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MH 104 15.28% (mh104-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: MH 104 15.28% (mh104-il)
Reynolds number: 200,000
Max Cl/Cd: 62.83 at α=10°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh104-il-200000.txt
Download as CSV file: xf-mh104-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 104  15.28%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.5581   0.08295   0.07966  -0.0248   1.0000   0.0275
 -12.250  -0.5889   0.07337   0.06997  -0.0306   1.0000   0.0272
 -12.000  -0.7061   0.06886   0.06492  -0.0393   1.0000   0.0280
 -11.750  -0.7207   0.06396   0.05993  -0.0418   1.0000   0.0277
 -11.500  -0.7384   0.05918   0.05502  -0.0436   1.0000   0.0271
 -11.250  -0.7566   0.05508   0.05076  -0.0441   1.0000   0.0267
 -11.000  -0.7761   0.05124   0.04671  -0.0432   1.0000   0.0259
 -10.750  -0.8216   0.04632   0.04120  -0.0382   1.0000   0.0241
 -10.500  -0.8362   0.04515   0.03952  -0.0336   1.0000   0.0232
 -10.250  -0.8277   0.04162   0.03584  -0.0324   1.0000   0.0228
 -10.000  -0.8208   0.03870   0.03270  -0.0307   1.0000   0.0226
  -9.750  -0.8125   0.03606   0.02980  -0.0288   1.0000   0.0225
  -9.500  -0.7998   0.03371   0.02724  -0.0272   1.0000   0.0224
  -9.250  -0.7851   0.03162   0.02490  -0.0257   1.0000   0.0225
  -9.000  -0.7683   0.02977   0.02285  -0.0243   1.0000   0.0227
  -8.750  -0.7502   0.02822   0.02110  -0.0230   1.0000   0.0230
  -8.500  -0.7300   0.02606   0.01892  -0.0222   1.0000   0.0236
  -8.250  -0.7124   0.02457   0.01749  -0.0211   1.0000   0.0244
  -8.000  -0.6781   0.02307   0.01600  -0.0232   0.9715   0.0258
  -7.750  -0.6367   0.02201   0.01474  -0.0262   0.9344   0.0286
  -7.500  -0.6142   0.02048   0.01323  -0.0258   0.8988   0.0315
  -7.250  -0.5962   0.01974   0.01233  -0.0238   0.8694   0.0348
  -7.000  -0.5843   0.01868   0.01119  -0.0209   0.8457   0.0384
  -6.750  -0.5695   0.01780   0.01021  -0.0185   0.8243   0.0465
  -6.500  -0.5547   0.01675   0.00913  -0.0161   0.8060   0.0652
  -6.250  -0.5453   0.01502   0.00800  -0.0134   0.7896   0.1579
  -6.000  -0.5264   0.01447   0.00766  -0.0119   0.7737   0.2297
  -5.750  -0.5044   0.01424   0.00745  -0.0107   0.7585   0.2666
  -5.500  -0.4813   0.01410   0.00725  -0.0096   0.7439   0.2952
  -5.250  -0.4576   0.01398   0.00705  -0.0087   0.7301   0.3183
  -5.000  -0.4334   0.01388   0.00684  -0.0078   0.7173   0.3398
  -4.750  -0.4096   0.01376   0.00668  -0.0069   0.7054   0.3615
  -4.500  -0.3853   0.01368   0.00652  -0.0060   0.6927   0.3846
  -4.250  -0.3606   0.01353   0.00635  -0.0053   0.6804   0.4044
  -4.000  -0.3355   0.01337   0.00616  -0.0046   0.6692   0.4225
  -3.750  -0.3102   0.01323   0.00595  -0.0039   0.6592   0.4406
  -3.500  -0.2845   0.01307   0.00577  -0.0034   0.6480   0.4594
  -3.250  -0.2589   0.01294   0.00560  -0.0028   0.6382   0.4796
  -3.000  -0.2334   0.01277   0.00542  -0.0022   0.6289   0.4998
  -2.750  -0.2079   0.01261   0.00530  -0.0016   0.6188   0.5222
  -2.500  -0.1826   0.01249   0.00516  -0.0009   0.6107   0.5464
  -2.250  -0.1573   0.01234   0.00508  -0.0002   0.6014   0.5730
  -2.000  -0.1321   0.01223   0.00500   0.0005   0.5942   0.6015
  -1.750  -0.1070   0.01209   0.00497   0.0012   0.5858   0.6331
  -1.500  -0.0820   0.01201   0.00493   0.0021   0.5791   0.6673
  -1.250  -0.0567   0.01190   0.00494   0.0029   0.5710   0.7039
  -1.000  -0.0309   0.01186   0.00494   0.0037   0.5650   0.7412
  -0.750  -0.0042   0.01183   0.00505   0.0043   0.5578   0.7790
  -0.500   0.0244   0.01187   0.00512   0.0047   0.5518   0.8149
  -0.250   0.0558   0.01199   0.00527   0.0045   0.5457   0.8470
   0.000   0.0909   0.01215   0.00543   0.0035   0.5389   0.8741
   0.250   0.1290   0.01240   0.00557   0.0020   0.5336   0.8955
   0.500   0.1691   0.01264   0.00583  -0.0001   0.5270   0.9125
   0.750   0.2092   0.01291   0.00600  -0.0022   0.5215   0.9267
   1.000   0.2505   0.01320   0.00621  -0.0046   0.5162   0.9388
   1.250   0.2987   0.01345   0.00643  -0.0086   0.5098   0.9461
   1.500   0.3406   0.01367   0.00656  -0.0113   0.5048   0.9565
   1.750   0.3856   0.01390   0.00674  -0.0147   0.4996   0.9653
   2.000   0.4307   0.01404   0.00687  -0.0183   0.4937   0.9737
   2.250   0.4740   0.01418   0.00692  -0.0215   0.4889   0.9827
   2.500   0.5211   0.01427   0.00702  -0.0256   0.4836   0.9900
   2.750   0.5675   0.01430   0.00705  -0.0297   0.4779   0.9974
   3.000   0.5988   0.01433   0.00702  -0.0308   0.4736   1.0000
   3.250   0.6204   0.01447   0.00714  -0.0300   0.4697   1.0000
   3.500   0.6418   0.01457   0.00731  -0.0291   0.4647   1.0000
   3.750   0.6638   0.01467   0.00740  -0.0283   0.4604   1.0000
   4.000   0.6864   0.01483   0.00748  -0.0275   0.4567   1.0000
   4.250   0.7079   0.01503   0.00776  -0.0266   0.4520   1.0000
   4.500   0.7299   0.01518   0.00797  -0.0258   0.4471   1.0000
   4.750   0.7528   0.01533   0.00807  -0.0250   0.4430   1.0000
   5.000   0.7754   0.01557   0.00832  -0.0242   0.4388   1.0000
   5.250   0.7969   0.01577   0.00862  -0.0232   0.4333   1.0000
   5.500   0.8199   0.01592   0.00876  -0.0224   0.4287   1.0000
   5.750   0.8434   0.01615   0.00894  -0.0217   0.4245   1.0000
   6.000   0.8644   0.01637   0.00931  -0.0206   0.4185   1.0000
   6.250   0.8875   0.01650   0.00944  -0.0198   0.4134   1.0000
   6.500   0.9108   0.01673   0.00965  -0.0190   0.4085   1.0000
   6.750   0.9317   0.01693   0.00998  -0.0180   0.4020   1.0000
   7.000   0.9556   0.01704   0.01007  -0.0172   0.3967   1.0000
   7.250   0.9769   0.01729   0.01041  -0.0162   0.3906   1.0000
   7.500   0.9990   0.01744   0.01061  -0.0152   0.3841   1.0000
   7.750   1.0227   0.01760   0.01074  -0.0145   0.3785   1.0000
   8.000   1.0426   0.01780   0.01111  -0.0132   0.3710   1.0000
   8.250   1.0666   0.01790   0.01114  -0.0125   0.3650   1.0000
   8.500   1.0855   0.01813   0.01155  -0.0111   0.3569   1.0000
   8.750   1.1085   0.01821   0.01160  -0.0102   0.3501   1.0000
   9.000   1.1270   0.01844   0.01200  -0.0088   0.3413   1.0000
   9.250   1.1487   0.01855   0.01208  -0.0078   0.3337   1.0000
   9.500   1.1663   0.01875   0.01244  -0.0062   0.3239   1.0000
   9.750   1.1846   0.01896   0.01272  -0.0048   0.3143   1.0000
  10.000   1.2031   0.01915   0.01290  -0.0033   0.3046   1.0000
  10.250   1.2182   0.01944   0.01331  -0.0015   0.2929   1.0000
  10.500   1.2326   0.01981   0.01375   0.0004   0.2808   1.0000
  10.750   1.2451   0.02025   0.01423   0.0025   0.2683   1.0000
  11.000   1.2554   0.02079   0.01479   0.0049   0.2556   1.0000
  11.250   1.2626   0.02146   0.01545   0.0075   0.2431   1.0000
  11.500   1.2650   0.02225   0.01622   0.0108   0.2316   1.0000
  11.750   1.2635   0.02315   0.01714   0.0144   0.2207   1.0000
  12.000   1.2624   0.02429   0.01831   0.0172   0.2097   1.0000
  12.250   1.2606   0.02571   0.01975   0.0194   0.1992   1.0000
  12.500   1.2572   0.02746   0.02146   0.0212   0.1894   1.0000
  12.750   1.2552   0.02938   0.02344   0.0224   0.1790   1.0000
  13.000   1.2524   0.03155   0.02566   0.0232   0.1693   1.0000
  13.250   1.2475   0.03402   0.02811   0.0238   0.1608   1.0000
  13.500   1.2433   0.03664   0.03077   0.0241   0.1517   1.0000
  13.750   1.2385   0.03940   0.03359   0.0242   0.1435   1.0000
  14.000   1.2309   0.04249   0.03664   0.0241   0.1360   1.0000
  14.250   1.2264   0.04545   0.03972   0.0239   0.1282   1.0000
  14.500   1.2172   0.04885   0.04306   0.0236   0.1215   1.0000
  14.750   1.2117   0.05211   0.04644   0.0231   0.1140   1.0000
  15.000   1.2031   0.05570   0.04998   0.0225   0.1077   1.0000
  15.250   1.1973   0.05925   0.05364   0.0216   0.1009   1.0000
  15.500   1.1891   0.06302   0.05736   0.0208   0.0950   1.0000
  15.750   1.1823   0.06691   0.06136   0.0197   0.0884   1.0000
  16.000   1.1740   0.07090   0.06530   0.0187   0.0827   1.0000
  16.250   1.1669   0.07502   0.06951   0.0173   0.0767   1.0000
  16.500   1.1590   0.07906   0.07349   0.0162   0.0716   1.0000
  16.750   1.1525   0.08330   0.07785   0.0147   0.0664   1.0000
  17.000   1.1449   0.08741   0.08188   0.0135   0.0618   1.0000
  17.250   1.1394   0.09161   0.08621   0.0120   0.0577   1.0000
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