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