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HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il)
Reynolds number: 200,000
Max Cl/Cd: 73.5 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq300gd2-il-200000-n5.txt
Download as CSV file: xf-hq300gd2-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.3029   0.09243   0.08855  -0.0665   0.8420   0.0191
 -10.750  -0.3876   0.06311   0.05908  -0.0877   0.8373   0.0177
 -10.500  -0.4331   0.05328   0.04884  -0.0931   0.8273   0.0175
 -10.250  -0.4500   0.04888   0.04417  -0.0940   0.8174   0.0176
 -10.000  -0.4602   0.04574   0.04077  -0.0936   0.8091   0.0177
  -9.750  -0.4589   0.04300   0.03780  -0.0939   0.8010   0.0179
  -9.500  -0.4527   0.04058   0.03512  -0.0938   0.7946   0.0181
  -9.250  -0.4419   0.03841   0.03271  -0.0938   0.7879   0.0185
  -9.000  -0.4293   0.03618   0.03020  -0.0936   0.7816   0.0189
  -8.750  -0.4142   0.03407   0.02776  -0.0935   0.7761   0.0197
  -8.500  -0.3988   0.03125   0.02446  -0.0933   0.7698   0.0209
  -8.250  -0.3804   0.02863   0.02124  -0.0929   0.7645   0.0217
  -8.000  -0.3585   0.02696   0.01937  -0.0928   0.7600   0.0223
  -7.750  -0.3346   0.02584   0.01812  -0.0930   0.7545   0.0229
  -7.500  -0.3101   0.02478   0.01689  -0.0930   0.7495   0.0236
  -7.250  -0.2850   0.02380   0.01571  -0.0930   0.7452   0.0246
  -7.000  -0.2592   0.02289   0.01460  -0.0930   0.7400   0.0261
  -6.750  -0.2333   0.02197   0.01345  -0.0929   0.7351   0.0272
  -6.500  -0.2081   0.02099   0.01244  -0.0928   0.7311   0.0281
  -6.250  -0.1821   0.02030   0.01168  -0.0928   0.7273   0.0291
  -6.000  -0.1558   0.01968   0.01101  -0.0929   0.7225   0.0304
  -5.750  -0.1292   0.01914   0.01037  -0.0930   0.7181   0.0323
  -5.500  -0.1025   0.01861   0.00971  -0.0930   0.7143   0.0336
  -5.250  -0.0765   0.01789   0.00900  -0.0931   0.7104   0.0351
  -5.000  -0.0495   0.01739   0.00850  -0.0934   0.7062   0.0367
  -4.750  -0.0218   0.01698   0.00804  -0.0938   0.7023   0.0392
  -4.500   0.0063   0.01658   0.00756  -0.0942   0.6988   0.0418
  -4.250   0.0346   0.01613   0.00708  -0.0949   0.6953   0.0448
  -4.000   0.0635   0.01579   0.00670  -0.0955   0.6911   0.0488
  -3.750   0.0928   0.01544   0.00634  -0.0963   0.6873   0.0552
  -3.500   0.1224   0.01511   0.00600  -0.0971   0.6841   0.0666
  -3.250   0.1525   0.01475   0.00567  -0.0980   0.6811   0.0909
  -3.000   0.1856   0.01347   0.00530  -0.1010   0.6774   0.3019
  -2.750   0.2189   0.01231   0.00534  -0.1034   0.6735   0.5783
  -2.500   0.2383   0.01259   0.00596  -0.1007   0.6701   0.6812
  -2.250   0.2628   0.01299   0.00634  -0.0993   0.6672   0.7200
  -2.000   0.2911   0.01335   0.00658  -0.0991   0.6644   0.7446
  -1.750   0.3156   0.01376   0.00697  -0.0979   0.6605   0.7607
  -1.500   0.3382   0.01409   0.00727  -0.0963   0.6568   0.7683
  -1.250   0.3707   0.01414   0.00720  -0.0976   0.6536   0.7760
  -1.000   0.3960   0.01429   0.00728  -0.0968   0.6507   0.7792
  -0.750   0.4226   0.01444   0.00736  -0.0964   0.6478   0.7834
  -0.500   0.4525   0.01454   0.00742  -0.0972   0.6439   0.7898
  -0.250   0.4794   0.01467   0.00752  -0.0970   0.6404   0.7945
   0.000   0.5045   0.01481   0.00761  -0.0963   0.6371   0.7984
   0.250   0.5332   0.01490   0.00763  -0.0965   0.6342   0.8029
   0.500   0.5664   0.01496   0.00763  -0.0982   0.6309   0.8080
   0.750   0.5922   0.01505   0.00773  -0.0978   0.6270   0.8101
   1.000   0.6190   0.01512   0.00778  -0.0977   0.6233   0.8124
   1.250   0.6470   0.01518   0.00781  -0.0979   0.6200   0.8149
   1.500   0.6766   0.01524   0.00780  -0.0985   0.6170   0.8177
   1.750   0.7063   0.01531   0.00791  -0.0993   0.6124   0.8207
   2.000   0.7387   0.01536   0.00794  -0.1008   0.6079   0.8240
   2.250   0.7658   0.01540   0.00796  -0.1008   0.6039   0.8256
   2.500   0.7929   0.01546   0.00801  -0.1008   0.5998   0.8274
   2.750   0.8195   0.01554   0.00814  -0.1008   0.5946   0.8295
   3.000   0.8477   0.01560   0.00820  -0.1011   0.5899   0.8317
   3.250   0.8775   0.01564   0.00819  -0.1018   0.5860   0.8339
   3.500   0.9061   0.01575   0.00838  -0.1024   0.5803   0.8365
   3.750   0.9368   0.01584   0.00849  -0.1035   0.5752   0.8391
   4.000   0.9656   0.01589   0.00851  -0.1039   0.5709   0.8408
   4.250   0.9912   0.01600   0.00871  -0.1038   0.5652   0.8423
   4.500   1.0173   0.01609   0.00886  -0.1037   0.5596   0.8442
   4.750   1.0449   0.01616   0.00891  -0.1039   0.5549   0.8462
   5.000   1.0713   0.01630   0.00915  -0.1041   0.5483   0.8482
   5.250   1.0993   0.01640   0.00929  -0.1045   0.5422   0.8502
   5.500   1.1274   0.01653   0.00947  -0.1050   0.5356   0.8523
   5.750   1.1560   0.01667   0.00966  -0.1057   0.5281   0.8547
   6.000   1.1811   0.01679   0.00984  -0.1055   0.5208   0.8564
   6.250   1.2051   0.01693   0.01004  -0.1051   0.5124   0.8580
   6.500   1.2294   0.01709   0.01026  -0.1048   0.5037   0.8597
   6.750   1.2537   0.01725   0.01046  -0.1045   0.4943   0.8614
   7.000   1.2771   0.01747   0.01076  -0.1041   0.4833   0.8636
   7.250   1.3005   0.01772   0.01105  -0.1038   0.4718   0.8660
   7.500   1.3237   0.01801   0.01136  -0.1035   0.4591   0.8682
   7.750   1.3458   0.01835   0.01173  -0.1031   0.4452   0.8702
   8.000   1.3631   0.01872   0.01211  -0.1016   0.4307   0.8718
   8.250   1.3788   0.01916   0.01256  -0.1000   0.4154   0.8737
   8.500   1.3922   0.01969   0.01310  -0.0980   0.4000   0.8760
   8.750   1.4015   0.02031   0.01372  -0.0955   0.3849   0.8788
   9.000   1.4131   0.02111   0.01451  -0.0937   0.3695   0.8813
   9.250   1.4247   0.02205   0.01544  -0.0921   0.3541   0.8836
   9.500   1.4336   0.02309   0.01648  -0.0903   0.3398   0.8856
  10.000   1.4484   0.02545   0.01888  -0.0865   0.3126   0.8900
  10.250   1.4556   0.02680   0.02027  -0.0850   0.2993   0.8927
  10.500   1.4623   0.02831   0.02179  -0.0836   0.2859   0.8952
  10.750   1.4674   0.03005   0.02353  -0.0823   0.2712   0.8974
  11.000   1.4699   0.03198   0.02545  -0.0809   0.2554   0.8994
  11.250   1.4702   0.03405   0.02751  -0.0792   0.2392   0.9013
  11.500   1.4699   0.03627   0.02971  -0.0778   0.2233   0.9034
  11.750   1.4700   0.03856   0.03198  -0.0765   0.2081   0.9057
  12.000   1.4706   0.04088   0.03431  -0.0754   0.1940   0.9082
  12.250   1.4714   0.04327   0.03671  -0.0744   0.1805   0.9105
  12.500   1.4723   0.04574   0.03918  -0.0736   0.1678   0.9125
  12.750   1.4721   0.04822   0.04168  -0.0726   0.1560   0.9143
  13.000   1.4717   0.05081   0.04429  -0.0718   0.1446   0.9163
  13.250   1.4707   0.05358   0.04706  -0.0710   0.1334   0.9183
  13.500   1.4691   0.05650   0.04999  -0.0704   0.1222   0.9204
  13.750   1.4682   0.05942   0.05293  -0.0700   0.1109   0.9225
  14.000   1.4670   0.06248   0.05602  -0.0696   0.1002   0.9247
  14.250   1.4642   0.06562   0.05918  -0.0692   0.0897   0.9270
  14.500   1.4605   0.06890   0.06248  -0.0688   0.0799   0.9294
  14.750   1.4561   0.07239   0.06599  -0.0685   0.0705   0.9318
  15.000   1.4510   0.07606   0.06967  -0.0685   0.0618   0.9342
  15.500   1.4414   0.08361   0.07730  -0.0687   0.0475   0.9386
  15.750   1.4357   0.08745   0.08120  -0.0689   0.0424   0.9411
  16.000   1.4292   0.09152   0.08532  -0.0692   0.0382   0.9438
  16.250   1.4242   0.09549   0.08939  -0.0697   0.0347   0.9468
  16.500   1.4177   0.09975   0.09372  -0.0703   0.0319   0.9500
  16.750   1.4114   0.10392   0.09799  -0.0710   0.0297   0.9541
  17.000   1.4059   0.10800   0.10220  -0.0718   0.0277   0.9599
  17.250   1.3982   0.11234   0.10664  -0.0727   0.0262   0.9711
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