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HQ 3.0/12 AIRFOIL (hq3012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/12 AIRFOIL (hq3012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.36 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3012-il-1000000-n5.txt
Download as CSV file: xf-hq3012-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.0/12 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.8535   0.04445   0.04192  -0.0791   1.0000   0.0042
 -13.500  -0.8738   0.03864   0.03594  -0.0831   1.0000   0.0041
 -13.250  -0.8936   0.03413   0.03126  -0.0850   1.0000   0.0041
 -13.000  -0.9043   0.03169   0.02872  -0.0844   1.0000   0.0041
 -12.750  -0.9050   0.02957   0.02648  -0.0846   0.9934   0.0042
 -12.500  -0.8858   0.02755   0.02430  -0.0868   0.9867   0.0043
 -12.250  -0.8628   0.02569   0.02226  -0.0892   0.9823   0.0044
 -12.000  -0.8379   0.02429   0.02074  -0.0910   0.9766   0.0045
 -11.750  -0.8107   0.02283   0.01913  -0.0931   0.9716   0.0046
 -11.500  -0.7852   0.02183   0.01803  -0.0941   0.9635   0.0048
 -11.250  -0.7609   0.02061   0.01665  -0.0950   0.9549   0.0049
 -11.000  -0.7381   0.01967   0.01557  -0.0952   0.9437   0.0050
 -10.750  -0.7167   0.01882   0.01459  -0.0948   0.9315   0.0051
 -10.500  -0.6955   0.01803   0.01366  -0.0944   0.9201   0.0052
 -10.250  -0.6736   0.01735   0.01284  -0.0939   0.9104   0.0054
 -10.000  -0.6508   0.01681   0.01218  -0.0934   0.9012   0.0055
  -9.750  -0.6279   0.01623   0.01149  -0.0929   0.8927   0.0057
  -9.500  -0.6041   0.01577   0.01092  -0.0925   0.8846   0.0058
  -9.250  -0.5802   0.01525   0.01031  -0.0921   0.8768   0.0059
  -9.000  -0.5577   0.01451   0.00943  -0.0916   0.8692   0.0060
  -8.750  -0.5348   0.01375   0.00854  -0.0911   0.8616   0.0062
  -8.500  -0.5108   0.01317   0.00785  -0.0907   0.8551   0.0064
  -8.250  -0.4858   0.01267   0.00728  -0.0904   0.8485   0.0066
  -8.000  -0.4606   0.01224   0.00677  -0.0901   0.8421   0.0068
  -7.750  -0.4349   0.01184   0.00630  -0.0899   0.8359   0.0070
  -7.500  -0.4089   0.01148   0.00587  -0.0897   0.8295   0.0072
  -7.250  -0.3828   0.01114   0.00546  -0.0895   0.8236   0.0075
  -7.000  -0.3563   0.01083   0.00509  -0.0894   0.8172   0.0079
  -6.750  -0.3298   0.01055   0.00475  -0.0892   0.8113   0.0082
  -6.500  -0.3029   0.01027   0.00441  -0.0891   0.8052   0.0084
  -6.250  -0.2763   0.00997   0.00404  -0.0889   0.7990   0.0089
  -6.000  -0.2493   0.00969   0.00372  -0.0888   0.7933   0.0097
  -5.750  -0.2222   0.00945   0.00344  -0.0888   0.7872   0.0105
  -5.500  -0.1950   0.00925   0.00319  -0.0887   0.7815   0.0116
  -5.250  -0.1677   0.00901   0.00295  -0.0886   0.7754   0.0151
  -5.000  -0.1406   0.00878   0.00275  -0.0886   0.7696   0.0222
  -4.750  -0.1128   0.00863   0.00259  -0.0886   0.7641   0.0269
  -4.500  -0.0851   0.00851   0.00243  -0.0886   0.7580   0.0292
  -4.250  -0.0575   0.00837   0.00228  -0.0886   0.7525   0.0331
  -4.000  -0.0295   0.00825   0.00215  -0.0886   0.7465   0.0365
  -3.750  -0.0018   0.00811   0.00201  -0.0886   0.7403   0.0423
  -3.500   0.0261   0.00801   0.00189  -0.0886   0.7334   0.0462
  -3.250   0.0538   0.00792   0.00177  -0.0886   0.7252   0.0519
  -3.000   0.0817   0.00781   0.00166  -0.0886   0.7173   0.0593
  -2.750   0.1094   0.00770   0.00156  -0.0886   0.7103   0.0734
  -2.500   0.1373   0.00754   0.00146  -0.0886   0.7044   0.0934
  -2.250   0.1651   0.00740   0.00137  -0.0887   0.6981   0.1174
  -2.000   0.1927   0.00722   0.00129  -0.0887   0.6924   0.1570
  -1.750   0.2202   0.00702   0.00121  -0.0888   0.6849   0.2053
  -1.500   0.2476   0.00683   0.00114  -0.0888   0.6763   0.2582
  -1.250   0.2744   0.00658   0.00106  -0.0888   0.6667   0.3290
  -1.000   0.3011   0.00623   0.00101  -0.0888   0.6576   0.4405
  -0.750   0.3284   0.00611   0.00101  -0.0887   0.6487   0.4946
  -0.500   0.3560   0.00604   0.00102  -0.0887   0.6400   0.5364
  -0.250   0.3837   0.00598   0.00106  -0.0887   0.6323   0.5783
   0.000   0.4114   0.00600   0.00109  -0.0886   0.6229   0.5984
   0.250   0.4394   0.00603   0.00110  -0.0886   0.6130   0.6082
   0.750   0.4941   0.00618   0.00117  -0.0884   0.5814   0.6306
   1.000   0.5209   0.00629   0.00122  -0.0881   0.5617   0.6398
   1.250   0.5482   0.00639   0.00127  -0.0880   0.5454   0.6470
   1.500   0.5751   0.00651   0.00133  -0.0879   0.5263   0.6526
   1.750   0.6014   0.00667   0.00141  -0.0876   0.5032   0.6584
   2.250   0.6537   0.00704   0.00160  -0.0870   0.4560   0.6697
   2.500   0.6794   0.00726   0.00173  -0.0867   0.4303   0.6761
   2.750   0.7051   0.00747   0.00186  -0.0863   0.4058   0.6820
   3.000   0.7307   0.00769   0.00200  -0.0860   0.3828   0.6887
   3.250   0.7562   0.00792   0.00215  -0.0856   0.3594   0.6951
   3.500   0.7812   0.00817   0.00231  -0.0852   0.3330   0.7020
   4.000   0.8318   0.00863   0.00264  -0.0844   0.2936   0.7164
   4.500   0.8822   0.00906   0.00300  -0.0836   0.2620   0.7317
   4.750   0.9076   0.00927   0.00318  -0.0832   0.2487   0.7399
   5.000   0.9323   0.00950   0.00338  -0.0828   0.2336   0.7485
   5.250   0.9570   0.00973   0.00358  -0.0823   0.2194   0.7570
   5.500   0.9813   0.00998   0.00379  -0.0818   0.2045   0.7666
   5.750   1.0043   0.01030   0.00405  -0.0810   0.1847   0.7767
   6.000   1.0271   0.01063   0.00432  -0.0803   0.1653   0.7875
   6.250   1.0492   0.01098   0.00461  -0.0794   0.1469   0.7998
   6.500   1.0717   0.01128   0.00489  -0.0786   0.1327   0.8142
   6.750   1.0927   0.01163   0.00520  -0.0775   0.1154   0.8328
   7.000   1.1130   0.01193   0.00552  -0.0762   0.1009   0.8604
   7.250   1.1386   0.01214   0.00587  -0.0761   0.0863   1.0000
   7.500   1.1596   0.01257   0.00622  -0.0751   0.0736   1.0000
   7.750   1.1786   0.01312   0.00666  -0.0738   0.0574   1.0000
   8.000   1.1981   0.01361   0.00709  -0.0726   0.0461   1.0000
   8.250   1.2156   0.01421   0.00760  -0.0710   0.0328   1.0000
   8.500   1.2321   0.01482   0.00814  -0.0693   0.0217   1.0000
   8.750   1.2483   0.01532   0.00861  -0.0675   0.0163   1.0000
   9.000   1.2621   0.01591   0.00916  -0.0653   0.0100   1.0000
   9.250   1.2740   0.01662   0.00985  -0.0628   0.0041   1.0000
   9.500   1.2901   0.01711   0.01036  -0.0610   0.0035   1.0000
   9.750   1.3060   0.01761   0.01092  -0.0593   0.0033   1.0000
  10.000   1.3215   0.01815   0.01150  -0.0576   0.0031   1.0000
  10.250   1.3362   0.01874   0.01213  -0.0559   0.0029   1.0000
  10.500   1.3508   0.01935   0.01279  -0.0542   0.0028   1.0000
  10.750   1.3633   0.02011   0.01362  -0.0522   0.0025   1.0000
  11.000   1.3753   0.02092   0.01450  -0.0504   0.0024   1.0000
  11.250   1.3877   0.02172   0.01535  -0.0486   0.0023   1.0000
  11.500   1.4002   0.02254   0.01623  -0.0470   0.0023   1.0000
  11.750   1.4122   0.02341   0.01717  -0.0454   0.0022   1.0000
  12.000   1.4237   0.02434   0.01816  -0.0438   0.0022   1.0000
  12.250   1.4344   0.02535   0.01923  -0.0423   0.0021   1.0000
  12.500   1.4441   0.02646   0.02041  -0.0407   0.0021   1.0000
  12.750   1.4530   0.02768   0.02170  -0.0392   0.0019   1.0000
  13.000   1.4619   0.02892   0.02301  -0.0378   0.0019   1.0000
  13.250   1.4693   0.03033   0.02450  -0.0364   0.0018   1.0000
  13.500   1.4763   0.03182   0.02605  -0.0351   0.0018   1.0000
  13.750   1.4818   0.03348   0.02780  -0.0339   0.0017   1.0000
  14.000   1.4863   0.03529   0.02971  -0.0327   0.0017   1.0000
  14.250   1.4898   0.03725   0.03176  -0.0317   0.0017   1.0000
  14.500   1.4933   0.03928   0.03387  -0.0308   0.0016   1.0000
  14.750   1.4954   0.04152   0.03621  -0.0301   0.0016   1.0000
  15.000   1.4962   0.04399   0.03877  -0.0295   0.0016   1.0000
  15.250   1.4951   0.04678   0.04166  -0.0291   0.0015   1.0000
  15.500   1.4946   0.04961   0.04459  -0.0289   0.0015   1.0000
  15.750   1.4915   0.05289   0.04798  -0.0290   0.0015   1.0000
  16.000   1.4867   0.05654   0.05174  -0.0293   0.0014   1.0000
  16.250   1.4792   0.06073   0.05605  -0.0300   0.0015   1.0000
  16.500   1.4743   0.06473   0.06017  -0.0309   0.0014   1.0000
  16.750   1.4656   0.06951   0.06507  -0.0323   0.0014   1.0000
  17.000   1.4521   0.07523   0.07093  -0.0342   0.0014   1.0000
  17.250   1.4427   0.08056   0.07639  -0.0363   0.0014   1.0000
  17.500   1.4288   0.08690   0.08286  -0.0389   0.0014   1.0000
  17.750   1.4136   0.09367   0.08977  -0.0420   0.0014   1.0000
  18.000   1.3989   0.10059   0.09682  -0.0453   0.0014   1.0000
  18.250   1.3817   0.10818   0.10456  -0.0491   0.0014   1.0000
  18.500   1.3615   0.11655   0.11307  -0.0535   0.0014   1.0000
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