Hi. . actually, for a given panel section it would be length in inches x .5 (root chord + tip chord). Or just ignore the .5 to get the sum of the area for both L & R panels combined. ----- Original Message ----- From: <[EMAIL PROTECTED]> To: <[EMAIL PROTECTED]> Sent: Tuesday, September 30, 2003 2:14 PM Subject: [RCSE] Wing area calculator
> 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. > 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.
