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AH 88-K-136/16 (ah88k136-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: AH 88-K-136/16 (ah88k136-il)
Reynolds number: 200,000
Max Cl/Cd: 73.32 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah88k136-il-200000.txt
Download as CSV file: xf-ah88k136-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 88-K-136/16                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.2201   0.10549   0.10154  -0.0963   0.8894   0.0508
 -11.500  -0.2287   0.10198   0.09808  -0.0997   0.8884   0.0512
 -11.250  -0.2323   0.09828   0.09441  -0.1023   0.8876   0.0513
 -11.000  -0.2366   0.09435   0.09052  -0.1049   0.8868   0.0514
 -10.750  -0.2157   0.09048   0.08662  -0.1012   0.8865   0.0533
 -10.500  -0.2065   0.08816   0.08431  -0.1009   0.8859   0.0550
 -10.250  -0.2051   0.08506   0.08123  -0.1020   0.8852   0.0562
 -10.000  -0.2075   0.08167   0.07788  -0.1035   0.8841   0.0575
  -9.750  -0.2137   0.07800   0.07426  -0.1055   0.8827   0.0588
  -9.500  -0.2272   0.07354   0.06985  -0.1089   0.8815   0.0596
  -9.250  -0.2558   0.06928   0.06556  -0.1109   0.8800   0.0616
  -9.000  -0.2748   0.06659   0.06282  -0.1092   0.8785   0.0618
  -8.750  -0.3031   0.06532   0.06140  -0.1046   0.8764   0.0626
  -8.500  -0.3279   0.06466   0.06047  -0.0998   0.8749   0.0633
  -8.250  -0.2884   0.04658   0.04288  -0.0984   0.8725   0.0656
  -8.000  -0.2741   0.04484   0.04120  -0.0977   0.8713   0.0683
  -7.750  -0.2776   0.04260   0.03888  -0.0954   0.8700   0.0711
  -7.500  -0.2899   0.04035   0.03640  -0.0917   0.8681   0.0749
  -7.250  -0.3140   0.04009   0.03561  -0.0842   0.8656   0.0774
  -7.000  -0.3686   0.03958   0.03355  -0.0766   0.8661   0.0414
  -6.750  -0.3627   0.03773   0.03148  -0.0734   0.8641   0.0408
  -6.500  -0.3602   0.03566   0.02912  -0.0695   0.8628   0.0407
  -6.250  -0.3554   0.03441   0.02753  -0.0656   0.8608   0.0410
  -6.000  -0.3431   0.03206   0.02496  -0.0635   0.8587   0.0431
  -5.750  -0.4914   0.04008   0.03386  -0.0350   0.8916   0.0407
  -5.500  -0.4694   0.03690   0.03020  -0.0340   0.8881   0.0405
  -5.250  -0.4430   0.03401   0.02680  -0.0333   0.8774   0.0422
  -5.000  -0.4132   0.03289   0.02559  -0.0338   0.8681   0.0449
  -4.750  -0.3860   0.03165   0.02408  -0.0333   0.8607   0.0467
  -4.500  -0.4525   0.03311   0.02568  -0.0187   0.8903   0.0456
  -4.250  -0.4187   0.03193   0.02419  -0.0194   0.8804   0.0477
  -4.000  -0.3823   0.03129   0.02324  -0.0204   0.8698   0.0518
  -3.750  -0.3275   0.02980   0.02173  -0.0249   0.8543   0.0577
  -3.500  -0.1929   0.02717   0.01896  -0.0419   0.8258   0.0779
  -3.250  -0.1971   0.02709   0.01894  -0.0363   0.8196   0.0827
  -3.000  -0.1530   0.02654   0.01842  -0.0392   0.8174   0.0998
  -2.750  -0.1581   0.02672   0.01855  -0.0333   0.8100   0.1074
  -2.500  -0.1213   0.02622   0.01819  -0.0349   0.8074   0.1351
  -2.250   0.0032   0.02390   0.01903  -0.0532   0.8094   0.8764
  -2.000  -0.0018   0.02479   0.01985  -0.0466   0.8022   0.9099
  -1.750   0.1648   0.02593   0.02060  -0.0710   0.8082   0.9454
  -1.500   0.2817   0.02607   0.02053  -0.0880   0.8086   0.9693
  -1.250   0.3891   0.02537   0.01969  -0.1039   0.8086   0.9914
  -1.000   0.4383   0.02510   0.01936  -0.1095   0.8042   1.0000
  -0.750   0.4547   0.02527   0.01949  -0.1078   0.7995   1.0000
  -0.500   0.4696   0.02551   0.01969  -0.1059   0.7944   1.0000
  -0.250   0.4828   0.02575   0.01990  -0.1039   0.7884   1.0000
   0.000   0.5057   0.02574   0.01984  -0.1028   0.7854   1.0000
   0.250   0.5136   0.02613   0.02024  -0.1002   0.7777   1.0000
   0.500   0.5344   0.02613   0.02020  -0.0990   0.7736   1.0000
   0.750   0.5595   0.02602   0.02007  -0.0981   0.7713   1.0000
   1.000   0.5658   0.02643   0.02049  -0.0953   0.7623   1.0000
   1.250   0.5904   0.02626   0.02030  -0.0945   0.7591   1.0000
   1.500   0.6174   0.02600   0.02003  -0.0938   0.7570   1.0000
   1.750   0.6235   0.02642   0.02049  -0.0909   0.7473   1.0000
   2.000   0.6499   0.02612   0.02018  -0.0903   0.7446   1.0000
   2.250   0.6738   0.02590   0.01996  -0.0893   0.7411   1.0000
   2.500   0.6853   0.02610   0.02020  -0.0870   0.7325   1.0000
   2.750   0.7137   0.02561   0.01974  -0.0865   0.7300   1.0000
   3.000   0.7404   0.02519   0.01934  -0.0858   0.7275   1.0000
   3.250   0.7509   0.02542   0.01962  -0.0833   0.7177   1.0000
   3.500   0.7810   0.02474   0.01900  -0.0830   0.7156   1.0000
   3.750   0.8104   0.02406   0.01836  -0.0825   0.7137   1.0000
   4.000   0.8211   0.02429   0.01866  -0.0800   0.7031   1.0000
   4.250   0.8523   0.02341   0.01784  -0.0798   0.7010   1.0000
   4.500   0.8663   0.02344   0.01794  -0.0776   0.6914   1.0000
   4.750   0.8965   0.02254   0.01713  -0.0772   0.6883   1.0000
   5.000   0.9292   0.02140   0.01607  -0.0770   0.6864   1.0000
   5.250   0.9450   0.02130   0.01608  -0.0749   0.6764   1.0000
   5.500   0.9765   0.02016   0.01504  -0.0745   0.6734   1.0000
   5.750   1.0111   0.01879   0.01376  -0.0745   0.6709   1.0000
   6.000   1.0325   0.01812   0.01320  -0.0728   0.6580   1.0000
   6.250   1.0598   0.01686   0.01200  -0.0715   0.6378   1.0000
   6.500   1.0861   0.01577   0.01085  -0.0700   0.6041   1.0000
   6.750   1.1086   0.01512   0.00997  -0.0678   0.5577   1.0000
   7.000   1.1194   0.01537   0.00992  -0.0644   0.5091   1.0000
   7.250   1.1222   0.01606   0.01039  -0.0600   0.4654   1.0000
   7.500   1.1157   0.01702   0.01110  -0.0543   0.4213   1.0000
   7.750   1.1040   0.01798   0.01190  -0.0478   0.3862   1.0000
   8.000   1.0836   0.01890   0.01268  -0.0400   0.3604   1.0000
   8.250   1.0665   0.01997   0.01360  -0.0331   0.3312   1.0000
   8.500   1.0482   0.02125   0.01465  -0.0264   0.2903   1.0000
   8.750   1.0307   0.02265   0.01576  -0.0201   0.2442   1.0000
   9.000   1.0062   0.02455   0.01719  -0.0131   0.1761   1.0000
   9.250   0.9844   0.02663   0.01871  -0.0070   0.1038   1.0000
   9.500   0.9688   0.02862   0.02033  -0.0017   0.0639   1.0000
   9.750   0.9637   0.03014   0.02179   0.0023   0.0525   1.0000
  10.000   0.9624   0.03149   0.02317   0.0056   0.0474   1.0000
  10.250   0.9585   0.03312   0.02483   0.0090   0.0435   1.0000
  10.500   0.9608   0.03443   0.02621   0.0116   0.0403   1.0000
  10.750   0.9618   0.03591   0.02773   0.0142   0.0377   1.0000
  11.000   0.9589   0.03782   0.02962   0.0170   0.0356   1.0000
  11.250   0.9661   0.03911   0.03099   0.0190   0.0339   1.0000
  11.500   0.9748   0.04038   0.03233   0.0208   0.0327   1.0000
  11.750   0.9856   0.04159   0.03359   0.0225   0.0313   1.0000
  12.000   0.9982   0.04278   0.03479   0.0240   0.0298   1.0000
  12.250   1.0284   0.04404   0.03596   0.0247   0.0276   1.0000
  12.500   1.0400   0.04532   0.03742   0.0261   0.0267   1.0000
  12.750   1.0588   0.04675   0.03903   0.0272   0.0259   1.0000
  13.000   1.0772   0.04851   0.04098   0.0283   0.0253   1.0000
  13.250   1.0936   0.05067   0.04338   0.0294   0.0251   1.0000
  13.500   1.1039   0.05327   0.04625   0.0309   0.0251   1.0000
  13.750   1.1057   0.05580   0.04903   0.0326   0.0247   1.0000
  14.000   1.1047   0.05830   0.05172   0.0342   0.0240   1.0000
  14.250   1.0974   0.06222   0.05599   0.0361   0.0248   1.0000
  14.500   1.0919   0.06463   0.05854   0.0374   0.0241   1.0000
  14.750   1.0950   0.06674   0.06067   0.0381   0.0230   1.0000
  15.000   1.0658   0.07221   0.06660   0.0398   0.0239   1.0000
  15.250   1.0481   0.07663   0.07127   0.0405   0.0241   1.0000
  15.500   1.0265   0.08205   0.07695   0.0406   0.0251   1.0000
  15.750   1.0034   0.08770   0.08283   0.0400   0.0253   1.0000
  16.000   0.9829   0.09352   0.08884   0.0388   0.0258   1.0000
  16.250   0.9613   0.09974   0.09524   0.0368   0.0261   1.0000
  16.500   0.9395   0.10653   0.10218   0.0343   0.0265   1.0000
  16.750   0.9156   0.11404   0.10985   0.0306   0.0265   1.0000
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