Return-Path: <marv@lancaironline.net>
Received: from [65.33.165.101] (account marv@lancaironline.net)
  by logan.com (CommuniGate Pro WebUser 4.1.3)
  with HTTP id 2578127 for lml@lancaironline.net; Sat, 13 Sep 2003 09:59:52 -0400
From: "Marvin Kaye" <marv@lancaironline.net>
Subject: Re: [LML] Re: Turbulator Tape
To: lml
X-Mailer: CommuniGate Pro WebUser Interface v.4.1.3
Date: Sat, 13 Sep 2003 09:59:52 -0400
Message-ID: <web-2578127@logan.com>
In-Reply-To: <sf626cf2.047@asdmngwia.mpls.udlp.com>
MIME-Version: 1.0
Content-Type: text/plain; charset="ISO-8859-1"; format="flowed"
Content-Transfer-Encoding: 8bit

Posted for "Christopher Zavatson" <Christopher.Zavatson@udlp.com>:

<<I always thought that the laminar flow separation occurs on the top of

the wing.>>
At low angles of attack NLF airfoils can develop flow seperation on the
bottom of the section. (Cruise condition at high speed) -Flow seperation
on the top occurs at high angles of attack.

Chris Zavatson
N91CZ
L360 std

Christopher Zavatson
Mobility Technologies
United Defense
(408)289-4329