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HQ 1.0/10 AIRFOIL (hq1010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 1.0/10 AIRFOIL (hq1010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.99 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq1010-il-1000000-n5.txt
Download as CSV file: xf-hq1010-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 1.0/10 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.9592   0.06267   0.06055  -0.0314   1.0000   0.0022
 -13.750  -0.9935   0.05116   0.04883  -0.0404   1.0000   0.0022
 -13.500  -1.0159   0.04426   0.04174  -0.0452   1.0000   0.0022
 -13.250  -1.0240   0.04033   0.03768  -0.0472   1.0000   0.0022
 -13.000  -1.0398   0.03621   0.03336  -0.0482   1.0000   0.0022
 -12.750  -1.0572   0.03274   0.02969  -0.0474   1.0000   0.0022
 -12.500  -1.0596   0.03106   0.02789  -0.0455   1.0000   0.0022
 -12.250  -1.0636   0.02918   0.02584  -0.0427   1.0000   0.0023
 -12.000  -1.0584   0.02739   0.02387  -0.0410   1.0000   0.0023
 -11.750  -1.0493   0.02579   0.02209  -0.0396   1.0000   0.0023
 -11.500  -1.0355   0.02455   0.02072  -0.0384   1.0000   0.0023
 -11.250  -1.0216   0.02320   0.01919  -0.0372   1.0000   0.0024
 -11.000  -1.0044   0.02215   0.01801  -0.0362   1.0000   0.0024
 -10.750  -0.9861   0.02120   0.01694  -0.0354   1.0000   0.0025
 -10.500  -0.9679   0.02017   0.01578  -0.0344   1.0000   0.0025
 -10.250  -0.9495   0.01911   0.01458  -0.0334   1.0000   0.0026
 -10.000  -0.9332   0.01769   0.01299  -0.0322   1.0000   0.0028
  -9.750  -0.9125   0.01694   0.01216  -0.0314   1.0000   0.0030
  -9.500  -0.8911   0.01629   0.01144  -0.0306   1.0000   0.0032
  -9.250  -0.8699   0.01563   0.01071  -0.0297   1.0000   0.0033
  -9.000  -0.8482   0.01508   0.01007  -0.0288   1.0000   0.0036
  -8.750  -0.8223   0.01447   0.00939  -0.0289   0.9970   0.0038
  -8.500  -0.7918   0.01387   0.00871  -0.0299   0.9907   0.0040
  -8.250  -0.7597   0.01328   0.00805  -0.0312   0.9845   0.0042
  -8.000  -0.7279   0.01276   0.00745  -0.0325   0.9760   0.0044
  -7.750  -0.6954   0.01230   0.00693  -0.0337   0.9663   0.0046
  -7.500  -0.6652   0.01165   0.00619  -0.0346   0.9524   0.0052
  -7.250  -0.6373   0.01124   0.00570  -0.0348   0.9338   0.0059
  -6.750  -0.5863   0.01067   0.00495  -0.0340   0.9003   0.0070
  -6.500  -0.5608   0.01042   0.00461  -0.0336   0.8872   0.0075
  -6.250  -0.5355   0.01008   0.00421  -0.0331   0.8754   0.0092
  -6.000  -0.5095   0.00981   0.00389  -0.0328   0.8651   0.0108
  -5.750  -0.4833   0.00958   0.00360  -0.0325   0.8559   0.0130
  -5.500  -0.4572   0.00932   0.00331  -0.0323   0.8469   0.0169
  -5.250  -0.4308   0.00906   0.00307  -0.0321   0.8387   0.0239
  -5.000  -0.4039   0.00889   0.00286  -0.0319   0.8307   0.0280
  -4.750  -0.3770   0.00869   0.00266  -0.0318   0.8226   0.0333
  -4.500  -0.3499   0.00855   0.00248  -0.0317   0.8149   0.0366
  -4.250  -0.3229   0.00836   0.00228  -0.0315   0.8067   0.0451
  -4.000  -0.2958   0.00818   0.00211  -0.0314   0.7990   0.0552
  -3.750  -0.2687   0.00799   0.00195  -0.0313   0.7908   0.0687
  -3.500  -0.2416   0.00780   0.00179  -0.0312   0.7827   0.0855
  -3.250  -0.2145   0.00762   0.00163  -0.0311   0.7742   0.1053
  -3.000  -0.1875   0.00741   0.00149  -0.0310   0.7648   0.1323
  -2.750  -0.1605   0.00720   0.00136  -0.0310   0.7560   0.1665
  -2.250  -0.1060   0.00683   0.00114  -0.0308   0.7393   0.2317
  -2.000  -0.0792   0.00660   0.00103  -0.0308   0.7292   0.2782
  -1.750  -0.0534   0.00621   0.00090  -0.0306   0.7169   0.3680
  -1.500  -0.0269   0.00596   0.00082  -0.0304   0.7044   0.4320
  -1.250  -0.0002   0.00574   0.00076  -0.0303   0.6924   0.4948
  -1.000   0.0267   0.00557   0.00074  -0.0301   0.6810   0.5505
  -0.750   0.0540   0.00550   0.00073  -0.0300   0.6693   0.5836
  -0.500   0.0818   0.00549   0.00072  -0.0300   0.6571   0.6041
  -0.250   0.1096   0.00550   0.00071  -0.0299   0.6440   0.6190
   0.250   0.1651   0.00553   0.00073  -0.0298   0.6163   0.6476
   0.500   0.1929   0.00555   0.00074  -0.0298   0.6029   0.6600
   0.750   0.2206   0.00559   0.00077  -0.0297   0.5866   0.6718
   1.000   0.2482   0.00564   0.00080  -0.0296   0.5689   0.6850
   1.250   0.2755   0.00571   0.00085  -0.0295   0.5475   0.6974
   1.500   0.3027   0.00583   0.00089  -0.0294   0.5192   0.7069
   1.750   0.3293   0.00602   0.00096  -0.0292   0.4798   0.7151
   2.250   0.3823   0.00647   0.00116  -0.0288   0.3991   0.7313
   2.750   0.4333   0.00716   0.00146  -0.0282   0.2867   0.7482
   3.000   0.4600   0.00733   0.00158  -0.0281   0.2647   0.7571
   3.250   0.4868   0.00750   0.00172  -0.0279   0.2457   0.7658
   3.750   0.5401   0.00786   0.00200  -0.0276   0.2051   0.7847
   4.000   0.5667   0.00802   0.00214  -0.0274   0.1888   0.7944
   4.250   0.5931   0.00820   0.00231  -0.0272   0.1713   0.8047
   4.500   0.6187   0.00848   0.00250  -0.0269   0.1434   0.8157
   4.750   0.6436   0.00881   0.00274  -0.0265   0.1126   0.8271
   5.000   0.6686   0.00910   0.00298  -0.0260   0.0908   0.8396
   5.250   0.6934   0.00939   0.00322  -0.0256   0.0711   0.8536
   5.500   0.7180   0.00963   0.00348  -0.0250   0.0580   0.8719
   5.750   0.7420   0.00981   0.00372  -0.0243   0.0484   0.8996
   6.000   0.7706   0.00999   0.00399  -0.0245   0.0402   0.9553
   6.250   0.8072   0.01035   0.00432  -0.0267   0.0300   1.0000
   6.500   0.8321   0.01069   0.00462  -0.0263   0.0234   1.0000
   6.750   0.8569   0.01104   0.00496  -0.0259   0.0175   1.0000
   7.000   0.8815   0.01142   0.00531  -0.0255   0.0128   1.0000
   7.250   0.9058   0.01182   0.00569  -0.0250   0.0091   1.0000
   7.500   0.9299   0.01224   0.00611  -0.0245   0.0058   1.0000
   7.750   0.9539   0.01267   0.00654  -0.0240   0.0046   1.0000
   8.000   0.9779   0.01310   0.00700  -0.0235   0.0040   1.0000
   8.250   1.0015   0.01356   0.00750  -0.0229   0.0035   1.0000
   8.500   1.0251   0.01399   0.00800  -0.0223   0.0033   1.0000
   8.750   1.0484   0.01446   0.00852  -0.0217   0.0031   1.0000
   9.000   1.0712   0.01497   0.00909  -0.0211   0.0029   1.0000
   9.250   1.0935   0.01550   0.00969  -0.0204   0.0027   1.0000
   9.500   1.1152   0.01610   0.01035  -0.0196   0.0025   1.0000
   9.750   1.1364   0.01672   0.01103  -0.0187   0.0024   1.0000
  10.000   1.1569   0.01739   0.01178  -0.0178   0.0024   1.0000
  10.250   1.1759   0.01819   0.01266  -0.0167   0.0022   1.0000
  10.500   1.1925   0.01920   0.01381  -0.0153   0.0020   1.0000
  10.750   1.2057   0.02047   0.01523  -0.0135   0.0019   1.0000
  11.000   1.2225   0.02129   0.01614  -0.0121   0.0019   1.0000
  11.250   1.2403   0.02195   0.01687  -0.0110   0.0018   1.0000
  11.500   1.2538   0.02293   0.01795  -0.0093   0.0018   1.0000
  11.750   1.2651   0.02386   0.01898  -0.0073   0.0018   1.0000
  12.000   1.2697   0.02502   0.02027  -0.0043   0.0018   1.0000
  12.250   1.2770   0.02601   0.02136  -0.0019   0.0017   1.0000
  12.500   1.2819   0.02722   0.02268   0.0005   0.0017   1.0000
  12.750   1.2819   0.02887   0.02447   0.0029   0.0017   1.0000
  13.000   1.2896   0.03004   0.02571   0.0044   0.0017   1.0000
  13.250   1.2897   0.03190   0.02772   0.0060   0.0017   1.0000
  13.500   1.2887   0.03401   0.02997   0.0073   0.0016   1.0000
  13.750   1.2876   0.03628   0.03237   0.0083   0.0016   1.0000
  14.000   1.2790   0.03951   0.03576   0.0088   0.0016   1.0000
  14.250   1.2724   0.04280   0.03920   0.0087   0.0016   1.0000
  14.500   1.2658   0.04637   0.04291   0.0081   0.0016   1.0000
  14.750   1.2534   0.05102   0.04771   0.0066   0.0016   1.0000
  15.000   1.2417   0.05603   0.05287   0.0045   0.0016   1.0000
  15.250   1.2284   0.06173   0.05872   0.0016   0.0016   1.0000
  15.500   1.2019   0.07036   0.06753  -0.0033   0.0016   1.0000
  15.750   1.1809   0.07881   0.07614  -0.0084   0.0016   1.0000
  16.000   1.1598   0.08782   0.08530  -0.0138   0.0016   1.0000
  16.250   1.1373   0.09732   0.09492  -0.0192   0.0016   1.0000
  16.500   1.0953   0.11120   0.10896  -0.0271   0.0017   1.0000
  16.750   1.0656   0.12270   0.12057  -0.0335   0.0017   1.0000
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