HS1 family of prop airfoils
HS1712 Airfoil (x,y) Co-ordinates
| 0 | 0.00001 |
| 0.0005 | 0.0043 |
| 0.001 | 0.006 |
| 0.002 | 0.00903 |
| 0.003 | 0.01127 |
| 0.005 | 0.0149 |
| 0.0075 | 0.01861 |
| 0.01 | 0.0218 |
| 0.02 | 0.03186 |
| 0.03 | 0.03967 |
| 0.04 | 0.04688 |
| 0.05 | 0.05192 |
| 0.06 | 0.05698 |
| 0.07 | 0.0611 |
| 0.08 | 0.06562 |
| 0.09 | 0.06937 |
| 0.1 | 0.0728 |
| 0.12 | 0.07886 |
| 0.14 | 0.08401 |
| 0.16 | 0.08839 |
| 0.18 | 0.09211 |
| 0.2 | 0.09525 |
| 0.22 | 0.09786 |
| 0.24 | 0.1 |
| 0.26 | 0.10173 |
| 0.28 | 0.10313 |
| 0.3 | 0.10418 |
| 0.34 | 0.10542 |
| 0.36 | 0.10632 |
| 0.38 | 0.10687 |
| 0.4 | 0.107 |
| 0.44 | 0.10656 |
| 0.46 | 0.106 |
| 0.48 | 0.10526 |
| 0.5 | 0.10423 |
| 0.54 | 0.10154 |
| 0.56 | 0.09965 |
| 0.58 | 0.09795 |
| 0.6 | 0.09587 |
| 0.64 | 0.09125 |
| 0.66 | 0.08872 |
| 0.68 | 0.08605 |
| 0.7 | 0.08322 |
| 0.74 | 0.07789 |
| 0.76 | 0.07477 |
| 0.78 | 0.07028 |
| 0.8 | 0.06668 |
| 0.82 | 0.06262 |
| 0.84 | 0.05834 |
| 0.86 | 0.05368 |
| 0.88 | 0.04856 |
| 0.9 | 0.04299 |
| 0.91 | 0.03997 |
| 0.92 | 0.03686 |
| 0.93 | 0.03364 |
| 0.94 | 0.03032 |
| 0.95 | 0.02689 |
| 0.96 | 0.02335 |
| 0.97 | 0.01968 |
| 0.98 | 0.0157 |
| 0.99 | 0.01171 |
| 1 | 0.0072 |
| 1 | -0.0107 |
| 0.99 | -0.00976 |
| 0.98 | -0.00882 |
| 0.97 | -0.00829 |
| 0.96 | -0.00807 |
| 0.95 | -0.00785 |
| 0.94 | -0.00753 |
| 0.93 | -0.00742 |
| 0.92 | -0.00721 |
| 0.91 | -0.00701 |
| 0.9 | -0.00683 |
| 0.88 | -0.00653 |
| 0.86 | -0.00633 |
| 0.84 | -0.00621 |
| 0.82 | -0.00614 |
| 0.8 | -0.00611 |
| 0.78 | -0.00609 |
| 0.76 | -0.00611 |
| 0.74 | -0.00619 |
| 0.7 | -0.00658 |
| 0.68 | -0.00687 |
| 0.66 | -0.00721 |
| 0.64 | -0.00756 |
| 0.6 | -0.00824 |
| 0.58 | -0.00856 |
| 0.56 | -0.00888 |
| 0.54 | -0.00919 |
| 0.5 | -0.00985 |
| 0.48 | -0.0102 |
| 0.46 | -0.0106 |
| 0.44 | -0.01105 |
| 0.4 | -0.01216 |
| 0.38 | -0.01279 |
| 0.36 | -0.01344 |
| 0.34 | -0.01389 |
| 0.3 | -0.01536 |
| 0.28 | -0.01607 |
| 0.26 | -0.01688 |
| 0.24 | -0.01786 |
| 0.22 | -0.01901 |
| 0.2 | -0.0203 |
| 0.18 | -0.02159 |
| 0.16 | -0.02279 |
| 0.14 | -0.02374 |
| 0.12 | -0.0244 |
| 0.1 | -0.02469 |
| 0.09 | -0.02466 |
| 0.08 | -0.0245 |
| 0.07 | -0.02417 |
| 0.06 | -0.02353 |
| 0.05 | -0.02283 |
| 0.04 | -0.02109 |
| 0.03 | -0.02006 |
| 0.02 | -0.01767 |
| 0.01 | -0.01376 |
| 0.0075 | -0.0123 |
| 0.005 | -0.01044 |
| 0.003 | -0.00842 |
| 0.002 | -0.00709 |
| 0.001 | -0.00519 |
| 0.0005 | -0.00377 |
| 0 | 0 |
HS1712 Airfoil CAD files