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FX 76-MP-120 (fx76mp120-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX 76-MP-120 (fx76mp120-il)
Reynolds number: 1,000,000
Max Cl/Cd: 173.96 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx76mp120-il-1000000-n5.txt
Download as CSV file: xf-fx76mp120-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 76-MP-120                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000   0.0981   0.09239   0.08932  -0.1433   0.7752   0.0067
 -10.750   0.1113   0.09053   0.08745  -0.1449   0.7734   0.0070
 -10.250  -0.1743   0.02118   0.01738  -0.2018   0.7630   0.0086
 -10.000  -0.1533   0.01911   0.01508  -0.2033   0.7609   0.0087
  -9.750  -0.1297   0.01778   0.01356  -0.2042   0.7592   0.0089
  -9.500  -0.1050   0.01668   0.01229  -0.2049   0.7574   0.0090
  -9.250  -0.0802   0.01549   0.01093  -0.2057   0.7555   0.0094
  -9.000  -0.0539   0.01472   0.01005  -0.2062   0.7539   0.0098
  -8.750  -0.0271   0.01414   0.00940  -0.2066   0.7522   0.0101
  -8.500   0.0000   0.01358   0.00875  -0.2070   0.7505   0.0104
  -8.250   0.0273   0.01307   0.00814  -0.2073   0.7487   0.0107
  -8.000   0.0546   0.01258   0.00755  -0.2077   0.7468   0.0111
  -7.750   0.0822   0.01215   0.00702  -0.2079   0.7449   0.0114
  -7.500   0.1097   0.01176   0.00653  -0.2082   0.7431   0.0117
  -7.250   0.1374   0.01137   0.00604  -0.2085   0.7413   0.0120
  -7.000   0.1653   0.01094   0.00554  -0.2088   0.7396   0.0126
  -6.750   0.1934   0.01061   0.00517  -0.2090   0.7379   0.0131
  -6.500   0.2215   0.01034   0.00485  -0.2093   0.7360   0.0137
  -6.250   0.2496   0.01009   0.00455  -0.2095   0.7340   0.0143
  -6.000   0.2777   0.00986   0.00427  -0.2097   0.7319   0.0149
  -5.750   0.3057   0.00960   0.00397  -0.2099   0.7299   0.0159
  -5.500   0.3337   0.00940   0.00372  -0.2100   0.7279   0.0170
  -5.250   0.3618   0.00924   0.00351  -0.2102   0.7259   0.0181
  -5.000   0.3901   0.00907   0.00331  -0.2103   0.7240   0.0190
  -4.750   0.4183   0.00887   0.00311  -0.2105   0.7220   0.0207
  -4.500   0.4465   0.00873   0.00296  -0.2107   0.7197   0.0225
  -4.250   0.4747   0.00860   0.00280  -0.2108   0.7174   0.0242
  -4.000   0.5027   0.00847   0.00266  -0.2109   0.7151   0.0263
  -3.750   0.5305   0.00838   0.00253  -0.2110   0.7127   0.0283
  -3.500   0.5585   0.00828   0.00240  -0.2111   0.7103   0.0302
  -3.250   0.5866   0.00817   0.00231  -0.2112   0.7078   0.0329
  -3.000   0.6146   0.00809   0.00222  -0.2113   0.7048   0.0354
  -2.750   0.6425   0.00800   0.00213  -0.2114   0.7019   0.0384
  -2.500   0.6701   0.00793   0.00206  -0.2114   0.6990   0.0419
  -2.000   0.7257   0.00782   0.00193  -0.2115   0.6937   0.0495
  -1.750   0.7535   0.00776   0.00188  -0.2116   0.6906   0.0532
  -1.500   0.7810   0.00772   0.00183  -0.2116   0.6871   0.0583
  -1.250   0.8082   0.00768   0.00180  -0.2115   0.6835   0.0644
  -1.000   0.8355   0.00766   0.00177  -0.2115   0.6800   0.0704
  -0.750   0.8630   0.00762   0.00176  -0.2115   0.6762   0.0786
  -0.500   0.8901   0.00760   0.00175  -0.2114   0.6720   0.0874
   0.000   0.9438   0.00758   0.00175  -0.2112   0.6639   0.1094
   0.250   0.9708   0.00756   0.00177  -0.2111   0.6592   0.1251
   0.500   0.9970   0.00755   0.00180  -0.2109   0.6544   0.1487
   1.000   1.0498   0.00751   0.00188  -0.2106   0.6443   0.2092
   1.250   1.0751   0.00750   0.00194  -0.2102   0.6385   0.2581
   1.500   1.1009   0.00746   0.00202  -0.2100   0.6324   0.3173
   1.750   1.1253   0.00737   0.00213  -0.2095   0.6250   0.4257
   2.000   1.1492   0.00719   0.00227  -0.2089   0.6180   0.5907
   2.250   1.1717   0.00713   0.00243  -0.2080   0.6099   0.7106
   2.500   1.1950   0.00717   0.00256  -0.2071   0.6022   0.7676
   3.000   1.2365   0.00729   0.00282  -0.2043   0.5829   0.8679
   3.250   1.2664   0.00728   0.00293  -0.2049   0.5726   1.0000
   3.500   1.2884   0.00749   0.00307  -0.2039   0.5616   1.0000
   3.750   1.3103   0.00769   0.00322  -0.2028   0.5503   1.0000
   4.000   1.3317   0.00790   0.00338  -0.2017   0.5385   1.0000
   4.250   1.3514   0.00815   0.00357  -0.2002   0.5260   1.0000
   4.500   1.3681   0.00842   0.00378  -0.1981   0.5119   1.0000
   4.750   1.3843   0.00872   0.00401  -0.1959   0.4978   1.0000
   5.000   1.4012   0.00902   0.00425  -0.1939   0.4852   1.0000
   5.500   1.4349   0.00965   0.00479  -0.1900   0.4607   1.0000
   5.750   1.4516   0.00999   0.00509  -0.1881   0.4491   1.0000
   6.000   1.4673   0.01038   0.00543  -0.1861   0.4370   1.0000
   6.250   1.4814   0.01083   0.00583  -0.1838   0.4229   1.0000
   6.500   1.4957   0.01131   0.00626  -0.1816   0.4097   1.0000
   6.750   1.5109   0.01179   0.00670  -0.1797   0.3980   1.0000
   7.000   1.5263   0.01230   0.00718  -0.1779   0.3861   1.0000
   7.250   1.5414   0.01286   0.00772  -0.1761   0.3752   1.0000
   7.500   1.5559   0.01350   0.00832  -0.1743   0.3639   1.0000
   7.750   1.5706   0.01417   0.00896  -0.1726   0.3520   1.0000
   8.000   1.5848   0.01493   0.00968  -0.1710   0.3386   1.0000
   8.250   1.6001   0.01567   0.01041  -0.1696   0.3274   1.0000
   8.500   1.6137   0.01655   0.01125  -0.1680   0.3141   1.0000
   8.750   1.6279   0.01743   0.01210  -0.1666   0.3033   1.0000
   9.000   1.6409   0.01841   0.01304  -0.1651   0.2907   1.0000
   9.250   1.6518   0.01954   0.01410  -0.1634   0.2747   1.0000
   9.500   1.6576   0.02100   0.01545  -0.1610   0.2511   1.0000
   9.750   1.6603   0.02268   0.01699  -0.1584   0.2255   1.0000
  10.000   1.6625   0.02438   0.01856  -0.1557   0.2028   1.0000
  10.250   1.6673   0.02592   0.02002  -0.1534   0.1834   1.0000
  10.500   1.6663   0.02788   0.02182  -0.1505   0.1583   1.0000
  10.750   1.6685   0.02964   0.02349  -0.1480   0.1388   1.0000
  11.000   1.6704   0.03148   0.02523  -0.1455   0.1214   1.0000
  11.250   1.6768   0.03301   0.02672  -0.1436   0.1097   1.0000
  11.500   1.6785   0.03491   0.02856  -0.1413   0.0944   1.0000
  11.750   1.6822   0.03670   0.03029  -0.1393   0.0818   1.0000
  12.000   1.6799   0.03902   0.03252  -0.1367   0.0638   1.0000
  12.250   1.6819   0.04101   0.03447  -0.1347   0.0530   1.0000
  12.500   1.6824   0.04316   0.03657  -0.1325   0.0421   1.0000
  12.750   1.6830   0.04537   0.03876  -0.1305   0.0329   1.0000
  13.000   1.6866   0.04736   0.04074  -0.1288   0.0268   1.0000
  13.250   1.6882   0.04955   0.04294  -0.1271   0.0210   1.0000
  13.500   1.6914   0.05161   0.04501  -0.1255   0.0170   1.0000
  13.750   1.6952   0.05369   0.04712  -0.1241   0.0145   1.0000
  14.250   1.7020   0.05798   0.05148  -0.1213   0.0102   1.0000
  14.500   1.7049   0.06023   0.05377  -0.1201   0.0089   1.0000
  14.750   1.7084   0.06243   0.05603  -0.1189   0.0077   1.0000
  15.000   1.7098   0.06490   0.05854  -0.1177   0.0067   1.0000
  15.250   1.7133   0.06717   0.06087  -0.1167   0.0061   1.0000
  15.500   1.7144   0.06978   0.06354  -0.1157   0.0053   1.0000
  15.750   1.7159   0.07237   0.06619  -0.1147   0.0049   1.0000
  16.000   1.7180   0.07496   0.06885  -0.1140   0.0046   1.0000
  16.250   1.7191   0.07767   0.07164  -0.1132   0.0043   1.0000
  16.500   1.7199   0.08047   0.07450  -0.1126   0.0040   1.0000
  16.750   1.7193   0.08354   0.07765  -0.1121   0.0038   1.0000
  17.000   1.7186   0.08666   0.08085  -0.1116   0.0035   1.0000
  17.250   1.7172   0.08994   0.08420  -0.1113   0.0033   1.0000
  17.500   1.7170   0.09313   0.08747  -0.1112   0.0033   1.0000
  17.750   1.7162   0.09643   0.09085  -0.1112   0.0031   1.0000
  18.000   1.7150   0.09983   0.09434  -0.1112   0.0030   1.0000
  18.250   1.7135   0.10334   0.09794  -0.1115   0.0029   1.0000
  18.500   1.7111   0.10706   0.10174  -0.1119   0.0028   1.0000
  18.750   1.7087   0.11080   0.10557  -0.1124   0.0027   1.0000
  19.000   1.7066   0.11453   0.10939  -0.1130   0.0027   1.0000
  19.250   1.7032   0.11850   0.11345  -0.1138   0.0026   1.0000
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