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AH 83-150 Q (ah83150q-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: AH 83-150 Q (ah83150q-il)
Reynolds number: 200,000
Max Cl/Cd: 73.87 at α=9°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ah83150q-il-200000.txt
Download as CSV file: xf-ah83150q-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AH 83-150 Q                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.2199   0.09853   0.09454  -0.0673   0.7972   0.0391
  -9.750  -0.2331   0.09344   0.08949  -0.0743   0.7943   0.0395
  -9.500  -0.2348   0.08869   0.08477  -0.0786   0.7909   0.0395
  -9.250  -0.2100   0.08699   0.08306  -0.0718   0.7886   0.0410
  -9.000  -0.1992   0.08485   0.08092  -0.0714   0.7858   0.0431
  -8.750  -0.1977   0.08144   0.07751  -0.0735   0.7833   0.0445
  -8.500  -0.2020   0.07717   0.07324  -0.0770   0.7809   0.0459
  -8.250  -0.2087   0.07269   0.06878  -0.0813   0.7779   0.0463
  -8.000  -0.2254   0.06860   0.06468  -0.0841   0.7741   0.0473
  -7.750  -0.2424   0.06567   0.06157  -0.0851   0.7707   0.0483
  -7.500  -0.2584   0.06423   0.05969  -0.0844   0.7679   0.0490
  -7.250  -0.2517   0.05800   0.05355  -0.0849   0.7660   0.0502
  -7.000  -0.2378   0.05543   0.05101  -0.0848   0.7639   0.0514
  -6.750  -0.2260   0.05313   0.04870  -0.0848   0.7609   0.0532
  -6.500  -0.2154   0.05075   0.04618  -0.0845   0.7578   0.0560
  -6.250  -0.2139   0.04845   0.04323  -0.0831   0.7548   0.0614
  -6.000  -0.1961   0.04507   0.03998  -0.0833   0.7526   0.0633
  -5.750  -0.1789   0.04311   0.03795  -0.0829   0.7505   0.0664
  -5.500  -0.1661   0.04147   0.03575  -0.0816   0.7484   0.0750
  -5.250  -0.1458   0.03893   0.03336  -0.0820   0.7452   0.0780
  -5.000  -0.1281   0.03772   0.03175  -0.0812   0.7420   0.0893
  -4.750  -0.1066   0.03550   0.02963  -0.0813   0.7395   0.0940
  -4.500  -0.0866   0.03392   0.02786  -0.0808   0.7372   0.1070
  -4.250  -0.0655   0.03247   0.02626  -0.0804   0.7351   0.1222
  -4.000  -0.0228   0.02642   0.01870  -0.0761   0.7335   0.0374
  -3.750   0.0051   0.02524   0.01708  -0.0752   0.7304   0.0319
  -3.500   0.0315   0.02377   0.01559  -0.0750   0.7273   0.0309
  -3.250   0.0579   0.02274   0.01449  -0.0746   0.7246   0.0303
  -3.000   0.0839   0.02189   0.01360  -0.0741   0.7221   0.0303
  -2.750   0.1094   0.02118   0.01282  -0.0734   0.7199   0.0311
  -2.500   0.1332   0.02044   0.01211  -0.0727   0.7180   0.0339
  -2.250   0.1565   0.02025   0.01197  -0.0723   0.7149   0.0377
  -2.000   0.1795   0.02008   0.01179  -0.0720   0.7109   0.0399
  -1.750   0.2038   0.01972   0.01139  -0.0715   0.7078   0.0470
  -1.500   0.2155   0.01736   0.01085  -0.0700   0.7053   0.4882
  -1.250   0.2139   0.01829   0.01282  -0.0605   0.7032   0.8280
  -1.000   0.2166   0.01920   0.01373  -0.0520   0.7014   0.8753
  -0.750   0.3283   0.01980   0.01415  -0.0623   0.6995   0.9408
  -0.500   0.3628   0.01999   0.01428  -0.0643   0.6949   0.9483
  -0.250   0.4072   0.01992   0.01409  -0.0678   0.6919   0.9551
   0.000   0.4364   0.01983   0.01389  -0.0683   0.6894   0.9605
   0.250   0.4735   0.01962   0.01357  -0.0703   0.6873   0.9631
   0.500   0.5066   0.01953   0.01336  -0.0716   0.6854   0.9661
   0.750   0.5261   0.02009   0.01399  -0.0715   0.6789   0.9704
   1.000   0.5517   0.02008   0.01394  -0.0715   0.6754   0.9732
   1.250   0.5856   0.01988   0.01367  -0.0729   0.6730   0.9750
   1.500   0.6172   0.01971   0.01341  -0.0738   0.6709   0.9768
   1.750   0.6404   0.02013   0.01388  -0.0740   0.6655   0.9793
   2.000   0.6636   0.02029   0.01405  -0.0739   0.6609   0.9814
   2.250   0.6902   0.02014   0.01386  -0.0738   0.6580   0.9832
   2.500   0.7177   0.01993   0.01359  -0.0738   0.6557   0.9846
   2.750   0.7432   0.02018   0.01387  -0.0742   0.6509   0.9860
   3.000   0.7695   0.02035   0.01408  -0.0747   0.6454   0.9878
   3.250   0.7990   0.02009   0.01380  -0.0751   0.6424   0.9890
   3.500   0.8285   0.01977   0.01344  -0.0754   0.6400   0.9900
   3.750   0.8496   0.02016   0.01391  -0.0751   0.6340   0.9920
   4.000   0.8752   0.02015   0.01394  -0.0751   0.6293   0.9936
   4.250   0.9041   0.01982   0.01360  -0.0753   0.6263   0.9945
   4.500   0.9360   0.01940   0.01313  -0.0759   0.6239   0.9952
   4.750   0.9558   0.01988   0.01375  -0.0756   0.6163   0.9972
   5.000   0.9865   0.01957   0.01346  -0.0762   0.6123   0.9986
   5.250   1.0192   0.01907   0.01294  -0.0769   0.6095   0.9995
   5.500   1.0336   0.01938   0.01336  -0.0752   0.6023   1.0000
   5.750   1.0560   0.01911   0.01313  -0.0742   0.5975   1.0000
   6.000   1.0862   0.01846   0.01245  -0.0742   0.5941   1.0000
   6.250   1.0963   0.01853   0.01264  -0.0714   0.5850   1.0000
   6.500   1.1272   0.01766   0.01172  -0.0713   0.5795   1.0000
   6.750   1.1373   0.01771   0.01188  -0.0685   0.5705   1.0000
   7.000   1.1627   0.01726   0.01142  -0.0679   0.5651   1.0000
   7.250   1.1708   0.01740   0.01168  -0.0647   0.5566   1.0000
   7.500   1.1938   0.01703   0.01132  -0.0637   0.5501   1.0000
   7.750   1.1979   0.01718   0.01158  -0.0599   0.5408   1.0000
   8.000   1.2164   0.01693   0.01134  -0.0581   0.5329   1.0000
   8.250   1.2232   0.01700   0.01148  -0.0548   0.5227   1.0000
   8.500   1.2375   0.01707   0.01163  -0.0528   0.5114   1.0000
   8.750   1.2560   0.01712   0.01172  -0.0516   0.4988   1.0000
   9.000   1.2750   0.01726   0.01188  -0.0506   0.4852   1.0000
   9.250   1.2919   0.01751   0.01216  -0.0494   0.4698   1.0000
   9.500   1.3045   0.01788   0.01253  -0.0476   0.4524   1.0000
   9.750   1.3137   0.01843   0.01301  -0.0455   0.4328   1.0000
  10.000   1.3193   0.01928   0.01382  -0.0433   0.4116   1.0000
  10.250   1.3233   0.02039   0.01485  -0.0412   0.3898   1.0000
  10.500   1.3269   0.02167   0.01606  -0.0394   0.3692   1.0000
  10.750   1.3292   0.02316   0.01753  -0.0378   0.3483   1.0000
  11.000   1.3301   0.02483   0.01912  -0.0361   0.3276   1.0000
  11.250   1.3304   0.02663   0.02087  -0.0346   0.3072   1.0000
  11.500   1.3297   0.02859   0.02277  -0.0332   0.2865   1.0000
  11.750   1.3277   0.03071   0.02480  -0.0318   0.2668   1.0000
  12.000   1.3262   0.03287   0.02691  -0.0305   0.2470   1.0000
  12.250   1.3249   0.03509   0.02907  -0.0294   0.2287   1.0000
  12.500   1.3236   0.03736   0.03129  -0.0283   0.2121   1.0000
  12.750   1.3232   0.03967   0.03356  -0.0274   0.1971   1.0000
  13.000   1.3236   0.04198   0.03584  -0.0266   0.1834   1.0000
  13.250   1.3246   0.04434   0.03818  -0.0260   0.1707   1.0000
  13.500   1.3255   0.04676   0.04058  -0.0255   0.1590   1.0000
  13.750   1.3258   0.04931   0.04310  -0.0250   0.1480   1.0000
  14.000   1.3250   0.05205   0.04580  -0.0247   0.1374   1.0000
  14.250   1.3263   0.05469   0.04848  -0.0245   0.1265   1.0000
  14.500   1.3267   0.05746   0.05129  -0.0243   0.1162   1.0000
  14.750   1.3253   0.06047   0.05426  -0.0241   0.1071   1.0000
  15.000   1.3249   0.06347   0.05727  -0.0242   0.0990   1.0000
  15.250   1.3267   0.06628   0.06016  -0.0242   0.0914   1.0000
  15.500   1.3266   0.06926   0.06306  -0.0242   0.0855   1.0000
  15.750   1.3306   0.07195   0.06589  -0.0245   0.0803   1.0000
  16.000   1.3309   0.07511   0.06906  -0.0250   0.0753   1.0000
  16.250   1.3344   0.07781   0.07182  -0.0252   0.0712   1.0000
  16.500   1.3367   0.08085   0.07498  -0.0258   0.0674   1.0000
  16.750   1.3377   0.08395   0.07807  -0.0264   0.0638   1.0000
  17.000   1.3401   0.08697   0.08120  -0.0270   0.0606   1.0000
  17.250   1.3411   0.09034   0.08472  -0.0280   0.0575   1.0000
  17.500   1.3413   0.09379   0.08823  -0.0290   0.0547   1.0000
  17.750   1.3430   0.09684   0.09129  -0.0297   0.0518   1.0000
  18.000   1.3426   0.10058   0.09523  -0.0310   0.0495   1.0000
  18.250   1.3419   0.10437   0.09914  -0.0324   0.0471   1.0000
  18.500   1.3406   0.10816   0.10297  -0.0339   0.0447   1.0000
  18.750   1.3399   0.11183   0.10673  -0.0351   0.0423   1.0000
  19.000   1.3367   0.11621   0.11131  -0.0370   0.0401   1.0000
  19.250   1.3322   0.12081   0.11602  -0.0392   0.0376   1.0000
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