![]() SA were part of a low Reynolds number airfoil study Wrapping wings, so as hard as one might try it is only possible toĪpproximate the 1903 Wright Flyer wing section with a single Keep in mind this aircraft had deformable fabric-covered He has done considerable research on the topic andīelieves that this airfoil is very close to the 1903 Wright FlyerĪirfoil. ![]() Report 93 it does not say so explicitly? I don't know however, IĪm labeling it as such based on communications with Prof Fred CulickĪt Caltech. How do I "know" this is the 1903 Wright Flyer even though in NACA Original backers of the Blackhawk project: Ray Olsen, Don Scegiel,īlackhawk vintage advertising: 020522-blackhawk.pdf Sections, and on 12/6/02 they were made public. These airfoils started life as proprietary Selig airfoils used on the carbon Blackhawk 113.5-inch span (openĬlass) RC sailplane (designed by Selig around ~1991). The Opus was available from (Northeast Sailplane Products): 021206-opus.pdf Life as proprietary sections, and on 12/6/02 they were made public. Sailplane (designed by Selig around ~1991). Selig airfoils used on the Opus 100 inch span (standard class) RC Replacements for the usual HT1x tail surface airfoils. Trim flap range is -1 deg (speed) to +4 deg (float). Longer laminar runs at the large Re ~ 600K, typical of an F3B speed run. Basically lower-camber versions of the AG40-43 which were aimed at F3J and TD. Some of these airfoils were designed for Mike Lachowski for his F3B competition RC sailplane designs. Sohn Verlagsgesellschaft mbH (publisher) Braunschweig/Weisbaden, Althaus, D., "Niedriggeschwindigkeitsprofile," Friedr. "Design of Low-Reynolds Number Airfoils - II," AIAA PaperĨ8-3764-CP, AIAA 6th Applied Aerodynamics Conference, Williamsburg, Pfenninger, W., Vemuru, C.S., Mangalam, S.M., and Evangelista, R., Pfenninger, W., and Vemuru, C.S., "Design of Low-Reynolds NumberĪirfoils - I," AIAA Paper 88-2572-CP, AIAA 6th AppliedĪerodynamics Conference, Williamsburg, VA, June 6-8, 1988, Performance Low-Reynolds Number Airfoil," AIAA Paper 84-0628, and Pfenninger, W., "Wind-Tunnel Tests on a High
0 Comments
Leave a Reply. |
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |