Return-Path: Sender: (Marvin Kaye) To: lml Date: Mon, 09 Dec 2002 16:44:23 -0500 Message-ID: X-Original-Return-Path: Received: from [32.97.166.32] (HELO prserv.net) by logan.com (CommuniGate Pro SMTP 4.0.2) with ESMTP id 1898205 for lml@lancaironline.net; Mon, 09 Dec 2002 16:07:56 -0500 Received: from oemcomputer (slip-12-65-217-221.mis.prserv.net[12.65.217.221]) by prserv.net (out2) with SMTP id <2002120921074820206bjklpe>; Mon, 9 Dec 2002 21:07:48 +0000 From: "Larry Henney" X-Original-To: "'Lancair Mailing List'" Subject: RE: [LML] aileron balancing X-Original-Date: Mon, 9 Dec 2002 14:54:16 -0600 X-Original-Message-ID: <000201c29fc5$24363060$ddd9410c@oemcomputer> MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.2627 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 >Sounds reasonable. What would you think of a 2-bid that would >go straight from the top of the weight and extend back on the >aileron surface. It would be suspended in space, but not for >very far, so it should be reasonably stiff (could still buckle >in compression, I suppose) and would certainly stiffen the >structure in beaming. Gary, Go with the half moon wedges. Glass in space will not withstand compression from the flexing. I had a little buzz in my ailerons. The wedges (1/4" foam with 2 bid) silenced the vibe. Larry