Return-Path: Received: from pop.centurytel.net ([209.142.136.253]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Mon, 8 Nov 1999 12:45:07 -0500 Received: from pavilion (ppp009.pa.centurytel.net [209.142.129.151]) by pop.centurytel.net (8.9.3/8.9.3) with SMTP id LAA29759 for ; Mon, 8 Nov 1999 11:49:22 -0600 (CST) Message-ID: <000201bf2a11$c5fa7780$97818ed1@pavilion> From: "J. N. Cameron" To: "Lancair List" Subject: Reflexing flaps Date: Mon, 8 Nov 1999 09:10:56 -0600 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> My understanding of the purpose of a "reflex" position for flaps is that it actually reduces the lift of the wing. Most wing/flap configurations have essentially two conditions: flaps up for normal airfoil, and flaps down for a higher-lift airfoil. The reflex gives you a "flaps farther up" position for a lower-lift airfoil, which is just another way of tweaking the airfoil's lift through a larger range of airspeeds. At high airspeed, you don't need as high a lift coefficient, and since lift brings drag with it, you get better performance by reducing both with a reflex flap position. In spam cans the increase in airspeed between stall and cruise is often only about 50 kts, which may be why nobody bothers with reflexed flaps on 172's. In the 360, the difference is maybe up to 150 kts, so some extra tweaking at the top range is worthwhile. The ideal, of course, would be flying machine with a continuously variable airfoil, optimized over the whole speed range. It's called a bird. Jim Cameron (once & future ES) >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>