Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5b3) with ESMTP id 857355 for rob@logan.com; Sun, 26 Aug 2001 11:14:58 -0400 Received: from robin.mail.pas.earthlink.net ([207.217.120.65]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Sun, 26 Aug 2001 10:14:28 -0400 Received: from [209.86.49.113] (user-38lccbh.dialup.mindspring.com [209.86.49.113]) by robin.mail.pas.earthlink.net (8.11.5/8.9.3) with SMTP id f7QEP1o03515 for ; Sun, 26 Aug 2001 07:25:02 -0700 (PDT) Message-Id: <200108261425.f7QEP1o03515@robin.mail.pas.earthlink.net> Subject: Re: L/D Max Date: Sun, 26 Aug 2001 09:25:02 -0500 From: Dane & Cindy White To: "Lancair List" Mime-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> > Determining maximum range would >require graphing fuel burn against airspeed, and somewhere along that curve >you'd find the best speed to fly to go the farthest based on available fuel. > > ] Marv, You are correct about using a graph of fuel burn versus airspeed to determine the speed to fly for max range or endurance. Recall from aerodynamics that if you plot total drag (thrust required for level, unaccelerated flight) versus angle of attack, you get a "U" shaped curve. The bottom of that curve defines the angle of attack for minimum drag - along with a corresponding airspeed at a given weight. This defines the angle of attack and airspeed (for a given weight) for maximum endurance since this is the minimum thrust required for level flight. A line drawn tangent from the graph's origin to the same total drag curve defines the angle of attack and total drag for max L/D. Obviously, this will be a faster airspeed, at a lower AOA, with more total drag, but you'll maximize your air range flown. Once you've determined the angles-of-attack for max L/D and min drag you're done. These angles don't change unless you change the configuration (lower flaps or gear). The airspeed to achieve these AOA's changes with weight. So in addition to avoiding aerodynamic stalls, an AOA gauge can help you quickly determine the airspeed to fly for maximum performance. Disclaimer: This discussion ignores the effects of changes in efficiency with airspeed changes of piston powered aircraft. Dane White Lancair IV-P Murfreesboro TN {Thanks for the backup, Dane. My point in trying to respond to Fili's post about max range vs endurance, is that endurance is a measure of time, without regard to distance. Range adds distance to the equation and is a separate issue. The two are not necessarily the same in the context of an AOA discussion. ] >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>