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MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 102 16.99% (mh102-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.16 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh102-il-1000000-n5.txt
Download as CSV file: xf-mh102-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 102  16.99%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.8826   0.08818   0.08455  -0.0474   1.0000   0.0054
 -17.000  -0.8958   0.08278   0.07908  -0.0501   1.0000   0.0054
 -16.750  -0.9153   0.07655   0.07274  -0.0533   1.0000   0.0054
 -16.500  -0.9353   0.07052   0.06662  -0.0564   1.0000   0.0054
 -16.250  -0.9637   0.06355   0.05953  -0.0600   1.0000   0.0054
 -16.000  -0.9869   0.05740   0.05327  -0.0631   1.0000   0.0054
 -15.750  -1.0091   0.05140   0.04715  -0.0662   1.0000   0.0053
 -15.500  -1.0295   0.04556   0.04119  -0.0693   1.0000   0.0054
 -15.250  -1.0451   0.04024   0.03575  -0.0722   1.0000   0.0053
 -15.000  -1.0561   0.03551   0.03089  -0.0751   1.0000   0.0054
 -14.750  -1.0629   0.03158   0.02684  -0.0773   1.0000   0.0055
 -14.500  -1.0660   0.02861   0.02378  -0.0785   1.0000   0.0055
 -14.250  -1.0677   0.02634   0.02142  -0.0786   1.0000   0.0056
 -14.000  -1.0692   0.02462   0.01962  -0.0775   1.0000   0.0056
 -13.750  -1.0725   0.02326   0.01818  -0.0751   1.0000   0.0057
 -13.500  -1.0764   0.02234   0.01721  -0.0715   1.0000   0.0057
 -13.250  -1.0641   0.02148   0.01629  -0.0703   0.9978   0.0058
 -13.000  -1.0426   0.02063   0.01539  -0.0705   0.9902   0.0059
 -12.500  -0.9908   0.01886   0.01352  -0.0723   0.9709   0.0064
 -12.250  -0.9516   0.01801   0.01262  -0.0756   0.9539   0.0067
 -12.000  -0.9077   0.01722   0.01175  -0.0797   0.9242   0.0071
 -11.500  -0.8674   0.01641   0.01063  -0.0776   0.8571   0.0077
 -11.250  -0.8490   0.01604   0.01013  -0.0761   0.8343   0.0080
 -11.000  -0.8297   0.01565   0.00965  -0.0748   0.8146   0.0083
 -10.750  -0.8096   0.01527   0.00918  -0.0736   0.7969   0.0091
 -10.500  -0.7881   0.01493   0.00876  -0.0726   0.7808   0.0096
 -10.250  -0.7665   0.01457   0.00832  -0.0716   0.7659   0.0105
 -10.000  -0.7441   0.01424   0.00793  -0.0707   0.7516   0.0114
  -9.750  -0.7212   0.01391   0.00753  -0.0699   0.7376   0.0126
  -9.500  -0.6978   0.01359   0.00716  -0.0692   0.7253   0.0143
  -9.250  -0.6743   0.01326   0.00679  -0.0684   0.7137   0.0165
  -9.000  -0.6502   0.01295   0.00643  -0.0678   0.7023   0.0191
  -8.750  -0.6260   0.01263   0.00608  -0.0672   0.6911   0.0227
  -8.500  -0.6016   0.01234   0.00576  -0.0665   0.6793   0.0265
  -8.250  -0.5767   0.01203   0.00543  -0.0660   0.6688   0.0313
  -8.000  -0.5521   0.01173   0.00511  -0.0654   0.6590   0.0376
  -7.750  -0.5271   0.01140   0.00479  -0.0649   0.6493   0.0460
  -7.500  -0.5025   0.01106   0.00446  -0.0644   0.6390   0.0572
  -7.250  -0.4776   0.01072   0.00414  -0.0638   0.6284   0.0711
  -7.000  -0.4534   0.01030   0.00381  -0.0633   0.6190   0.0916
  -6.750  -0.4285   0.00994   0.00352  -0.0628   0.6097   0.1137
  -6.500  -0.4025   0.00969   0.00332  -0.0624   0.6013   0.1310
  -6.250  -0.3759   0.00950   0.00316  -0.0621   0.5921   0.1448
  -6.000  -0.3491   0.00935   0.00301  -0.0618   0.5829   0.1568
  -5.750  -0.3217   0.00924   0.00289  -0.0616   0.5730   0.1647
  -5.500  -0.2943   0.00915   0.00278  -0.0614   0.5646   0.1728
  -5.250  -0.2668   0.00903   0.00268  -0.0612   0.5563   0.1823
  -5.000  -0.2390   0.00898   0.00259  -0.0610   0.5484   0.1881
  -4.750  -0.2110   0.00891   0.00249  -0.0608   0.5406   0.1928
  -4.250  -0.1553   0.00881   0.00233  -0.0605   0.5238   0.2021
  -4.000  -0.1273   0.00879   0.00226  -0.0604   0.5155   0.2052
  -3.750  -0.0993   0.00873   0.00218  -0.0602   0.5090   0.2103
  -3.500  -0.0713   0.00868   0.00212  -0.0601   0.5019   0.2153
  -3.250  -0.0433   0.00867   0.00207  -0.0600   0.4948   0.2193
  -3.000  -0.0150   0.00864   0.00202  -0.0599   0.4879   0.2233
  -2.750   0.0128   0.00861   0.00197  -0.0597   0.4803   0.2293
  -2.500   0.0409   0.00859   0.00193  -0.0596   0.4744   0.2342
  -2.250   0.0692   0.00858   0.00190  -0.0595   0.4684   0.2382
  -2.000   0.0970   0.00856   0.00186  -0.0594   0.4616   0.2445
  -1.750   0.1252   0.00854   0.00184  -0.0593   0.4559   0.2509
  -1.500   0.1534   0.00854   0.00182  -0.0592   0.4500   0.2558
  -1.250   0.1812   0.00853   0.00181  -0.0591   0.4437   0.2625
  -1.000   0.2094   0.00852   0.00180  -0.0590   0.4384   0.2694
  -0.750   0.2375   0.00852   0.00179  -0.0589   0.4327   0.2768
  -0.500   0.2652   0.00852   0.00180  -0.0587   0.4269   0.2850
  -0.250   0.2934   0.00854   0.00180  -0.0586   0.4220   0.2917
   0.000   0.3214   0.00852   0.00181  -0.0586   0.4172   0.3003
   0.250   0.3493   0.00855   0.00183  -0.0584   0.4116   0.3087
   0.500   0.3768   0.00856   0.00186  -0.0583   0.4065   0.3198
   0.750   0.4050   0.00856   0.00188  -0.0582   0.4023   0.3292
   1.000   0.4329   0.00856   0.00191  -0.0581   0.3976   0.3398
   1.250   0.4605   0.00860   0.00195  -0.0580   0.3926   0.3497
   1.500   0.4881   0.00862   0.00199  -0.0578   0.3883   0.3624
   1.750   0.5160   0.00862   0.00203  -0.0577   0.3843   0.3766
   2.000   0.5436   0.00864   0.00208  -0.0576   0.3794   0.3897
   2.500   0.5983   0.00871   0.00220  -0.0572   0.3705   0.4190
   2.750   0.6259   0.00871   0.00226  -0.0571   0.3663   0.4369
   3.000   0.6530   0.00874   0.00233  -0.0569   0.3613   0.4563
   3.250   0.6797   0.00879   0.00242  -0.0566   0.3559   0.4755
   3.500   0.7070   0.00880   0.00250  -0.0565   0.3518   0.4979
   3.750   0.7338   0.00881   0.00258  -0.0562   0.3466   0.5265
   4.000   0.7600   0.00885   0.00269  -0.0559   0.3408   0.5570
   4.250   0.7863   0.00886   0.00279  -0.0556   0.3361   0.5898
   4.500   0.8125   0.00887   0.00290  -0.0552   0.3302   0.6268
   4.750   0.8377   0.00892   0.00303  -0.0547   0.3237   0.6634
   5.000   0.8633   0.00894   0.00315  -0.0542   0.3186   0.7027
   5.250   0.8880   0.00897   0.00329  -0.0536   0.3115   0.7448
   5.500   0.9119   0.00903   0.00344  -0.0528   0.3048   0.7875
   5.750   0.9351   0.00904   0.00359  -0.0518   0.2978   0.8356
   6.000   0.9566   0.00912   0.00378  -0.0504   0.2900   0.8874
   6.250   0.9847   0.00919   0.00395  -0.0503   0.2831   0.9399
   6.500   1.0300   0.00946   0.00420  -0.0542   0.2730   0.9765
   6.750   1.0685   0.00970   0.00440  -0.0567   0.2638   0.9981
   7.000   1.0927   0.00995   0.00461  -0.0561   0.2560   1.0000
   7.250   1.1150   0.01016   0.00480  -0.0551   0.2487   1.0000
   7.500   1.1364   0.01042   0.00501  -0.0540   0.2415   1.0000
   7.750   1.1587   0.01063   0.00522  -0.0530   0.2346   1.0000
   8.250   1.2016   0.01114   0.00568  -0.0508   0.2215   1.0000
   8.500   1.2217   0.01145   0.00595  -0.0495   0.2139   1.0000
   8.750   1.2426   0.01171   0.00620  -0.0483   0.2080   1.0000
   9.000   1.2626   0.01199   0.00646  -0.0471   0.2019   1.0000
   9.250   1.2808   0.01231   0.00676  -0.0455   0.1953   1.0000
   9.500   1.2979   0.01259   0.00704  -0.0436   0.1895   1.0000
   9.750   1.3121   0.01296   0.00738  -0.0413   0.1833   1.0000
  10.000   1.3286   0.01326   0.00769  -0.0395   0.1786   1.0000
  10.250   1.3436   0.01363   0.00805  -0.0375   0.1729   1.0000
  10.500   1.3576   0.01406   0.00846  -0.0354   0.1672   1.0000
  10.750   1.3732   0.01445   0.00886  -0.0336   0.1622   1.0000
  11.000   1.3856   0.01498   0.00937  -0.0315   0.1561   1.0000
  11.250   1.3998   0.01546   0.00986  -0.0297   0.1516   1.0000
  11.500   1.4130   0.01600   0.01041  -0.0278   0.1467   1.0000
  11.750   1.4238   0.01669   0.01109  -0.0258   0.1416   1.0000
  12.000   1.4372   0.01729   0.01172  -0.0242   0.1378   1.0000
  12.250   1.4482   0.01806   0.01249  -0.0225   0.1329   1.0000
  12.500   1.4575   0.01896   0.01340  -0.0208   0.1282   1.0000
  12.750   1.4692   0.01979   0.01425  -0.0194   0.1245   1.0000
  13.000   1.4781   0.02084   0.01531  -0.0180   0.1200   1.0000
  13.250   1.4866   0.02198   0.01647  -0.0166   0.1162   1.0000
  13.500   1.4957   0.02315   0.01767  -0.0155   0.1119   1.0000
  13.750   1.5027   0.02453   0.01906  -0.0144   0.1080   1.0000
  14.000   1.5090   0.02603   0.02058  -0.0134   0.1041   1.0000
  14.250   1.5160   0.02754   0.02213  -0.0126   0.1004   1.0000
  14.500   1.5188   0.02946   0.02406  -0.0117   0.0962   1.0000
  14.750   1.5235   0.03129   0.02593  -0.0111   0.0927   1.0000
  15.000   1.5262   0.03334   0.02801  -0.0105   0.0890   1.0000
  15.250   1.5256   0.03576   0.03045  -0.0100   0.0853   1.0000
  15.500   1.5291   0.03786   0.03260  -0.0097   0.0829   1.0000
  15.750   1.5282   0.04044   0.03522  -0.0095   0.0793   1.0000
  16.000   1.5258   0.04323   0.03805  -0.0093   0.0765   1.0000
  16.250   1.5260   0.04583   0.04071  -0.0093   0.0741   1.0000
  16.500   1.5248   0.04862   0.04355  -0.0093   0.0718   1.0000
  16.750   1.5189   0.05196   0.04693  -0.0095   0.0687   1.0000
  17.000   1.5157   0.05507   0.05009  -0.0097   0.0665   1.0000
  17.250   1.5112   0.05837   0.05345  -0.0100   0.0637   1.0000
  17.500   1.5049   0.06192   0.05704  -0.0104   0.0614   1.0000
  17.750   1.4990   0.06548   0.06065  -0.0109   0.0591   1.0000
  18.000   1.4931   0.06912   0.06435  -0.0115   0.0569   1.0000
  18.250   1.4831   0.07330   0.06857  -0.0123   0.0543   1.0000
  18.500   1.4778   0.07694   0.07227  -0.0131   0.0530   1.0000
  18.750   1.4726   0.08063   0.07603  -0.0139   0.0508   1.0000
  19.000   1.4650   0.08471   0.08016  -0.0149   0.0492   1.0000
  19.250   1.4549   0.08918   0.08468  -0.0162   0.0472   1.0000
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