Return-Path: Received: from lanfear.nidlink.com ([216.18.128.7]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Thu, 9 Sep 1999 10:26:58 -0400 Received: from enaila.nidlink.com (root@enaila.nidlink.com [216.18.128.8]) by lanfear.nidlink.com (8.9.0/8.9.0) with ESMTP id HAA16368 for ; Thu, 9 Sep 1999 07:30:42 -0700 (PDT) Received: from regandesigns.com (tnt132-50.nidlink.com [216.18.132.50]) by enaila.nidlink.com (8.9.0/8.9.0) with ESMTP id HAA01364 for ; Thu, 9 Sep 1999 07:30:41 -0700 (PDT) Message-ID: <37D7C475.58909E05@regandesigns.com> Date: Thu, 09 Sep 1999 07:30:13 -0700 From: Brent Regan To: Lancair List Subject: Re Wing root fairing X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> According to the Orin at the factory, taping the gap between the wing root and the wing reduces the stall speed 5 to 10 Kts! Orin swears that this is good empirical data achieved by flying the same AC with and without the tape. When they tried this in Derek Hine's AC the improvement was less than 5 Kts. Derek's AC, Like mine, has a joggle at the wing to fairing interface so that there is a seam but no airflow across it. The joggle was formed by taping a 1 inch wide strip trimmed from the fairing flush with the end of the wing. The strip is covered in release tape and 4 bid x 2 inch is laid over it. The strip is removed, leaving the joggle with just the right depth for the fairing. To fit the fairing, install the "joggled" wings and trim the fairings. The foam bulkhead can be eliminated, except in the flap area, because the wing now supports the fairing. Leave a 2mm gap for the fuselage to expand during pressurization. Works for me ;) Brent Regan >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html