Return-Path: Received: from [65.33.87.205] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.1.3) with HTTP id 2576607 for lml@lancaironline.net; Thu, 11 Sep 2003 22:54:29 -0400 From: "Marvin Kaye" Subject: Re: Turbulator Tape To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.1.3 Date: Thu, 11 Sep 2003 22:54:29 -0400 Message-ID: In-Reply-To: <002301c378d2$032186e0$65e92844@brghtn01.mi.comcast.net> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Lloyd Dunlap" : I'm curious if anyone has applied turbulator tape to the bottom of their 320 / 360 wings like Dave Morss did to decrease parasitic drag. When I put some used oil on the wings to find the airflow separation point I don't seem to have any remarkable airflow patterns on the bottom of the wing that would indicate separation of the laminar flow. Am I missing something here ??? I sure did make a nice mess though ! Thanks in advance... Any comments or pictures Dave ?? Lloyd Dunlap N214MM