8.000  -0.2876   0.01596   0.00876  -0.1160   0.6613   0.0199
  -7.750  -0.2602   0.01549   0.00826  -0.1163   0.6596   0.0206
  -7.500  -0.2323   0.01513   0.00786  -0.1166   0.6578   0.0214
  -7.250  -0.2042   0.01478   0.00746  -0.1169   0.6561   0.0222
  -7.000  -0.1760   0.01445   0.00704  -0.1172   0.6545   0.0231
  -6.750  -0.1479   0.01408   0.00663  -0.1175   0.6530   0.0240
  -6.500  -0.1196   0.01378   0.00629  -0.1178   0.6516   0.0250
  -6.250  -0.0911   0.01352   0.00597  -0.1181   0.6501   0.0262
  -6.000  -0.0625   0.01326   0.00566  -0.1184   0.6487   0.0275
  -5.750  -0.0337   0.01299   0.00540  -0.1188   0.6471   0.0292
  -5.500  -0.0048   0.01277   0.00515  -0.1192   0.6455   0.0313
  -5.250   0.0241   0.01253   0.00493  -0.1196   0.6439   0.0336
  -5.000   0.0532   0.01234   0.00471  -0.1200   0.6424   0.0362
  -4.750   0.0822   0.01214   0.00452  -0.1204   0.6409   0.0391
  -4.500   0.1114   0.01198   0.00433  -0.1208   0.6393   0.0426
  -4.250   0.1405   0.01182   0.00418  -0.1212   0.6377   0.0466
  -4.000   0.1697   0.01168   0.00402  -0.1216   0.6361   0.0507
  -3.750   0.1990   0.01158   0.00389  -0.1220   0.6346   0.0553
  -3.500   0.2282   0.01147   0.00378  -0.1224   0.6332   0.0602
  -3.250   0.2576   0.01137   0.00368  -0.1228   0.6319   0.0649
  -3.000   0.2870   0.01124   0.00359  -0.1233   0.6305   0.0707
  -2.750   0.3164   0.01114   0.00350  -0.1237   0.6289   0.0763
  -2.500   0.3458   0.01103   0.00342  -0.1242   0.6271   0.0831
  -2.250   0.3753   0.01093   0.00333  -0.1246   0.6254   0.0901
  -2.000   0.4047   0.01085   0.00326  -0.1251   0.6237   0.0986
  -1.750   0.4342   0.01074   0.00319  -0.1256   0.6223   0.1112
  -1.500   0.4636   0.01063   0.00313  -0.1261   0.6208   0.1302
  -1.250   0.4930   0.01048   0.00308  -0.1266   0.6193   0.1644
  -1.000   0.5224   0.01029   0.00304  -0.1272   0.6178   0.2208
  -0.750   0.5518   0.01003   0.00303  -0.1279   0.6162   0.3059
  -0.500   0.5812   0.00972   0.00305  -0.1287   0.6146   0.4100
  -0.250   0.6106   0.00943   0.00310  -0.1294   0.6129   0.5215
   0.000   0.6398   0.00928   0.00317  -0.1299   0.6112   0.5971
   0.250   0.6689   0.00921   0.00323  -0.1302   0.6093   0.6487
   0.500   0.6978   0.00917   0.00328  -0.1306   0.6075   0.6844
   0.750   0.7265   0.00913   0.00334  -0.1308   0.6057   0.7220
   1.000   0.7536   0.00907   0.00344  -0.1306   0.6042   0.7804
   1.250   0.7802   0.00906   0.00354  -0.1303   0.6027   0.8267
   1.500   0.8067   0.00910   0.00362  -0.1300   0.6011   0.8529
   1.750   0.8337   0.00913   0.00371  -0.1298   0.5992   0.8709
   2.000   0.8606   0.00916   0.00379  -0.1297   0.5971   0.8858
   2.250   0.8873   0.00920   0.00386  -0.1295   0.5952   0.8996
   2.500   0.9137   0.00924   0.00393  -0.1293   0.5932   0.9137
   2.750   0.9395   0.00927   0.00398  -0.1289   0.5912   0.9286
   3.000   0.9651   0.00929   0.00401  -0.1284   0.5892   0.9448
   3.250   0.9927   0.00932   0.00403  -0.1284   0.5873   0.9636
   3.500   1.0248   0.00937   0.00407  -0.1296   0.5854   0.9909
   3.750   1.0545   0.00946   0.00420  -0.1302   0.5831   0.9998
   4.000   1.0837   0.00956   0.00432  -0.1308   0.5807   0.9998
   4.250   1.1127   0.00966   0.00444  -0.1313   0.5781   0.9998
   4.500   1.1416   0.00975   0.00454  -0.1318   0.5755   0.9998
   4.750   1.1704   0.00984   0.00462  -0.1323   0.5727   0.9998
   5.000   1.1988   0.00995   0.00472  -0.1327   0.5696   0.9998
   5.250   1.2267   0.01004   0.00488  -0.1330   0.5650   0.9998
   5.500   1.2544   0.01013   0.00497  -0.1332   0.5595   0.9998
   5.750   1.2817   0.01023   0.00506  -0.1334   0.5538   0.9998
   6.000   1.3085   0.01034   0.00520  -0.1335   0.5458   0.9998
   6.250   1.3346   0.01047   0.00532  -0.1335   0.5376   0.9998
   6.500   1.3602   0.01063   0.00549  -0.1334   0.5280   0.9998
   6.750   1.3857   0.01082   0.00569  -0.1333   0.5192   0.9998
   7.000   1.4098   0.01105   0.00589  -0.1330   0.5098   0.9998
   7.250   1.4340   0.01129   0.00615  -0.1327   0.4988   0.9998
   7.500   1.4567   0.01158   0.00644  -0.1322   0.4870   0.9998
   7.750   1.4773   0.01196   0.00678  -0.1313   0.4729   0.9998
   8.000   1.4952   0.01243   0.00721  -0.1300   0.4556   0.9998
   8.250   1.5067   0.01311   0.00781  -0.1277   0.4340   0.9998
   8.500   1.5111   0.01402   0.00862  -0.1243   0.4087   0.9998
   8.750   1.5095   0.01545   0.00992  -0.1207   0.3798   0.9998
   9.000   1.5039   0.01741   0.01175  -0.1171   0.3497   0.9998
   9.250   1.4971   0.01977   0.01398  -0.1141   0.3214   0.9998
   9.500   1.4907   0.02232   0.01642  -0.1114   0.2951   0.9998
   9.750   1.4855   0.02489   0.01889  -0.1090   0.2712   0.9998
  10.000   1.4806   0.02743   0.02135  -0.1067   0.2497   0.9998
  10.250   1.4773   0.02988   0.02372  -0.1046   0.2306   0.9998
  10.500   1.4748   0.03224   0.02602  -0.1025   0.2125   0.9998
  10.750   1.4730   0.03458   0.02829  -0.1006   0.1956   0.9998
  11.000   1.4720   0.03687   0.03053  -0.0988   0.1805   0.9998
  11.250   1.4726   0.03910   0.03271  -0.0972   0.1664   0.9998
  11.500   1.4741   0.04130   0.03487  -0.0957   0.1535   0.9998
  11.750   1.4762   0.04349   0.03701  -0.0943   0.1420   0.9998
  12.000   1.4789   0.04566   0.03915  -0.0930   0.1311   0.9998
  12.250   1.4837   0.04767   0.04115  -0.0919   0.1217   0.9998
  12.500   1.4880   0.04976   0.04323  -0.0908   0.1134   0.9998
  12.750   1.4919   0.05188   0.04533  -0.0898   0.1053   0.9998
  13.000   1.4978   0.05387   0.04734  -0.0889   0.0989   0.9998
  13.250   1.5022   0.05602   0.04947  -0.0879   0.0927   0.9998
  13.500   1.5087   0.05798   0.05146  -0.0871   0.0872   0.9998
  13.750   1.5124   0.06025   0.05372  -0.0862   0.0818   0.9998
  14.000   1.5194   0.06217   0.05568  -0.0855   0.0772   0.9998
  14.250   1.5233   0.06446   0.05798  -0.0848   0.0726   0.9998
  14.500   1.5291   0.06656   0.06011  -0.0841   0.0687   0.9998
  14.750   1.5342   0.06875   0.06232  -0.0834   0.0645   0.9998
  15.000   1.5379   0.07113   0.06473  -0.0828   0.0610   0.9998
  15.250   1.5434   0.07329   0.06693  -0.0823   0.0575   0.9998
  15.500   1.5463   0.07577   0.06943  -0.0817   0.0542   0.9998
  15.750   1.5511   0.07808   0.07178  -0.0812   0.0515   0.9998
  16.000   1.5554   0.08044   0.07418  -0.0808   0.0487   0.9998
  16.250   1.5572   0.08312   0.07689  -0.0804   0.0462   0.9998
  16.500   1.5621   0.08546   0.07929  -0.0800   0.0439   0.9998
  16.750   1.5647   0.08806   0.08194  -0.0797   0.0417   0.9998
  17.000   1.5661   0.09084   0.08475  -0.0794   0.0397   0.9998
  17.250   1.5699   0.09333   0.08731  -0.0793   0.0381   0.9998
  17.500   1.5718   0.09610   0.09014  -0.0791   0.0363   0.9998
  17.750   1.5734   0.09891   0.09300  -0.0791   0.0348   0.9998
  18.000   1.5742   0.10186   0.09601  -0.0791   0.0334   0.9998
  18.250   1.5769   0.10456   0.09878  -0.0791   0.0322   0.9998
  18.500   1.5776   0.10753   0.10182  -0.0793   0.0309   0.9998
  18.750   1.5777   0.11060   0.10495  -0.0795   0.0297   0.9998
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