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MH 93 15.98% (mh93-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 93 15.98% (mh93-il)
Reynolds number: 500,000
Max Cl/Cd: 71.26 at α=10.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh93-il-500000-n5.txt
Download as CSV file: xf-mh93-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 93  15.98%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.9165   0.12443   0.12133   0.0197   1.0000   0.0068
 -17.250  -0.9504   0.11195   0.10863   0.0120   1.0000   0.0066
 -17.000  -0.9743   0.10224   0.09873   0.0060   1.0000   0.0067
 -16.750  -0.9966   0.09332   0.08962   0.0006   1.0000   0.0066
 -16.500  -1.0133   0.08586   0.08199  -0.0038   1.0000   0.0066
 -16.250  -1.0278   0.07915   0.07512  -0.0077   1.0000   0.0067
 -16.000  -1.0405   0.07303   0.06884  -0.0111   1.0000   0.0067
 -15.750  -1.0505   0.06764   0.06331  -0.0138   1.0000   0.0067
 -15.500  -1.0581   0.06291   0.05843  -0.0160   1.0000   0.0067
 -15.250  -1.0639   0.05866   0.05405  -0.0178   1.0000   0.0067
 -15.000  -1.0693   0.05469   0.04993  -0.0191   1.0000   0.0068
 -14.750  -1.0728   0.05118   0.04630  -0.0201   1.0000   0.0068
 -14.500  -1.0756   0.04792   0.04292  -0.0206   1.0000   0.0069
 -14.250  -1.0766   0.04506   0.03993  -0.0208   1.0000   0.0069
 -14.000  -1.0759   0.04250   0.03726  -0.0207   1.0000   0.0069
 -13.750  -1.0749   0.04008   0.03473  -0.0203   1.0000   0.0070
 -13.500  -1.0721   0.03795   0.03249  -0.0197   1.0000   0.0070
 -13.250  -1.0678   0.03603   0.03047  -0.0189   1.0000   0.0070
 -13.000  -1.0631   0.03422   0.02855  -0.0179   1.0000   0.0072
 -12.750  -1.0567   0.03261   0.02685  -0.0168   1.0000   0.0073
 -12.500  -1.0492   0.03114   0.02528  -0.0156   1.0000   0.0074
 -12.250  -1.0409   0.02978   0.02384  -0.0142   1.0000   0.0075
 -12.000  -1.0327   0.02844   0.02242  -0.0128   1.0000   0.0075
 -11.750  -1.0224   0.02730   0.02120  -0.0113   1.0000   0.0076
 -11.500  -1.0116   0.02621   0.02004  -0.0098   1.0000   0.0077
 -11.250  -1.0002   0.02519   0.01895  -0.0083   1.0000   0.0078
 -11.000  -0.9888   0.02418   0.01789  -0.0066   1.0000   0.0079
 -10.750  -0.9781   0.02315   0.01681  -0.0048   1.0000   0.0079
 -10.500  -0.9588   0.02222   0.01579  -0.0045   0.9199   0.0081
 -10.000  -0.9377   0.02106   0.01435   0.0008   0.8527   0.0084
  -9.750  -0.9250   0.02046   0.01364   0.0031   0.8327   0.0085
  -9.500  -0.9112   0.01989   0.01297   0.0053   0.8150   0.0086
  -9.250  -0.8962   0.01937   0.01236   0.0073   0.7993   0.0088
  -9.000  -0.8807   0.01889   0.01178   0.0094   0.7850   0.0090
  -8.750  -0.8648   0.01840   0.01119   0.0114   0.7710   0.0093
  -8.500  -0.8462   0.01793   0.01063   0.0129   0.7581   0.0096
  -8.250  -0.8266   0.01746   0.01009   0.0143   0.7456   0.0098
  -8.000  -0.8059   0.01706   0.00958   0.0155   0.7337   0.0100
  -7.750  -0.7859   0.01655   0.00903   0.0168   0.7215   0.0105
  -7.500  -0.7640   0.01617   0.00859   0.0178   0.7104   0.0110
  -7.250  -0.7417   0.01581   0.00815   0.0188   0.6988   0.0117
  -7.000  -0.7187   0.01546   0.00774   0.0197   0.6876   0.0125
  -6.750  -0.6962   0.01507   0.00731   0.0206   0.6769   0.0133
  -6.500  -0.6726   0.01474   0.00693   0.0214   0.6656   0.0145
  -6.250  -0.6490   0.01441   0.00654   0.0222   0.6550   0.0160
  -6.000  -0.6248   0.01411   0.00619   0.0229   0.6438   0.0178
  -5.750  -0.6006   0.01379   0.00586   0.0236   0.6336   0.0205
  -5.500  -0.5762   0.01351   0.00552   0.0243   0.6227   0.0247
  -5.250  -0.5516   0.01320   0.00522   0.0249   0.6122   0.0305
  -5.000  -0.5272   0.01289   0.00492   0.0256   0.6017   0.0408
  -4.750  -0.5031   0.01254   0.00462   0.0262   0.5910   0.0577
  -4.500  -0.4797   0.01211   0.00431   0.0270   0.5811   0.0862
  -4.250  -0.4572   0.01162   0.00399   0.0278   0.5708   0.1287
  -4.000  -0.4349   0.01109   0.00369   0.0287   0.5610   0.1839
  -3.750  -0.4130   0.01056   0.00340   0.0296   0.5509   0.2473
  -3.500  -0.3903   0.01009   0.00318   0.0304   0.5415   0.3085
  -3.250  -0.3668   0.00973   0.00298   0.0312   0.5316   0.3612
  -3.000  -0.3431   0.00937   0.00281   0.0319   0.5217   0.4121
  -2.750  -0.3196   0.00905   0.00266   0.0327   0.5125   0.4660
  -2.500  -0.2955   0.00876   0.00254   0.0335   0.5026   0.5164
  -2.250  -0.2700   0.00859   0.00244   0.0340   0.4930   0.5500
  -2.000  -0.2438   0.00846   0.00235   0.0344   0.4830   0.5763
  -1.750  -0.2173   0.00835   0.00228   0.0348   0.4741   0.6024
  -1.500  -0.1907   0.00826   0.00223   0.0352   0.4641   0.6280
  -1.250  -0.1641   0.00817   0.00220   0.0355   0.4547   0.6547
  -1.000  -0.1371   0.00813   0.00218   0.0359   0.4451   0.6787
  -0.750  -0.1097   0.00811   0.00218   0.0361   0.4363   0.6991
  -0.500  -0.0820   0.00812   0.00218   0.0363   0.4265   0.7161
  -0.250  -0.0540   0.00814   0.00219   0.0364   0.4173   0.7312
   0.000  -0.0261   0.00819   0.00221   0.0365   0.4083   0.7449
   0.250   0.0021   0.00822   0.00224   0.0366   0.3995   0.7563
   0.500   0.0302   0.00830   0.00226   0.0366   0.3903   0.7671
   0.750   0.0585   0.00835   0.00230   0.0367   0.3821   0.7768
   1.250   0.1149   0.00850   0.00240   0.0368   0.3652   0.7940
   1.500   0.1430   0.00860   0.00244   0.0368   0.3568   0.8021
   1.750   0.1712   0.00867   0.00252   0.0368   0.3496   0.8098
   2.000   0.1991   0.00878   0.00258   0.0368   0.3414   0.8184
   2.250   0.2271   0.00887   0.00268   0.0369   0.3342   0.8256
   2.500   0.2550   0.00898   0.00276   0.0370   0.3269   0.8332
   2.750   0.2829   0.00910   0.00284   0.0370   0.3202   0.8389
   3.000   0.3109   0.00920   0.00294   0.0370   0.3131   0.8441
   3.250   0.3385   0.00934   0.00304   0.0371   0.3063   0.8497
   3.500   0.3666   0.00944   0.00313   0.0370   0.3009   0.8549
   3.750   0.3943   0.00956   0.00325   0.0371   0.2947   0.8591
   4.000   0.4216   0.00971   0.00338   0.0371   0.2884   0.8638
   4.250   0.4494   0.00982   0.00349   0.0371   0.2827   0.8687
   4.500   0.4768   0.00996   0.00360   0.0371   0.2769   0.8734
   4.750   0.5038   0.01012   0.00376   0.0373   0.2719   0.8775
   5.000   0.5311   0.01024   0.00390   0.0374   0.2669   0.8822
   5.250   0.5579   0.01040   0.00405   0.0375   0.2612   0.8874
   5.500   0.5843   0.01058   0.00421   0.0377   0.2558   0.8924
   5.750   0.6111   0.01071   0.00438   0.0379   0.2513   0.8968
   6.000   0.6374   0.01088   0.00455   0.0381   0.2464   0.9015
   6.250   0.6632   0.01109   0.00473   0.0383   0.2411   0.9063
   6.500   0.6898   0.01123   0.00491   0.0384   0.2365   0.9101
   6.750   0.7158   0.01140   0.00510   0.0387   0.2318   0.9138
   7.000   0.7411   0.01162   0.00531   0.0390   0.2270   0.9180
   7.250   0.7666   0.01180   0.00551   0.0392   0.2225   0.9225
   7.500   0.7921   0.01198   0.00571   0.0395   0.2179   0.9266
   7.750   0.8170   0.01221   0.00595   0.0398   0.2131   0.9305
   8.000   0.8415   0.01244   0.00619   0.0402   0.2086   0.9349
   8.250   0.8660   0.01264   0.00642   0.0406   0.2039   0.9400
   8.500   0.8905   0.01290   0.00668   0.0409   0.1985   0.9443
   8.750   0.9151   0.01317   0.00697   0.0411   0.1937   0.9488
   9.000   0.9396   0.01340   0.00723   0.0414   0.1891   0.9539
   9.250   0.9647   0.01370   0.00754   0.0415   0.1845   0.9586
   9.500   0.9913   0.01405   0.00790   0.0411   0.1800   0.9631
   9.750   1.0176   0.01433   0.00823   0.0409   0.1759   0.9682
  10.000   1.0456   0.01468   0.00860   0.0402   0.1712   0.9721
  10.250   1.0742   0.01513   0.00905   0.0392   0.1665   0.9758
  10.500   1.1031   0.01548   0.00946   0.0383   0.1623   0.9802
  10.750   1.1321   0.01591   0.00991   0.0372   0.1577   0.9841
  11.000   1.1611   0.01646   0.01047   0.0358   0.1530   0.9877
  11.250   1.1901   0.01689   0.01096   0.0346   0.1486   0.9916
  11.500   1.2170   0.01745   0.01154   0.0336   0.1439   0.9980
  11.750   1.2183   0.01798   0.01207   0.0371   0.1407   1.0000
  12.000   1.2238   0.01849   0.01263   0.0399   0.1381   1.0000
  12.250   1.2323   0.01915   0.01333   0.0418   0.1343   1.0000
  12.500   1.2402   0.02002   0.01421   0.0433   0.1303   1.0000
  12.750   1.2485   0.02098   0.01521   0.0446   0.1271   1.0000
  13.000   1.2589   0.02192   0.01619   0.0455   0.1233   1.0000
  13.250   1.2669   0.02310   0.01740   0.0464   0.1192   1.0000
  13.500   1.2727   0.02451   0.01884   0.0472   0.1156   1.0000
  13.750   1.2816   0.02578   0.02017   0.0477   0.1121   1.0000
  14.000   1.2871   0.02737   0.02179   0.0481   0.1082   1.0000
  14.250   1.2891   0.02932   0.02377   0.0484   0.1045   1.0000
  14.500   1.2944   0.03106   0.02557   0.0486   0.1009   1.0000
  14.750   1.2964   0.03317   0.02773   0.0486   0.0975   1.0000
  15.000   1.2942   0.03574   0.03033   0.0485   0.0941   1.0000
  15.250   1.2959   0.03800   0.03266   0.0483   0.0911   1.0000
  15.500   1.2940   0.04068   0.03540   0.0479   0.0880   1.0000
  15.750   1.2879   0.04386   0.03861   0.0473   0.0851   1.0000
  16.000   1.2853   0.04678   0.04161   0.0466   0.0829   1.0000
  16.250   1.2822   0.04986   0.04477   0.0458   0.0805   1.0000
  16.500   1.2757   0.05344   0.04841   0.0447   0.0781   1.0000
  16.750   1.2667   0.05740   0.05242   0.0434   0.0760   1.0000
  17.000   1.2604   0.06114   0.05624   0.0421   0.0742   1.0000
  17.250   1.2553   0.06480   0.05999   0.0408   0.0724   1.0000
  17.500   1.2482   0.06878   0.06404   0.0393   0.0706   1.0000
  17.750   1.2380   0.07328   0.06861   0.0375   0.0688   1.0000
  18.000   1.2270   0.07797   0.07336   0.0355   0.0671   1.0000
  18.250   1.2201   0.08215   0.07762   0.0337   0.0653   1.0000
  18.500   1.2140   0.08632   0.08186   0.0319   0.0637   1.0000
  18.750   1.2054   0.09091   0.08653   0.0298   0.0620   1.0000
  19.000   1.1951   0.09582   0.09151   0.0275   0.0605   1.0000
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