HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il)
HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL - DFVLR/Braunschweig Horstmann and Quast HQ-300 GD(MOD 2) sailplane airfoil
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(hq300gd2-il) HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL DFVLR/Braunschweig Horstmann and Quast HQ-300 GD(MOD 2) sailplane airfoil Max thickness 16.6% at 39.1% chord. Max camber 3.9% at 39.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL
49. 32.
0.0000000 0.0000000
0.0012684 0.0062908
0.0071875 0.0166469
0.0159428 0.0266338
0.0298655 0.0387292
0.0481690 0.0512466
0.0700870 0.0632883
0.0951833 0.0744954
0.1231304 0.0846863
0.1548681 0.0940678
0.1768614 0.0994577
0.1870348 0.1016806
0.1980554 0.1039082
0.2398947 0.1108535
0.2572032 0.1131073
0.2964495 0.1170439
0.3249072 0.1189502
0.3430856 0.1197665
0.3492295 0.1199706
0.3608384 0.1202585
0.3914933 0.1203863
0.3993033 0.1202716
0.4052784 0.1201437
0.4122175 0.1199504
0.4148237 0.1198652
0.4305371 0.1191998
0.4790006 0.1155416
0.5406950 0.1075875
0.5677551 0.1030819
0.5898949 0.0990158
0.5909140 0.0988215
0.5993221 0.0971942
0.6054170 0.0959893
0.6076642 0.0955399
0.6108516 0.0948971
0.6179766 0.0934389
0.6478070 0.0870481
0.6617652 0.0839256
0.6713626 0.0817400
0.6771104 0.0804160
0.8148217 0.0462144
0.8541776 0.0360241
0.8899908 0.0268184
0.9215463 0.0187888
0.9481668 0.0120468
0.9695556 0.0065983
0.9857564 0.0024113
0.9962803 -.0003555
1.0000000 -.0013460
0.0000000 0.0000000
0.0004619 -.0032567
0.0062400 -.0105398
0.0176007 -.0159931
0.0484967 -.0234371
0.0811471 -.0285380
0.0977626 -.0307187
0.1442271 -.0358762
0.1708338 -.0382802
0.1814613 -.0391320
0.2183401 -.0416010
0.2666845 -.0437942
0.2959121 -.0446292
0.3204255 -.0450896
0.3712958 -.0454632
0.4234485 -.0451358
0.4762438 -.0441000
0.5290216 -.0422683
0.5811418 -.0394719
0.6319972 -.0355414
0.6986371 -.0281713
0.7128459 -.0262376
0.7499000 -.0206165
0.7744281 -.0165489
0.8193740 -.0089005
0.8622946 -.0022884
0.9017916 0.0019954
0.9363069 0.0031838
0.9642510 0.0015728
0.9843190 -.0013976
0.9961277 -.0039486
1.0000000 -.0049210
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Polars for HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| hq300gd2-il | 50,000 | 9 | 5.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq300gd2-il | 50,000 | 5 | 15.1 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq300gd2-il | 100,000 | 9 | 42.8 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq300gd2-il | 100,000 | 5 | 44.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq300gd2-il | 200,000 | 9 | 74.7 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq300gd2-il | 200,000 | 5 | 73.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq300gd2-il | 500,000 | 9 | 107.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq300gd2-il | 500,000 | 5 | 107.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq300gd2-il | 1,000,000 | 9 | 139.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq300gd2-il | 1,000,000 | 5 | 131.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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