Return-Path: Received: from envelope.rose-hulman.edu ([137.112.8.21] verified) by logan.com (CommuniGate Pro SMTP 4.2b3) with ESMTP-TLS id 3220671 for flyrotary@lancaironline.net; Fri, 07 May 2004 17:49:42 -0400 Received: from madsena (dhcp024-160-213-196.ma.rr.com [24.160.213.196]) (authenticated (0 bits)) by envelope.rose-hulman.edu (8.11.6/8.11.6) with ESMTP id i47Ln2Q08633 (using TLSv1/SSLv3 with cipher RC4-MD5 (128 bits) verified NO) for ; Fri, 7 May 2004 16:49:08 -0500 (EST) From: "Alex Madsen" To: "'Rotary motors in aircraft'" Subject: Intake manifold tuning Date: Fri, 7 May 2004 16:48:47 -0500 Message-ID: <000001c4347d$17cec640$f166fea9@madsena> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" 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 V6.00.2800.1409 I am trying to get a general idea of what size tube people are using for their intake manifolds. I will uses these numbers for a starting point and modify them for my design using tuning equations and such. 1. Runner diameter 2. Runner length 3. Plenum diameter 4. Plenum length 5. Location of fuel injector Speaking of tuning equations I am looking for the tuning equations of rotary engines. Could someone point me to a location that has them or send them to me. Thank You Alex Madsen