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MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: MH 102 16.99% (mh102-il)
Reynolds number: 200,000
Max Cl/Cd: 63.5 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh102-il-200000.txt
Download as CSV file: xf-mh102-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.6527   0.11497   0.11053  -0.0425   1.0000   0.0269
 -16.500  -0.6734   0.10690   0.10235  -0.0471   1.0000   0.0266
 -16.250  -0.7014   0.09778   0.09304  -0.0527   1.0000   0.0265
 -16.000  -0.7226   0.09033   0.08542  -0.0573   1.0000   0.0263
 -15.750  -0.7387   0.08409   0.07903  -0.0611   1.0000   0.0261
 -15.500  -0.7553   0.07805   0.07282  -0.0647   1.0000   0.0261
 -15.250  -0.7660   0.07318   0.06780  -0.0674   1.0000   0.0260
 -15.000  -0.7807   0.06791   0.06235  -0.0704   1.0000   0.0262
 -14.750  -0.7912   0.06338   0.05764  -0.0728   1.0000   0.0264
 -14.500  -0.7944   0.05994   0.05408  -0.0742   1.0000   0.0264
 -14.250  -0.8021   0.05600   0.04996  -0.0760   1.0000   0.0267
 -14.000  -0.8059   0.05268   0.04647  -0.0773   1.0000   0.0269
 -13.750  -0.8000   0.05057   0.04437  -0.0769   1.0000   0.0275
 -13.500  -0.7931   0.04871   0.04255  -0.0765   1.0000   0.0280
 -13.250  -0.7900   0.04644   0.04025  -0.0767   1.0000   0.0286
 -13.000  -0.7873   0.04417   0.03792  -0.0768   1.0000   0.0291
 -12.750  -0.7864   0.04177   0.03545  -0.0769   1.0000   0.0298
 -12.500  -0.7855   0.03948   0.03306  -0.0769   1.0000   0.0305
 -12.250  -0.7855   0.03728   0.03082  -0.0764   1.0000   0.0313
 -12.000  -0.7861   0.03526   0.02886  -0.0758   1.0000   0.0321
 -11.750  -0.7893   0.03328   0.02686  -0.0748   1.0000   0.0330
 -11.500  -0.7948   0.03155   0.02507  -0.0730   1.0000   0.0341
 -11.250  -0.8021   0.03018   0.02361  -0.0700   1.0000   0.0349
 -11.000  -0.8155   0.02910   0.02252  -0.0652   1.0000   0.0354
 -10.750  -0.8286   0.02807   0.02156  -0.0603   1.0000   0.0368
 -10.500  -0.8386   0.02729   0.02078  -0.0554   1.0000   0.0379
 -10.250  -0.8510   0.02670   0.02012  -0.0500   1.0000   0.0396
 -10.000  -0.8286   0.02518   0.01862  -0.0515   0.9943   0.0433
  -9.750  -0.7951   0.02342   0.01682  -0.0547   0.9854   0.0510
  -9.500  -0.7627   0.02161   0.01505  -0.0575   0.9763   0.0637
  -9.250  -0.7301   0.01966   0.01330  -0.0605   0.9679   0.0904
  -9.000  -0.6979   0.01853   0.01238  -0.0625   0.9574   0.1291
  -8.750  -0.6549   0.01815   0.01198  -0.0657   0.9515   0.1568
  -8.500  -0.6169   0.01799   0.01167  -0.0677   0.9416   0.1741
  -8.250  -0.5790   0.01786   0.01148  -0.0697   0.9325   0.1880
  -8.000  -0.5415   0.01773   0.01133  -0.0715   0.9226   0.1998
  -7.750  -0.5091   0.01756   0.01107  -0.0723   0.9098   0.2098
  -7.500  -0.4770   0.01750   0.01087  -0.0729   0.8971   0.2195
  -7.000  -0.4206   0.01726   0.01046  -0.0725   0.8692   0.2362
  -6.750  -0.3950   0.01707   0.01022  -0.0718   0.8544   0.2436
  -6.500  -0.3691   0.01701   0.01007  -0.0712   0.8407   0.2512
  -6.250  -0.3432   0.01677   0.00965  -0.0706   0.8279   0.2579
  -6.000  -0.3177   0.01657   0.00945  -0.0699   0.8138   0.2639
  -5.750  -0.2922   0.01643   0.00916  -0.0692   0.8004   0.2704
  -5.500  -0.2660   0.01614   0.00874  -0.0686   0.7888   0.2762
  -5.250  -0.2400   0.01593   0.00851  -0.0680   0.7759   0.2819
  -5.000  -0.2141   0.01579   0.00824  -0.0674   0.7634   0.2884
  -4.750  -0.1875   0.01553   0.00787  -0.0669   0.7525   0.2944
  -4.500  -0.1615   0.01535   0.00767  -0.0664   0.7398   0.3005
  -4.250  -0.1350   0.01525   0.00742  -0.0659   0.7288   0.3076
  -4.000  -0.1085   0.01500   0.00714  -0.0655   0.7180   0.3141
  -3.750  -0.0821   0.01486   0.00697  -0.0650   0.7063   0.3212
  -3.500  -0.0551   0.01475   0.00669  -0.0646   0.6965   0.3289
  -3.250  -0.0291   0.01457   0.00657  -0.0641   0.6849   0.3366
  -3.000  -0.0020   0.01452   0.00638  -0.0637   0.6754   0.3455
  -2.750   0.0243   0.01432   0.00623  -0.0633   0.6649   0.3537
  -2.500   0.0512   0.01429   0.00609  -0.0629   0.6553   0.3641
  -2.250   0.0776   0.01412   0.00597  -0.0625   0.6454   0.3739
  -2.000   0.1044   0.01407   0.00586  -0.0621   0.6362   0.3854
  -1.750   0.1309   0.01397   0.00578  -0.0617   0.6272   0.3971
  -1.500   0.1575   0.01390   0.00571  -0.0613   0.6188   0.4100
  -1.250   0.1840   0.01383   0.00565  -0.0609   0.6097   0.4248
  -1.000   0.2109   0.01381   0.00560  -0.0606   0.6020   0.4411
  -0.750   0.2369   0.01373   0.00559  -0.0601   0.5933   0.4579
  -0.500   0.2639   0.01370   0.00555  -0.0598   0.5865   0.4774
  -0.250   0.2894   0.01363   0.00560  -0.0593   0.5781   0.4990
   0.000   0.3155   0.01356   0.00560  -0.0588   0.5709   0.5228
   0.250   0.3413   0.01354   0.00567  -0.0582   0.5641   0.5505
   0.500   0.3665   0.01347   0.00574  -0.0576   0.5566   0.5823
   0.750   0.3923   0.01345   0.00579  -0.0569   0.5505   0.6200
   1.000   0.4163   0.01340   0.00595  -0.0560   0.5435   0.6623
   1.250   0.4406   0.01335   0.00605  -0.0549   0.5369   0.7094
   1.750   0.4883   0.01337   0.00638  -0.0524   0.5247   0.8105
   2.000   0.5143   0.01341   0.00651  -0.0514   0.5184   0.8607
   2.250   0.5485   0.01358   0.00664  -0.0521   0.5128   0.9044
   2.500   0.5890   0.01371   0.00686  -0.0543   0.5053   0.9385
   2.750   0.6360   0.01388   0.00694  -0.0579   0.4985   0.9630
   3.000   0.6852   0.01410   0.00711  -0.0621   0.4917   0.9806
   3.250   0.7373   0.01423   0.00722  -0.0671   0.4841   0.9945
   3.500   0.7723   0.01440   0.00725  -0.0688   0.4785   1.0000
   3.750   0.7891   0.01458   0.00746  -0.0670   0.4728   1.0000
   4.000   0.8081   0.01474   0.00760  -0.0655   0.4668   1.0000
   4.250   0.8300   0.01493   0.00769  -0.0644   0.4617   1.0000
   4.500   0.8505   0.01517   0.00794  -0.0631   0.4560   1.0000
   4.750   0.8712   0.01535   0.00813  -0.0618   0.4498   1.0000
   5.000   0.8945   0.01555   0.00824  -0.0609   0.4444   1.0000
   5.250   0.9162   0.01581   0.00851  -0.0598   0.4386   1.0000
   5.500   0.9375   0.01601   0.00873  -0.0586   0.4321   1.0000
   5.750   0.9617   0.01621   0.00885  -0.0579   0.4265   1.0000
   6.000   0.9835   0.01648   0.00916  -0.0569   0.4203   1.0000
   6.250   1.0055   0.01669   0.00938  -0.0558   0.4137   1.0000
   6.500   1.0307   0.01692   0.00952  -0.0553   0.4079   1.0000
   6.750   1.0510   0.01719   0.00987  -0.0540   0.4011   1.0000
   7.000   1.0736   0.01739   0.01007  -0.0531   0.3944   1.0000
   7.250   1.0980   0.01768   0.01030  -0.0525   0.3884   1.0000
   7.500   1.1172   0.01791   0.01064  -0.0511   0.3809   1.0000
   7.750   1.1406   0.01814   0.01081  -0.0503   0.3745   1.0000
   8.000   1.1607   0.01845   0.01118  -0.0491   0.3675   1.0000
   8.250   1.1812   0.01868   0.01144  -0.0479   0.3602   1.0000
   8.500   1.2036   0.01900   0.01171  -0.0471   0.3537   1.0000
   8.750   1.2208   0.01928   0.01209  -0.0454   0.3458   1.0000
   9.000   1.2433   0.01958   0.01229  -0.0445   0.3392   1.0000
   9.250   1.2583   0.01992   0.01277  -0.0425   0.3314   1.0000
   9.500   1.2771   0.02022   0.01304  -0.0412   0.3244   1.0000
   9.750   1.2927   0.02063   0.01352  -0.0394   0.3170   1.0000
  10.000   1.3079   0.02099   0.01389  -0.0375   0.3096   1.0000
  10.250   1.3229   0.02144   0.01434  -0.0356   0.3025   1.0000
  10.500   1.3326   0.02187   0.01483  -0.0329   0.2954   1.0000
  10.750   1.3469   0.02237   0.01526  -0.0310   0.2887   1.0000
  11.000   1.3528   0.02293   0.01594  -0.0279   0.2815   1.0000
  11.250   1.3663   0.02351   0.01643  -0.0261   0.2749   1.0000
  11.500   1.3722   0.02425   0.01729  -0.0234   0.2680   1.0000
  11.750   1.3812   0.02497   0.01801  -0.0213   0.2613   1.0000
  12.000   1.3901   0.02583   0.01889  -0.0193   0.2548   1.0000
  12.250   1.3956   0.02677   0.01991  -0.0172   0.2483   1.0000
  12.500   1.4081   0.02765   0.02070  -0.0159   0.2420   1.0000
  12.750   1.4093   0.02889   0.02210  -0.0137   0.2357   1.0000
  13.000   1.4165   0.02999   0.02318  -0.0122   0.2297   1.0000
  13.250   1.4222   0.03130   0.02453  -0.0107   0.2238   1.0000
  13.500   1.4244   0.03278   0.02611  -0.0092   0.2178   1.0000
  13.750   1.4366   0.03386   0.02707  -0.0083   0.2120   1.0000
  14.000   1.4331   0.03583   0.02924  -0.0069   0.2066   1.0000
  14.250   1.4357   0.03753   0.03098  -0.0059   0.2013   1.0000
  14.500   1.4438   0.03896   0.03236  -0.0051   0.1959   1.0000
  14.750   1.4402   0.04126   0.03483  -0.0043   0.1908   1.0000
  15.000   1.4425   0.04318   0.03677  -0.0037   0.1858   1.0000
  15.250   1.4480   0.04494   0.03852  -0.0031   0.1808   1.0000
  15.500   1.4430   0.04765   0.04139  -0.0028   0.1760   1.0000
  15.750   1.4446   0.04981   0.04357  -0.0025   0.1713   1.0000
  16.000   1.4492   0.05179   0.04555  -0.0022   0.1667   1.0000
  16.250   1.4426   0.05499   0.04891  -0.0024   0.1623   1.0000
  16.500   1.4425   0.05755   0.05151  -0.0026   0.1579   1.0000
  16.750   1.4482   0.05952   0.05344  -0.0024   0.1534   1.0000
  17.000   1.4393   0.06330   0.05741  -0.0031   0.1494   1.0000
  17.250   1.4372   0.06631   0.06048  -0.0037   0.1453   1.0000
  17.500   1.4465   0.06791   0.06198  -0.0036   0.1408   1.0000
  17.750   1.4334   0.07253   0.06683  -0.0049   0.1374   1.0000
  18.000   1.4286   0.07612   0.07051  -0.0059   0.1335   1.0000
  18.250   1.4380   0.07771   0.07199  -0.0060   0.1293   1.0000
  18.500   1.4258   0.08250   0.07697  -0.0076   0.1260   1.0000
  18.750   1.4167   0.08696   0.08156  -0.0092   0.1224   1.0000
  19.000   1.4183   0.08981   0.08441  -0.0101   0.1188   1.0000
  19.250   1.4181   0.09294   0.08757  -0.0111   0.1153   1.0000
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