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)) 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.
