Citazione:
Originalmente inviato da Ehstìkatzi  Avevo trovato questo
....
Through the use of carbon fiber and epoxy resin
construction materials, Wilhelm was able to use
one of the newest German HQ airfoil that is remarkably thin in its profile. Our actual thicknessto-chord ratio measurements showed .1293 at the
flap roots and about .1283 average over the remainder of the wing panels. As is common these
days, the airfoil coordinates are proprietary and, therefore,
unavailable to the public in general.
The airfoil is reportedly designed to require turgulator strips on both its upper and lower surfaces to prevent formation of high drag separation bubbles at the aft ends
of its extensive low drag laminar flow regions. Our measurements showed that the factory installed .50 mm (.020 in.)
thick zig-zag boundary layer control tape was positioned at
.82 chord aft of the leading edges on the wing bottom surfaces and at .68 chord aft of the leading edges on the wing
top surfaces and at .68 chord aft of the leading edges on the
wing to surfaces. |
le coordinate del profilo alare sono proprietarie e, quindi,
non disponibili al pubblico in generale.......sara' difficile trovarle
