Return-Path: Received: from imo27.mx.aol.com ([198.81.17.71]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Thu, 9 Sep 1999 12:26:59 -0400 Received: from Fredmoreno@aol.com by imo27.mx.aol.com (mail_out_v22.4.) id zWNUa01404 (4264); Thu, 9 Sep 1999 12:30:20 -0400 (EDT) From: Fredmoreno@aol.com Message-ID: Date: Thu, 9 Sep 1999 12:30:20 EDT Subject: Tape gaps on Lancair 2 place? To: wrumburg@cdicorp.com, lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Bill: Responding to your question about tape on the 2 place Lancairs: You are probably OK on the 2 place with the tape. It is the higher true air speed, and particularly the rain that causes the problems on the 4 place. My recollection on droplet damage is that it goes with the fourth or fifth power of velocity once a threshold limit is exceeded. Thus once one crosses the threshold level (don't know what it is -- probably depends on surface, curvature, etc.) small increases in true air speed (not IAS) cause big increases in damage rate. On thinking about it a bit more, it seems that if you were to use the polyurethane leading edge tape trimmed to appropriate width, it should be OK. It is tough stuff, and speeds are probably low enough not to be a problem. On Brent Regan's Lancair IV, he applied an adhesively backed anti skid layer on the top of the wing outside of the cockpit. We flew through some clouds when trying to set the SFO to DEN record, and when we landed, there was no anti-skid pad left, just a thin layer of adhesive. Otherwise it was completely gone. We climbed out of the cockpit and promptly stuck to the wing. Others have told me that rain punches through the tape over gaps on the leading edge and then the tape peels back. Rain and droplets are the big enemy. The polyurethane tape is probably tough enough to withstand rain if the gap is not too great. I think Don is right: limited drag effect on the 2 place particularly at cruise. The bad news is at lower speed when the leakage through the gap becomes greater at greater angles of attack. The Lancair IV is more sensitive because the flow at the wing fuselage intersection is very complicated (on all airplanes, particularly at high angles of attack) and easily disrupted. And this location is frequently the origination point of stall (separated flow). I say go with the tape, and you will probably be fine. Watch out for the rain. But if the rain takes it off, so what? Put on more tape! Fred >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html