Designed for pylon racing model aircraft (FAI class F3D)
Image (7 kBytes)
Image (8 kBytes)x y 1.00000000 0.00000000 0.99663722 -0.00000502 0.98661979 0.00015827 0.97016021 0.00083998 0.94762865 0.00232279 0.91954306 0.00478393 0.88649448 0.00827457 0.84911235 0.01276792 0.80805809 0.01815911 0.76400822 0.02428373 0.71763596 0.03091656 0.66960153 0.03779462 0.62054465 0.04463611 0.57116423 0.05108921 0.52197689 0.05654881 0.47303495 0.06058278 0.42440107 0.06327690 0.37650891 0.06484632 0.32990396 0.06532833 0.28507654 0.06470811 0.24245961 0.06294654 0.20241194 0.06004635 0.16525807 0.05604350 0.13126736 0.05103062 0.10070840 0.04515568 0.07383715 0.03858238 0.05087461 0.03148085 0.03197380 0.02406597 0.01728446 0.01663089 0.00695149 0.00951360 0.00230137 0.00483181 0.00108635 0.00304916 0.00030031 0.00141854 0.00003307 0.00043894 0.00003397 -0.00041277 0.00037497 -0.00121038 0.00103088 -0.00204638 0.00246899 -0.00334802 0.00439569 -0.00470397 0.00659525 -0.00600849 0.01770495 -0.01053427 0.03378029 -0.01462203 0.05477004 -0.01806289 0.08059598 -0.02079484 0.11108204 -0.02281900 0.14599903 -0.02417183 0.18503357 -0.02493978 0.22778877 -0.02522602 0.27377743 -0.02513931 0.32245228 -0.02476081 0.37320774 -0.02415208 0.42543910 -0.02331965 0.47854562 -0.02229529 0.53191756 -0.02109606 0.58494209 -0.01975863 0.63701018 -0.01829908 0.68752329 -0.01675217 0.73589960 -0.01513154 0.78158078 -0.01346836 0.82403743 -0.01177234 0.86277561 -0.01006936 0.89734096 -0.00836027 0.92732470 -0.00666124 0.95236187 -0.00491317 0.97233203 -0.00304938 0.98724618 -0.00134670 0.99671459 -0.00030431 1.00000000 0.00000000This airfoil has originally been published in [4].
Last modification of this page: 04.10.04
[Back to Home Page] Suggestions? Corrections? Remarks? e-mail: Martin Hepperle.
Due to the increasing amount of SPAM mail, I have to change this e-Mail address regularly. You will always find the latest version in the footer of all my pages.
It might take some time until you receive an
answer and in some cases you may even receive no answer at all. I apologize for
this, but my spare time is limited. If you have not lost patience, you might
want to send me a copy of your e-mail after a month or so.
This is a privately owned, non-profit page of purely educational
purpose. Any statements may be incorrect and unsuitable for practical usage. I
cannot take any responsibility for actions you perform based on data,
assumptions, calculations etc. taken from this web page.
© 1996-2005 Martin Hepperle
You may use the data given in this document for your personal use. If you use
this document for a publication, you have to cite the source. A publication of a
recompilation of the given material is not allowed, if the resulting product is
sold for more than the production costs.
This document may accidentally refer to trade names and trademarks, which are owned by national or international companies, but which are unknown by me. Their rights are fully recognized and these companies are kindly asked to inform me if they do not wish their names to be used at all or to be used in a different way.
This document is part of a frame set and can be found by navigating from the entry point at the Web site http://www.MH-AeroTools.de/.