Return-Path: Sender: (Marvin Kaye) To: lml Date: Fri, 12 Sep 2003 13:01:03 -0400 Message-ID: X-Original-Return-Path: Received: from www.dynacomm.ws ([198.22.63.66] verified) by logan.com (CommuniGate Pro SMTP 4.1.3) with ESMTP id 2577206 for lml@lancaironline.net; Fri, 12 Sep 2003 12:36:15 -0400 Received: from dynacomm.ws (adsl-68-248-37-218.dsl.sfldmi.ameritech.net [68.248.37.218]) by www.dynacomm.ws (8.10.2/8.10.2) with ESMTP id h8CGaBN31453; Fri, 12 Sep 2003 12:36:11 -0400 X-Original-Date: Fri, 12 Sep 2003 12:36:10 -0400 Subject: Re: Turbulator Tape Content-Type: text/plain; charset=US-ASCII; format=flowed Mime-Version: 1.0 (Apple Message framework v552) X-Original-Cc: Lloyd Dunlap X-Original-To: Lancair List From: "Lorn H. Olsen" Content-Transfer-Encoding: 7bit X-Original-Message-Id: <373CAD8A-E53F-11D7-B9BD-000393C2C1A6@dynacomm.ws> X-Mailer: Apple Mail (2.552) > 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 ! > > Lloyd Dunlap > N214MM Lloyd, I always thought that the laminar flow separation occurs on the top of the wing. Why are you checking the bottom? Someone please correct me and the "Aerodynamics for Navel Aviators" manual, if I am wrong. -- Lorn H. 'Feathers' Olsen, MAA, DynaComm, Corp. 248-478-4301, mailto:lorn@dynacomm.ws LNC2, O-320-D1F, N31161, Y47, SE Michigan