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HQ 3.5/14 AIRFOIL (hq3514-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.5/14 AIRFOIL (hq3514-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.5 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3514-il-1000000-n5.txt
Download as CSV file: xf-hq3514-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.5/14 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8987   0.06884   0.06609  -0.0775   1.0000   0.0061
 -16.500  -0.9606   0.05376   0.05068  -0.0881   1.0000   0.0059
 -16.250  -0.9827   0.04737   0.04413  -0.0923   1.0000   0.0058
 -16.000  -1.0017   0.04203   0.03864  -0.0955   1.0000   0.0059
 -15.750  -1.0134   0.03800   0.03449  -0.0974   1.0000   0.0060
 -15.500  -1.0203   0.03487   0.03125  -0.0985   1.0000   0.0061
 -15.250  -1.0266   0.03210   0.02838  -0.0988   1.0000   0.0062
 -15.000  -1.0299   0.02997   0.02616  -0.0984   1.0000   0.0063
 -14.750  -1.0194   0.02777   0.02385  -0.1003   0.9890   0.0064
 -14.500  -0.9984   0.02585   0.02182  -0.1036   0.9828   0.0066
 -14.250  -0.9736   0.02414   0.02000  -0.1070   0.9766   0.0068
 -14.000  -0.9474   0.02264   0.01839  -0.1102   0.9694   0.0071
 -13.750  -0.9236   0.02147   0.01711  -0.1119   0.9600   0.0073
 -13.500  -0.9059   0.02062   0.01615  -0.1117   0.9479   0.0075
 -13.250  -0.8895   0.01987   0.01530  -0.1110   0.9352   0.0077
 -13.000  -0.8730   0.01918   0.01450  -0.1100   0.9212   0.0079
 -12.750  -0.8569   0.01846   0.01368  -0.1088   0.9062   0.0083
 -12.500  -0.8391   0.01784   0.01295  -0.1078   0.8929   0.0087
 -12.250  -0.8202   0.01726   0.01228  -0.1069   0.8824   0.0092
 -12.000  -0.8001   0.01674   0.01166  -0.1061   0.8737   0.0097
 -11.750  -0.7788   0.01626   0.01109  -0.1055   0.8664   0.0102
 -11.500  -0.7573   0.01574   0.01052  -0.1048   0.8600   0.0110
 -11.250  -0.7349   0.01529   0.01000  -0.1043   0.8541   0.0118
 -11.000  -0.7115   0.01487   0.00952  -0.1039   0.8485   0.0125
 -10.750  -0.6879   0.01448   0.00906  -0.1035   0.8430   0.0132
 -10.500  -0.6639   0.01407   0.00862  -0.1031   0.8383   0.0141
 -10.250  -0.6392   0.01371   0.00822  -0.1029   0.8331   0.0150
 -10.000  -0.6143   0.01338   0.00783  -0.1026   0.8277   0.0158
  -9.750  -0.5891   0.01305   0.00745  -0.1023   0.8228   0.0166
  -9.500  -0.5637   0.01271   0.00709  -0.1021   0.8168   0.0176
  -9.250  -0.5381   0.01244   0.00677  -0.1019   0.8107   0.0186
  -9.000  -0.5119   0.01217   0.00645  -0.1018   0.8044   0.0195
  -8.750  -0.4860   0.01189   0.00612  -0.1016   0.7974   0.0205
  -8.500  -0.4599   0.01162   0.00582  -0.1014   0.7908   0.0216
  -8.250  -0.4335   0.01138   0.00555  -0.1013   0.7833   0.0226
  -8.000  -0.4070   0.01117   0.00527  -0.1011   0.7765   0.0236
  -7.750  -0.3801   0.01096   0.00501  -0.1011   0.7698   0.0243
  -7.500  -0.3537   0.01070   0.00472  -0.1009   0.7637   0.0258
  -7.250  -0.3266   0.01049   0.00450  -0.1009   0.7580   0.0274
  -7.000  -0.2994   0.01032   0.00429  -0.1008   0.7518   0.0287
  -6.750  -0.2722   0.01015   0.00406  -0.1008   0.7458   0.0296
  -6.500  -0.2450   0.00993   0.00381  -0.1007   0.7398   0.0313
  -6.250  -0.2177   0.00975   0.00361  -0.1007   0.7342   0.0331
  -6.000  -0.1902   0.00959   0.00342  -0.1007   0.7293   0.0346
  -5.750  -0.1623   0.00944   0.00324  -0.1007   0.7242   0.0359
  -5.500  -0.1347   0.00928   0.00306  -0.1007   0.7194   0.0380
  -5.250  -0.1070   0.00914   0.00291  -0.1008   0.7151   0.0409
  -5.000  -0.0788   0.00900   0.00276  -0.1008   0.7111   0.0433
  -4.750  -0.0508   0.00889   0.00261  -0.1009   0.7057   0.0454
  -4.250   0.0050   0.00866   0.00236  -0.1010   0.6944   0.0526
  -4.000   0.0331   0.00857   0.00224  -0.1010   0.6883   0.0556
  -3.750   0.0609   0.00847   0.00214  -0.1010   0.6823   0.0602
  -3.500   0.0894   0.00837   0.00204  -0.1012   0.6776   0.0643
  -3.250   0.1177   0.00827   0.00195  -0.1013   0.6732   0.0699
  -3.000   0.1457   0.00820   0.00187  -0.1013   0.6683   0.0759
  -2.750   0.1741   0.00812   0.00178  -0.1014   0.6634   0.0820
  -2.500   0.2024   0.00802   0.00171  -0.1015   0.6576   0.0909
  -2.000   0.2582   0.00775   0.00153  -0.1017   0.6452   0.1350
  -1.750   0.2858   0.00756   0.00148  -0.1018   0.6382   0.1935
  -1.250   0.3421   0.00736   0.00138  -0.1020   0.6267   0.2366
  -1.000   0.3695   0.00716   0.00134  -0.1021   0.6203   0.3013
  -0.750   0.3965   0.00675   0.00126  -0.1023   0.6133   0.4106
  -0.500   0.4241   0.00665   0.00128  -0.1023   0.6053   0.4752
  -0.250   0.4524   0.00666   0.00130  -0.1024   0.5978   0.4890
   0.000   0.4799   0.00670   0.00132  -0.1023   0.5857   0.5044
   0.250   0.5071   0.00675   0.00135  -0.1022   0.5698   0.5178
   0.500   0.5339   0.00686   0.00139  -0.1020   0.5478   0.5273
   0.750   0.5585   0.00708   0.00147  -0.1014   0.5104   0.5371
   1.000   0.5824   0.00738   0.00160  -0.1007   0.4705   0.5469
   1.250   0.6082   0.00754   0.00171  -0.1004   0.4524   0.5567
   1.750   0.6613   0.00781   0.00190  -0.1000   0.4290   0.5699
   2.250   0.7149   0.00802   0.00209  -0.0997   0.4114   0.5886
   2.500   0.7416   0.00813   0.00219  -0.0995   0.4023   0.5994
   2.750   0.7683   0.00824   0.00230  -0.0994   0.3917   0.6106
   3.000   0.7941   0.00839   0.00243  -0.0990   0.3741   0.6233
   3.250   0.8168   0.00873   0.00261  -0.0982   0.3326   0.6352
   3.500   0.8400   0.00905   0.00282  -0.0975   0.3093   0.6449
   3.750   0.8647   0.00927   0.00300  -0.0970   0.2966   0.6540
   4.000   0.8897   0.00946   0.00317  -0.0965   0.2876   0.6618
   4.250   0.9151   0.00961   0.00333  -0.0962   0.2805   0.6697
   4.500   0.9399   0.00981   0.00350  -0.0957   0.2726   0.6764
   4.750   0.9651   0.00996   0.00366  -0.0953   0.2655   0.6830
   5.250   1.0146   0.01029   0.00401  -0.0943   0.2528   0.6975
   5.500   1.0387   0.01049   0.00420  -0.0937   0.2448   0.7043
   5.750   1.0627   0.01068   0.00439  -0.0931   0.2364   0.7099
   6.000   1.0850   0.01095   0.00461  -0.0922   0.2212   0.7158
   6.250   1.1032   0.01142   0.00493  -0.0907   0.1912   0.7215
   6.500   1.1224   0.01180   0.00524  -0.0893   0.1748   0.7273
   6.750   1.1426   0.01210   0.00553  -0.0881   0.1656   0.7337
   7.000   1.1612   0.01239   0.00580  -0.0865   0.1582   0.7400
   7.250   1.1797   0.01264   0.00608  -0.0849   0.1528   0.7476
   7.750   1.2158   0.01323   0.00670  -0.0817   0.1420   0.7654
   8.000   1.2345   0.01349   0.00702  -0.0802   0.1381   0.7756
   8.750   1.2868   0.01442   0.00809  -0.0753   0.1244   0.8240
   9.000   1.3028   0.01470   0.00847  -0.0735   0.1193   0.8570
   9.500   1.3404   0.01543   0.00936  -0.0713   0.1055   1.0000
   9.750   1.3555   0.01598   0.00988  -0.0697   0.0984   1.0000
  10.000   1.3703   0.01656   0.01043  -0.0680   0.0901   1.0000
  10.250   1.3843   0.01720   0.01104  -0.0664   0.0822   1.0000
  10.500   1.3947   0.01807   0.01183  -0.0643   0.0694   1.0000
  10.750   1.4004   0.01924   0.01289  -0.0617   0.0527   1.0000
  11.000   1.4058   0.02049   0.01406  -0.0593   0.0392   1.0000
  11.250   1.4167   0.02143   0.01500  -0.0576   0.0342   1.0000
  11.500   1.4280   0.02238   0.01595  -0.0560   0.0306   1.0000
  11.750   1.4405   0.02327   0.01687  -0.0546   0.0283   1.0000
  12.000   1.4509   0.02432   0.01793  -0.0531   0.0256   1.0000
  12.250   1.4634   0.02526   0.01890  -0.0518   0.0242   1.0000
  12.500   1.4747   0.02630   0.01998  -0.0506   0.0221   1.0000
  12.750   1.4839   0.02752   0.02121  -0.0492   0.0199   1.0000
  13.000   1.4946   0.02866   0.02238  -0.0480   0.0177   1.0000
  13.250   1.5029   0.03002   0.02376  -0.0467   0.0152   1.0000
  13.500   1.5100   0.03150   0.02525  -0.0455   0.0124   1.0000
  13.750   1.5156   0.03316   0.02692  -0.0442   0.0099   1.0000
  14.000   1.5221   0.03479   0.02859  -0.0431   0.0086   1.0000
  14.250   1.5282   0.03651   0.03036  -0.0421   0.0077   1.0000
  14.500   1.5349   0.03822   0.03214  -0.0412   0.0071   1.0000
  14.750   1.5402   0.04011   0.03408  -0.0404   0.0067   1.0000
  15.000   1.5446   0.04216   0.03619  -0.0397   0.0063   1.0000
  15.250   1.5489   0.04427   0.03837  -0.0390   0.0059   1.0000
  15.500   1.5539   0.04636   0.04053  -0.0385   0.0057   1.0000
  15.750   1.5578   0.04862   0.04287  -0.0381   0.0055   1.0000
  16.000   1.5610   0.05104   0.04536  -0.0379   0.0053   1.0000
  16.250   1.5630   0.05366   0.04806  -0.0377   0.0051   1.0000
  16.500   1.5639   0.05648   0.05096  -0.0376   0.0049   1.0000
  16.750   1.5639   0.05948   0.05405  -0.0377   0.0048   1.0000
  17.000   1.5629   0.06271   0.05736  -0.0380   0.0047   1.0000
  17.250   1.5596   0.06636   0.06110  -0.0385   0.0045   1.0000
  17.500   1.5558   0.07018   0.06502  -0.0392   0.0044   1.0000
  17.750   1.5507   0.07430   0.06924  -0.0402   0.0043   1.0000
  18.000   1.5449   0.07868   0.07372  -0.0413   0.0042   1.0000
  18.250   1.5408   0.08292   0.07807  -0.0426   0.0041   1.0000
  18.500   1.5346   0.08759   0.08285  -0.0442   0.0041   1.0000
  18.750   1.5267   0.09259   0.08796  -0.0460   0.0041   1.0000
  19.000   1.5179   0.09784   0.09333  -0.0481   0.0040   1.0000
  19.250   1.5078   0.10341   0.09901  -0.0504   0.0040   1.0000
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