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MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: MH 150 23.89% (mh150-il)
Reynolds number: 100,000
Max Cl/Cd: 38.49 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh150-il-100000-n5.txt
Download as CSV file: xf-mh150-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 150  23.89%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.4223   0.11724   0.11157  -0.0716   1.0001   0.0571
 -16.500  -0.4111   0.11582   0.11026  -0.0726   1.0001   0.0591
 -16.250  -0.4422   0.10710   0.10136  -0.0770   1.0001   0.0623
 -16.000  -0.4276   0.10541   0.09976  -0.0792   0.9886   0.0650
 -15.750  -0.4410   0.09815   0.09231  -0.0846   0.9797   0.0688
 -15.500  -0.4243   0.09595   0.09020  -0.0875   0.9684   0.0722
 -15.250  -0.4284   0.09058   0.08471  -0.0916   0.9582   0.0764
 -15.000  -0.4227   0.08722   0.08134  -0.0944   0.9462   0.0806
 -14.750  -0.4228   0.08338   0.07747  -0.0969   0.9340   0.0849
 -14.500  -0.4258   0.07929   0.07329  -0.0994   0.9230   0.0897
 -14.250  -0.4232   0.07647   0.07047  -0.1008   0.9109   0.0941
 -14.000  -0.4321   0.07200   0.06584  -0.1031   0.9005   0.0993
 -13.750  -0.4270   0.06986   0.06375  -0.1039   0.8895   0.1040
 -13.500  -0.4336   0.06597   0.05974  -0.1058   0.8800   0.1095
 -13.250  -0.4311   0.06352   0.05730  -0.1068   0.8697   0.1147
 -13.000  -0.4352   0.06021   0.05387  -0.1082   0.8612   0.1203
 -12.750  -0.4347   0.05745   0.05109  -0.1097   0.8512   0.1262
 -12.500  -0.4358   0.05465   0.04822  -0.1108   0.8430   0.1320
 -12.250  -0.4372   0.05174   0.04524  -0.1125   0.8342   0.1384
 -12.000  -0.4354   0.04938   0.04286  -0.1137   0.8254   0.1445
 -11.750  -0.4390   0.04645   0.03980  -0.1150   0.8182   0.1512
 -11.500  -0.4337   0.04452   0.03789  -0.1162   0.8090   0.1578
 -11.250  -0.4368   0.04162   0.03486  -0.1179   0.8010   0.1652
 -11.000  -0.4287   0.04012   0.03337  -0.1185   0.7941   0.1721
 -10.750  -0.4307   0.03741   0.03053  -0.1205   0.7850   0.1800
 -10.500  -0.4187   0.03637   0.02952  -0.1207   0.7779   0.1871
 -10.250  -0.4196   0.03415   0.02714  -0.1220   0.7707   0.1951
 -10.000  -0.4086   0.03349   0.02653  -0.1219   0.7625   0.2019
  -9.750  -0.4028   0.03170   0.02455  -0.1235   0.7556   0.2106
  -9.500  -0.3837   0.03115   0.02400  -0.1241   0.7495   0.2180
  -9.250  -0.3694   0.02986   0.02255  -0.1263   0.7413   0.2271
  -9.000  -0.3460   0.02945   0.02212  -0.1270   0.7350   0.2346
  -8.750  -0.3225   0.02839   0.02081  -0.1293   0.7299   0.2440
  -8.500  -0.2992   0.02828   0.02074  -0.1296   0.7220   0.2509
  -8.250  -0.2745   0.02741   0.01963  -0.1318   0.7154   0.2605
  -8.000  -0.2466   0.02736   0.01956  -0.1317   0.7103   0.2667
  -7.750  -0.2202   0.02687   0.01890  -0.1332   0.7040   0.2753
  -7.250  -0.1659   0.02646   0.01837  -0.1341   0.6914   0.2886
  -7.000  -0.1343   0.02579   0.01740  -0.1363   0.6869   0.2974
  -6.750  -0.1099   0.02589   0.01759  -0.1357   0.6797   0.3023
  -6.500  -0.0820   0.02573   0.01735  -0.1362   0.6733   0.3088
  -6.250  -0.0496   0.02516   0.01651  -0.1383   0.6682   0.3169
  -6.000  -0.0224   0.02517   0.01653  -0.1379   0.6632   0.3216
  -5.750   0.0042   0.02512   0.01648  -0.1382   0.6564   0.3274
  -5.500   0.0359   0.02473   0.01588  -0.1399   0.6506   0.3349
  -5.250   0.0655   0.02456   0.01563  -0.1402   0.6459   0.3400
  -5.000   0.0927   0.02456   0.01563  -0.1402   0.6402   0.3452
  -4.750   0.1215   0.02443   0.01541  -0.1410   0.6338   0.3515
  -4.500   0.1537   0.02414   0.01495  -0.1425   0.6286   0.3581
  -4.250   0.1827   0.02407   0.01485  -0.1424   0.6243   0.3627
  -4.000   0.2099   0.02408   0.01485  -0.1427   0.6183   0.3683
  -3.750   0.2403   0.02394   0.01460  -0.1439   0.6121   0.3749
  -3.500   0.2708   0.02379   0.01436  -0.1446   0.6071   0.3803
  -3.250   0.3006   0.02373   0.01425  -0.1448   0.6031   0.3851
  -3.000   0.3279   0.02378   0.01429  -0.1452   0.5972   0.3906
  -2.750   0.3587   0.02369   0.01409  -0.1464   0.5913   0.3972
  -2.500   0.3882   0.02363   0.01398  -0.1468   0.5864   0.4023
  -2.250   0.4184   0.02359   0.01388  -0.1472   0.5825   0.4074
  -2.000   0.4459   0.02368   0.01398  -0.1476   0.5770   0.4132
  -1.750   0.4766   0.02368   0.01388  -0.1488   0.5714   0.4201
  -1.500   0.5044   0.02372   0.01392  -0.1488   0.5666   0.4250
  -1.250   0.5347   0.02371   0.01385  -0.1492   0.5627   0.4310
  -1.000   0.5634   0.02382   0.01393  -0.1499   0.5577   0.4379
  -0.750   0.5915   0.02396   0.01406  -0.1505   0.5523   0.4443
  -0.500   0.6183   0.02410   0.01422  -0.1504   0.5478   0.4497
  -0.250   0.6488   0.02414   0.01420  -0.1510   0.5438   0.4570
   0.000   0.6817   0.02417   0.01411  -0.1523   0.5399   0.4655
   0.250   0.7034   0.02452   0.01459  -0.1516   0.5343   0.4708
   0.500   0.7299   0.02473   0.01482  -0.1517   0.5295   0.4777
   0.750   0.7617   0.02482   0.01481  -0.1528   0.5256   0.4866
   1.000   0.7904   0.02493   0.01491  -0.1529   0.5223   0.4931
   1.250   0.8156   0.02525   0.01528  -0.1528   0.5180   0.5008
   1.500   0.8417   0.02561   0.01564  -0.1533   0.5128   0.5102
   1.750   0.8653   0.02588   0.01598  -0.1527   0.5085   0.5162
   2.000   0.8936   0.02604   0.01611  -0.1529   0.5048   0.5242
   2.250   0.9269   0.02614   0.01609  -0.1541   0.5017   0.5342
   2.500   0.9455   0.02669   0.01678  -0.1530   0.4974   0.5405
   2.750   0.9665   0.02720   0.01737  -0.1524   0.4929   0.5490
   3.000   0.9930   0.02753   0.01769  -0.1528   0.4888   0.5582
   3.250   1.0181   0.02777   0.01795  -0.1523   0.4854   0.5652
   3.500   1.0491   0.02792   0.01802  -0.1530   0.4824   0.5748
   3.750   1.0681   0.02854   0.01873  -0.1523   0.4782   0.5830
   4.000   1.0825   0.02926   0.01958  -0.1508   0.4738   0.5898
   4.250   1.1048   0.02978   0.02013  -0.1505   0.4701   0.5993
   4.500   1.1293   0.03013   0.02049  -0.1503   0.4669   0.6074
   4.750   1.1561   0.03035   0.02069  -0.1501   0.4641   0.6154
   5.000   1.1837   0.03075   0.02105  -0.1507   0.4610   0.6258
   5.250   1.1814   0.03198   0.02250  -0.1472   0.4562   0.6314
   5.500   1.1917   0.03291   0.02353  -0.1454   0.4521   0.6387
   5.750   1.2148   0.03349   0.02410  -0.1455   0.4488   0.6487
   6.000   1.2382   0.03383   0.02447  -0.1449   0.4461   0.6557
   6.250   1.2678   0.03396   0.02456  -0.1451   0.4439   0.6643
   6.500   1.2704   0.03567   0.02640  -0.1435   0.4396   0.6733
   6.750   1.2578   0.03802   0.02897  -0.1400   0.4345   0.6781
   7.000   1.2676   0.03921   0.03024  -0.1387   0.4307   0.6853
   7.250   1.2945   0.03961   0.03061  -0.1391   0.4280   0.6957
   7.500   1.3200   0.03970   0.03070  -0.1385   0.4259   0.7021
   7.750   1.3540   0.03953   0.03048  -0.1390   0.4241   0.7110
   8.000   1.2512   0.04952   0.04101  -0.1323   0.4128   0.7122
   8.250   1.2713   0.05017   0.04169  -0.1319   0.4100   0.7204
   8.500   1.2996   0.04990   0.04140  -0.1315   0.4082   0.7281
   8.750   1.3367   0.04930   0.04076  -0.1322   0.4068   0.7383
   9.000   1.3703   0.04864   0.04007  -0.1319   0.4055   0.7456
   9.250   1.1933   0.06963   0.06163  -0.1274   0.3853   0.7406
   9.500   1.2399   0.06677   0.05875  -0.1268   0.3862   0.7499
   9.750   1.2938   0.06374   0.05564  -0.1271   0.3871   0.7610
  12.250   1.0574   0.12965   0.12267  -0.1309   0.3046   0.8003
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