Return-Path: Received: from imo-d07.mx.aol.com ([205.188.157.39]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Fri, 22 Sep 2000 10:53:21 -0400 Received: from RWolf99@aol.com by imo-d07.mx.aol.com (mail_out_v28.15.) id k.96.9eb10f5 (3318) for ; Fri, 22 Sep 2000 11:00:12 -0400 (EDT) From: RWolf99@aol.com Message-ID: <96.9eb10f5.26fccdfc@aol.com> Date: Fri, 22 Sep 2000 11:00:12 EDT Subject: Re: Aluminum Panel Inserts To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> In a message dated 9/21/0 10:33:01 PM, you wrote: <> I don't think it really matters. This is not a highly stressed part. I'd use any 6000 series (6061, 6063), 2024 or 7075. I'm using 6061, because it was readily available. If you think about it, the likely failure modes are buckling, not overstress. Buckling will not be affected significantly by alloy selected, since the Young's modulus for the alloys is comparable (he says, without actually looking it up). - Rob Wolf >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>