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MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: MH 102 16.99% (mh102-il)
Reynolds number: 200,000
Max Cl/Cd: 65.21 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh102-il-200000-n5.txt
Download as CSV file: xf-mh102-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.6894   0.09126   0.08588  -0.0475   1.0000   0.0165
 -15.250  -0.6913   0.08754   0.08211  -0.0491   1.0000   0.0167
 -15.000  -0.6960   0.08341   0.07789  -0.0509   1.0000   0.0172
 -14.750  -0.7019   0.07921   0.07367  -0.0529   1.0000   0.0175
 -14.500  -0.7069   0.07527   0.06967  -0.0546   1.0000   0.0176
 -14.250  -0.7172   0.07076   0.06511  -0.0567   1.0000   0.0179
 -14.000  -0.7270   0.06639   0.06069  -0.0587   1.0000   0.0181
 -13.750  -0.7391   0.06175   0.05599  -0.0608   1.0000   0.0185
 -13.500  -0.7508   0.05723   0.05139  -0.0629   1.0000   0.0187
 -13.250  -0.7633   0.05265   0.04673  -0.0650   1.0000   0.0189
 -13.000  -0.7754   0.04815   0.04214  -0.0671   1.0000   0.0190
 -12.750  -0.7880   0.04363   0.03752  -0.0693   1.0000   0.0194
 -12.500  -0.7985   0.03953   0.03331  -0.0712   1.0000   0.0196
 -12.250  -0.8081   0.03596   0.02961  -0.0725   1.0000   0.0202
 -12.000  -0.8188   0.03303   0.02660  -0.0728   1.0000   0.0207
 -11.750  -0.8312   0.03083   0.02431  -0.0711   1.0000   0.0210
 -11.500  -0.8437   0.02939   0.02282  -0.0677   1.0000   0.0216
 -11.250  -0.8560   0.02836   0.02174  -0.0630   1.0000   0.0220
 -11.000  -0.8573   0.02730   0.02062  -0.0598   0.9990   0.0228
 -10.750  -0.8305   0.02577   0.01901  -0.0621   0.9880   0.0254
 -10.500  -0.8041   0.02446   0.01761  -0.0637   0.9757   0.0280
 -10.250  -0.7784   0.02325   0.01632  -0.0649   0.9618   0.0317
 -10.000  -0.7504   0.02210   0.01511  -0.0663   0.9482   0.0365
  -9.750  -0.7209   0.02098   0.01395  -0.0678   0.9349   0.0439
  -9.500  -0.6904   0.01988   0.01282  -0.0694   0.9211   0.0543
  -9.250  -0.6616   0.01884   0.01180  -0.0705   0.9054   0.0699
  -9.000  -0.6344   0.01793   0.01093  -0.0712   0.8891   0.0900
  -8.750  -0.6082   0.01723   0.01028  -0.0714   0.8724   0.1121
  -8.500  -0.5820   0.01677   0.00980  -0.0713   0.8560   0.1314
  -8.250  -0.5562   0.01645   0.00942  -0.0710   0.8403   0.1470
  -8.000  -0.5306   0.01622   0.00909  -0.0706   0.8251   0.1600
  -7.750  -0.5056   0.01601   0.00881  -0.0700   0.8106   0.1708
  -7.500  -0.4807   0.01583   0.00854  -0.0693   0.7961   0.1796
  -7.250  -0.4551   0.01570   0.00826  -0.0688   0.7827   0.1887
  -7.000  -0.4302   0.01554   0.00804  -0.0682   0.7700   0.1968
  -6.750  -0.4043   0.01545   0.00778  -0.0676   0.7571   0.2055
  -6.500  -0.3793   0.01527   0.00759  -0.0670   0.7450   0.2124
  -6.250  -0.3533   0.01516   0.00732  -0.0665   0.7336   0.2190
  -6.000  -0.3276   0.01498   0.00706  -0.0660   0.7214   0.2243
  -5.750  -0.3018   0.01481   0.00684  -0.0654   0.7102   0.2296
  -5.500  -0.2755   0.01469   0.00658  -0.0650   0.6991   0.2351
  -5.250  -0.2492   0.01454   0.00634  -0.0645   0.6885   0.2401
  -5.000  -0.2233   0.01439   0.00613  -0.0640   0.6783   0.2452
  -4.750  -0.1969   0.01426   0.00593  -0.0636   0.6672   0.2507
  -4.500  -0.1703   0.01416   0.00571  -0.0632   0.6572   0.2562
  -4.250  -0.1442   0.01401   0.00555  -0.0627   0.6469   0.2616
  -4.000  -0.1176   0.01391   0.00537  -0.0623   0.6378   0.2675
  -3.750  -0.0908   0.01383   0.00520  -0.0620   0.6278   0.2735
  -3.500  -0.0646   0.01371   0.00507  -0.0615   0.6186   0.2797
  -3.250  -0.0380   0.01364   0.00493  -0.0612   0.6089   0.2866
  -3.000  -0.0112   0.01357   0.00480  -0.0608   0.6001   0.2931
  -2.750   0.0153   0.01348   0.00470  -0.0604   0.5914   0.3004
  -2.500   0.0422   0.01345   0.00459  -0.0601   0.5834   0.3087
  -2.250   0.0686   0.01336   0.00452  -0.0597   0.5744   0.3166
  -2.000   0.0953   0.01334   0.00443  -0.0593   0.5666   0.3253
  -1.750   0.1219   0.01327   0.00438  -0.0590   0.5582   0.3342
  -1.500   0.1487   0.01326   0.00431  -0.0587   0.5510   0.3448
  -1.250   0.1753   0.01321   0.00429  -0.0583   0.5437   0.3554
  -1.000   0.2020   0.01320   0.00426  -0.0580   0.5360   0.3667
  -0.750   0.2284   0.01318   0.00424  -0.0576   0.5292   0.3788
  -0.500   0.2551   0.01315   0.00424  -0.0573   0.5220   0.3920
  -0.250   0.2815   0.01315   0.00424  -0.0569   0.5156   0.4066
   0.000   0.3082   0.01315   0.00426  -0.0566   0.5091   0.4221
   0.250   0.3345   0.01314   0.00429  -0.0562   0.5023   0.4384
   0.500   0.3606   0.01315   0.00431  -0.0558   0.4965   0.4568
   0.750   0.3869   0.01314   0.00437  -0.0554   0.4903   0.4775
   1.000   0.4129   0.01313   0.00444  -0.0549   0.4839   0.5001
   1.250   0.4385   0.01314   0.00449  -0.0544   0.4784   0.5248
   1.500   0.4643   0.01313   0.00459  -0.0539   0.4725   0.5540
   1.750   0.4896   0.01311   0.00470  -0.0533   0.4665   0.5863
   2.000   0.5145   0.01312   0.00479  -0.0526   0.4613   0.6219
   2.250   0.5393   0.01311   0.00493  -0.0519   0.4559   0.6611
   2.500   0.5638   0.01310   0.00507  -0.0510   0.4501   0.7031
   2.750   0.5878   0.01312   0.00521  -0.0500   0.4449   0.7485
   3.000   0.6122   0.01315   0.00536  -0.0490   0.4399   0.7957
   3.250   0.6389   0.01319   0.00554  -0.0484   0.4341   0.8434
   3.500   0.6711   0.01329   0.00571  -0.0490   0.4285   0.8903
   3.750   0.7099   0.01346   0.00587  -0.0511   0.4230   0.9308
   4.000   0.7517   0.01361   0.00606  -0.0539   0.4165   0.9626
   4.250   0.7923   0.01379   0.00621  -0.0567   0.4103   0.9874
   4.500   0.8260   0.01401   0.00638  -0.0580   0.4049   1.0000
   4.750   0.8474   0.01417   0.00656  -0.0569   0.3992   1.0000
   5.000   0.8689   0.01436   0.00672  -0.0557   0.3938   1.0000
   5.250   0.8907   0.01458   0.00688  -0.0546   0.3890   1.0000
   5.500   0.9129   0.01476   0.00710  -0.0536   0.3829   1.0000
   5.750   0.9350   0.01497   0.00730  -0.0526   0.3771   1.0000
   6.000   0.9569   0.01521   0.00749  -0.0516   0.3720   1.0000
   6.250   0.9794   0.01541   0.00775  -0.0507   0.3657   1.0000
   6.500   1.0012   0.01565   0.00797  -0.0496   0.3596   1.0000
   6.750   1.0228   0.01591   0.00821  -0.0486   0.3539   1.0000
   7.000   1.0446   0.01614   0.00849  -0.0476   0.3472   1.0000
   7.250   1.0654   0.01641   0.00875  -0.0464   0.3410   1.0000
   7.500   1.0864   0.01668   0.00905  -0.0454   0.3346   1.0000
   7.750   1.1066   0.01697   0.00935  -0.0441   0.3274   1.0000
   8.000   1.1257   0.01729   0.00965  -0.0428   0.3212   1.0000
   8.250   1.1453   0.01759   0.01001  -0.0415   0.3139   1.0000
   8.500   1.1627   0.01795   0.01035  -0.0399   0.3071   1.0000
   8.750   1.1807   0.01829   0.01074  -0.0384   0.2999   1.0000
   9.000   1.1953   0.01868   0.01113  -0.0364   0.2928   1.0000
   9.250   1.2092   0.01909   0.01155  -0.0343   0.2860   1.0000
   9.500   1.2224   0.01954   0.01202  -0.0321   0.2789   1.0000
   9.750   1.2342   0.02006   0.01254  -0.0299   0.2725   1.0000
  10.000   1.2473   0.02059   0.01312  -0.0280   0.2653   1.0000
  10.250   1.2574   0.02125   0.01375  -0.0258   0.2590   1.0000
  10.500   1.2698   0.02188   0.01444  -0.0240   0.2522   1.0000
  10.750   1.2795   0.02265   0.01522  -0.0221   0.2457   1.0000
  11.000   1.2892   0.02347   0.01607  -0.0203   0.2396   1.0000
  11.250   1.2989   0.02435   0.01700  -0.0186   0.2331   1.0000
  11.750   1.3153   0.02642   0.01914  -0.0154   0.2214   1.0000
  12.000   1.3218   0.02765   0.02040  -0.0140   0.2153   1.0000
  12.250   1.3279   0.02897   0.02174  -0.0126   0.2100   1.0000
  12.500   1.3353   0.03028   0.02312  -0.0115   0.2043   1.0000
  12.750   1.3391   0.03188   0.02474  -0.0104   0.1989   1.0000
  13.000   1.3447   0.03344   0.02637  -0.0095   0.1938   1.0000
  13.250   1.3496   0.03511   0.02811  -0.0087   0.1885   1.0000
  13.500   1.3510   0.03711   0.03011  -0.0079   0.1835   1.0000
  13.750   1.3552   0.03897   0.03205  -0.0073   0.1786   1.0000
  14.000   1.3579   0.04101   0.03417  -0.0068   0.1737   1.0000
  14.250   1.3574   0.04337   0.03654  -0.0064   0.1692   1.0000
  14.500   1.3599   0.04558   0.03884  -0.0061   0.1647   1.0000
  14.750   1.3607   0.04801   0.04135  -0.0060   0.1599   1.0000
  15.000   1.3593   0.05070   0.04406  -0.0060   0.1559   1.0000
  15.250   1.3600   0.05329   0.04673  -0.0061   0.1517   1.0000
  15.500   1.3601   0.05603   0.04956  -0.0063   0.1474   1.0000
  15.750   1.3578   0.05906   0.05262  -0.0066   0.1433   1.0000
  16.000   1.3568   0.06201   0.05562  -0.0070   0.1398   1.0000
  16.250   1.3561   0.06506   0.05878  -0.0076   0.1355   1.0000
  16.500   1.3537   0.06833   0.06211  -0.0082   0.1318   1.0000
  16.750   1.3503   0.07173   0.06552  -0.0090   0.1285   1.0000
  17.000   1.3495   0.07498   0.06890  -0.0098   0.1246   1.0000
  17.250   1.3466   0.07853   0.07253  -0.0108   0.1210   1.0000
  17.500   1.3426   0.08221   0.07623  -0.0118   0.1177   1.0000
  17.750   1.3404   0.08575   0.07987  -0.0129   0.1144   1.0000
  18.000   1.3369   0.08958   0.08380  -0.0141   0.1109   1.0000
  18.250   1.3323   0.09355   0.08782  -0.0155   0.1076   1.0000
  18.500   1.3291   0.09731   0.09161  -0.0169   0.1047   1.0000
  18.750   1.3249   0.10140   0.09583  -0.0184   0.1014   1.0000
  19.000   1.3203   0.10554   0.10005  -0.0201   0.0982   1.0000
  19.250   1.3159   0.10962   0.10414  -0.0218   0.0954   1.0000
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