> Date: Tue, 30 Sep 2003 14:14:48 -0700 > From: [EMAIL PROTECTED] > To: [EMAIL PROTECTED] > Subject: Wing area calculator > Message-ID: <[EMAIL PROTECTED]> > > I used to have a link to a page that would calculate the area of wing > panels, but can't find it anymore. Anyone have a URL? > > Barring that, in figuring out the area of a single wing panel, with a > tapered leading edge and straight trailing edge, is the following formula > correct? .5 * (panel span * (root chord + tip chord)) > Check out this site, it has a wing area calculator on the download section if you have Windows9x / NT application. It also have a lot of other interesting subjects. http://www.mh-aerotools.de/airfoils/index.htm Cato Hansen. RCSE-List facilities provided by Model Airplane News. Send "subscribe" and "unsubscribe" requests to [EMAIL PROTECTED] Please note that subscribe and unsubscribe messages must be sent in text only format with MIME turned off.
