Return-Path: Received: from [65.33.162.138] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.1.8) with HTTP id 2782689 for lml@lancaironline.net; Wed, 03 Dec 2003 21:47:59 -0500 From: "Marvin Kaye" Subject: Re: [LML] Re: Vortex Generators To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.1.8 Date: Wed, 03 Dec 2003 21:47:59 -0500 Message-ID: In-Reply-To: <003601c3ba0c$f8990e60$4f00a8c0@paul> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Paul Nafziger" : Vortex generators create turbulent boundary layer flow, essentially adding energy to the boundary layer. This does indeed re-attach flow if it separates, or rather prevent the flow from separating in the first place. Also, they do indeed ruin the laminar flow we all strive to attain. Also, imparting that energy to the boundary layer comes at a cost, which is increased drag under normal conditions. (When flow is separated, it's another story). Hence my question, why are we interested in doing that to these high performance airplanes? I understand that you can lower your stall speed, but who wants to do that at the expense of decreased performance? Naf Paul Nafziger LNC2 N7PN > It would seem that the generators would ruin the laminar flow > at reduced angles of attack, as in cruise?