Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.2 9/18/84; site dataio.UUCP Path: utzoo!watmath!clyde!burl!ulysses!mhuxr!mhuxt!houxm!mtuxo!mtunh!mtung!mtunf!ariel!vax135!cornell!uw-beaver!uw-june!entropy!dataio!dbp From: dbp@dataio.UUCP (Dave Pellerin) Newsgroups: net.aviation Subject: Re: Acrobatics (Really How Things Fly) Message-ID: <726@dataio.UUCP> Date: Tue, 23-Jul-85 10:24:02 EDT Article-I.D.: dataio.726 Posted: Tue Jul 23 10:24:02 1985 Date-Received: Thu, 25-Jul-85 21:53:37 EDT Reply-To: dbp@dataio.UUCP (Dave Pellerin) Distribution: net Organization: The Boneless Chicken Farm Lines: 28 Keywords: Say What?? > >>2) ....describing the differential airflow... how this creates lift. >>OK; so how does a plane fly inverted? ... >>Will Martin >> >Common misconception, differential airflow causes lift. Basic laws of >physics will tell you "action = reaction" Lift is caused by the acceleration >of a mass of air downward, period. The airfoil is just an efficient way >of doing this. A lot of aerobatic planes have symetrical wings with zero >dihedral and get lift purely from angle of attack. Hope this helps. > Tom ihnp4!cbnap!tel Sorry, lift is created by two factors; increased air velocity over the upper surface, and the so-called "action = reaction" lift. The first factor accounts for (in normal aircraft) about 80% of the lift produced. "Action = reaction", where air is deflected downward, accounts for only 20% of the total. If Newton's law were the only factor, the perfect airfoil would probably be a flat plate! Most asymetrical airfoils will produce a significant amount of lift at slightly negative angles of attack. A "symetrical" airfoil becomes quite asymetrical with a little angle of attack. Dihedral has little or no affect on lift, it only provides yaw stability. Dave Pellerin ..uw-beaver!entropy!dataio!dbp