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AH 94-145 (ah94145-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: AH 94-145 (ah94145-il)
Reynolds number: 200,000
Max Cl/Cd: 75.69 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah94145-il-200000.txt
Download as CSV file: xf-ah94145-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 94-145                                       
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.1599   0.10559   0.10134  -0.0694   0.7882   0.0519
  -9.750  -0.1716   0.10162   0.09743  -0.0778   0.7853   0.0534
  -9.500  -0.1695   0.09704   0.09286  -0.0805   0.7827   0.0538
  -9.250  -0.1517   0.09441   0.09019  -0.0776   0.7804   0.0547
  -9.000  -0.1383   0.09217   0.08792  -0.0770   0.7782   0.0560
  -8.750  -0.1292   0.08955   0.08528  -0.0782   0.7761   0.0579
  -8.500  -0.1238   0.08618   0.08195  -0.0816   0.7736   0.0605
  -8.250  -0.1397   0.07969   0.07556  -0.0980   0.7702   0.0628
  -8.000  -0.1359   0.07395   0.06982  -0.1025   0.7676   0.0636
  -7.750  -0.1211   0.07280   0.06868  -0.0972   0.7653   0.0644
  -7.500  -0.1085   0.07052   0.06637  -0.0973   0.7630   0.0656
  -7.250  -0.0974   0.06728   0.06309  -0.1007   0.7610   0.0672
  -7.000  -0.0860   0.06296   0.05872  -0.1069   0.7588   0.0699
  -6.750  -0.0814   0.05390   0.04920  -0.1211   0.7560   0.0750
  -6.500  -0.0635   0.05141   0.04679  -0.1211   0.7533   0.0762
  -6.250  -0.0525   0.03849   0.03282  -0.1271   0.7509   0.0527
  -6.000  -0.0314   0.03493   0.02896  -0.1282   0.7485   0.0520
  -5.750  -0.0083   0.03131   0.02489  -0.1291   0.7465   0.0506
  -5.500   0.0171   0.02813   0.02117  -0.1298   0.7447   0.0501
  -5.250   0.0441   0.02610   0.01868  -0.1302   0.7429   0.0511
  -5.000   0.0722   0.02514   0.01731  -0.1306   0.7402   0.0535
  -4.750   0.0984   0.02386   0.01604  -0.1311   0.7373   0.0564
  -4.500   0.1262   0.02313   0.01519  -0.1313   0.7346   0.0594
  -4.250   0.1547   0.02249   0.01429  -0.1315   0.7324   0.0633
  -4.000   0.1821   0.02178   0.01363  -0.1318   0.7304   0.0685
  -3.750   0.2108   0.02146   0.01312  -0.1319   0.7287   0.0740
  -3.500   0.2383   0.02084   0.01254  -0.1321   0.7271   0.0820
  -3.250   0.2648   0.02050   0.01224  -0.1324   0.7241   0.0903
  -3.000   0.2918   0.02045   0.01220  -0.1327   0.7209   0.1004
  -2.750   0.3190   0.02012   0.01195  -0.1330   0.7183   0.1123
  -2.500   0.3471   0.01986   0.01174  -0.1334   0.7161   0.1259
  -2.250   0.3757   0.01961   0.01152  -0.1338   0.7142   0.1424
  -2.000   0.4048   0.01936   0.01131  -0.1343   0.7123   0.1661
  -1.750   0.4346   0.01887   0.01116  -0.1351   0.7107   0.2359
  -1.500   0.4587   0.01796   0.01178  -0.1358   0.7074   0.6277
  -1.250   0.4739   0.01818   0.01247  -0.1331   0.7041   0.7660
  -1.000   0.4884   0.01850   0.01291  -0.1299   0.7013   0.8389
  -0.750   0.5041   0.01870   0.01311  -0.1269   0.6989   0.8855
  -0.500   0.5188   0.01873   0.01309  -0.1234   0.6970   0.9226
  -0.250   0.5377   0.01868   0.01296  -0.1208   0.6953   0.9595
   0.000   0.5815   0.01867   0.01283  -0.1239   0.6939   0.9990
   0.250   0.5978   0.01988   0.01409  -0.1238   0.6884   0.9998
   0.500   0.6236   0.02039   0.01455  -0.1244   0.6849   0.9998
   0.750   0.6531   0.02061   0.01468  -0.1251   0.6826   0.9998
   1.000   0.6838   0.02075   0.01473  -0.1259   0.6808   0.9998
   1.250   0.7149   0.02089   0.01478  -0.1266   0.6794   0.9998
   1.500   0.7460   0.02104   0.01485  -0.1274   0.6780   0.9998
   1.750   0.7578   0.02285   0.01677  -0.1270   0.6704   0.9998
   2.000   0.7839   0.02338   0.01727  -0.1274   0.6674   0.9998
   2.250   0.8138   0.02353   0.01737  -0.1280   0.6654   0.9998
   2.500   0.8454   0.02352   0.01732  -0.1286   0.6639   0.9998
   2.750   0.8776   0.02351   0.01725  -0.1293   0.6627   0.9998
   3.000   0.9088   0.02361   0.01731  -0.1299   0.6615   0.9998
   3.250   0.9073   0.02638   0.02024  -0.1283   0.6509   0.9998
   3.500   0.9379   0.02640   0.02024  -0.1288   0.6491   0.9998
   3.750   0.9705   0.02625   0.02008  -0.1294   0.6478   0.9998
   4.000   1.0043   0.02602   0.01981  -0.1301   0.6467   0.9998
   4.250   1.0373   0.02588   0.01965  -0.1307   0.6456   0.9998
   4.500   1.0281   0.02902   0.02296  -0.1281   0.6337   0.9998
   4.750   1.0624   0.02864   0.02258  -0.1287   0.6324   0.9998
   5.000   1.0983   0.02811   0.02205  -0.1295   0.6314   0.9998
   5.250   1.0880   0.03121   0.02527  -0.1266   0.6198   0.9998
   5.500   1.1234   0.03061   0.02469  -0.1272   0.6183   0.9998
   5.750   1.1615   0.02976   0.02387  -0.1280   0.6173   0.9998
   6.000   1.2025   0.02866   0.02277  -0.1291   0.6164   0.9998
   6.250   1.2450   0.02736   0.02148  -0.1304   0.6152   0.9998
   6.500   1.2883   0.02596   0.02006  -0.1317   0.6135   0.9998
   6.750   1.2908   0.02736   0.02161  -0.1291   0.6032   0.9998
   7.000   1.3400   0.02527   0.01952  -0.1308   0.6012   0.9998
   7.250   1.3886   0.02336   0.01755  -0.1328   0.5989   0.9998
   7.500   1.3962   0.02423   0.01860  -0.1303   0.5894   0.9998
   7.750   1.4384   0.02279   0.01715  -0.1317   0.5857   0.9998
   8.000   1.4599   0.02274   0.01721  -0.1307   0.5787   0.9998
   8.250   1.4892   0.02213   0.01667  -0.1307   0.5723   0.9998
   8.500   1.5180   0.02155   0.01615  -0.1305   0.5654   0.9998
   8.750   1.5417   0.02114   0.01582  -0.1296   0.5563   0.9998
   9.000   1.5574   0.02120   0.01600  -0.1278   0.5456   0.9998
   9.250   1.5773   0.02100   0.01586  -0.1264   0.5343   0.9998
   9.500   1.5917   0.02103   0.01594  -0.1242   0.5213   0.9998
   9.750   1.5992   0.02150   0.01647  -0.1214   0.5059   0.9998
  10.000   1.6034   0.02235   0.01738  -0.1185   0.4876   0.9998
  10.250   1.6091   0.02325   0.01823  -0.1159   0.4648   0.9998
  10.500   1.6079   0.02481   0.01971  -0.1131   0.4360   0.9998
  10.750   1.6021   0.02686   0.02158  -0.1100   0.4016   0.9998
  11.000   1.5900   0.02958   0.02409  -0.1067   0.3652   0.9998
  11.250   1.5741   0.03278   0.02707  -0.1034   0.3313   0.9998
  11.500   1.5575   0.03618   0.03027  -0.1003   0.3002   0.9998
  11.750   1.5418   0.03962   0.03355  -0.0975   0.2714   0.9998
  12.000   1.5278   0.04308   0.03686  -0.0951   0.2450   0.9998
  12.250   1.5149   0.04661   0.04024  -0.0929   0.2214   0.9998
  12.500   1.5059   0.04991   0.04343  -0.0911   0.1990   0.9998
  12.750   1.4973   0.05327   0.04667  -0.0895   0.1800   0.9998
  13.000   1.4903   0.05656   0.04986  -0.0880   0.1637   0.9998
  13.250   1.4854   0.05969   0.05290  -0.0867   0.1493   0.9998
  13.500   1.4824   0.06269   0.05586  -0.0856   0.1365   0.9998
  13.750   1.4813   0.06554   0.05869  -0.0846   0.1252   0.9998
  14.000   1.4807   0.06834   0.06150  -0.0836   0.1155   0.9998
  14.250   1.4783   0.07135   0.06444  -0.0826   0.1076   0.9998
  14.500   1.4798   0.07402   0.06715  -0.0819   0.0998   0.9998
  14.750   1.4803   0.07674   0.06986  -0.0811   0.0934   0.9998
  15.000   1.4818   0.07945   0.07261  -0.0805   0.0874   0.9998
  15.250   1.4831   0.08204   0.07519  -0.0797   0.0822   0.9998
  15.500   1.4862   0.08463   0.07786  -0.0792   0.0774   0.9998
  15.750   1.4878   0.08703   0.08016  -0.0783   0.0730   0.9998
  16.000   1.4919   0.08960   0.08291  -0.0780   0.0693   0.9998
  16.250   1.4949   0.09221   0.08556  -0.0777   0.0658   0.9998
  16.500   1.4998   0.09411   0.08738  -0.0767   0.0624   0.9998
  16.750   1.5031   0.09682   0.09027  -0.0766   0.0597   0.9998
  17.000   1.5066   0.09937   0.09289  -0.0765   0.0569   0.9998
  17.250   1.5117   0.10144   0.09491  -0.0760   0.0544   0.9998
  17.500   1.5168   0.10361   0.09721  -0.0755   0.0521   0.9998
  17.750   1.5193   0.10642   0.10016  -0.0756   0.0499   0.9998
  18.000   1.5226   0.10903   0.10283  -0.0757   0.0479   0.9998
  18.250   1.5305   0.11053   0.10426  -0.0751   0.0458   0.9998
  18.500   1.5329   0.11323   0.10712  -0.0751   0.0442   0.9998
  18.750   1.5329   0.11651   0.11059  -0.0757   0.0426   0.9998
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