Return-Path: Received: from imo12.mx.aol.com ([198.81.17.2]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Fri, 1 Oct 1999 01:08:19 -0400 Received: from Fredmoreno@aol.com by imo12.mx.aol.com (mail_out_v22.4.) id kNVCa08594 (4254) for ; Fri, 1 Oct 1999 01:12:12 -0400 (EDT) From: Fredmoreno@aol.com Message-ID: <70222a88.25259cab@aol.com> Date: Fri, 1 Oct 1999 01:12:11 EDT Subject: NACA inlet lip To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I have a chart from a technical paper describing the preferred shape for the NACA duct. The lip of the NACA duct should not be sharp, but should have a rounded cross section somewhat like a semi-ellipse with a leading edge radius that is 9.4% of the duct depth at the edge location. The total thickness of the lip is 48% of the duct duct height (seems a lot but true). For the example presented, the inlet is 1 inch high by 4 inches wide under the lip, and the lip is 0.48 thick so that the floor of the duct is 1.48 below the outer fuselage surface. You seldom see such thick lips at Oshkosh, but then most of these ducts do not comply with the recommended guidelines. I sanded a piece of foam to the duct width, made it 1/8 inch thick, radiused the leading edge, and then tapered it to zero thickness about 2 inches aft of the leading edge. I wrapped this with light weight fiber glass, trimmed and sanded, and then bonded into the inside of the NACA duct to make the lip which I then blended in with micro. It strengthens the vertical wall, improved pressure recovery, and I believe probably reduces the noise significantly. Fred >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html