Return-Path: Received: from tomcat.al.noaa.gov ([140.172.240.2] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 552561 for flyrotary@lancaironline.net; Wed, 01 Dec 2004 11:19:45 -0500 Received-SPF: none receiver=logan.com; client-ip=140.172.240.2; envelope-from=bdube@al.noaa.gov Received: from PILEUS.al.noaa.gov (pileus.al.noaa.gov [140.172.241.195]) by tomcat.al.noaa.gov (8.12.0/8.12.0) with ESMTP id iB1GJFa5024410 for ; Wed, 1 Dec 2004 09:19:16 -0700 (MST) Message-Id: <5.2.1.1.0.20041201090413.04e08d88@mailsrvr.al.noaa.gov> X-Sender: bdube@mailsrvr.al.noaa.gov X-Mailer: QUALCOMM Windows Eudora Version 5.2.1 Date: Wed, 01 Dec 2004 09:19:18 -0700 To: "Rotary motors in aircraft" From: Bill Dube Subject: Re: [FlyRotary] Re: Muffler design In-Reply-To: Mime-Version: 1.0 Content-Type: text/plain; charset="us-ascii"; format=flowed > > >I believe (have not done the calculations) that if you put both exhaust into >the same tube that you may find 24" is sufficient to get some good noise >reduction. However, in order to handle double the exhaust gas flow that >putting both exhaust ports into one tube, you might find that a 2"DIA tube >might be on the small size. I would probably think about at least a 2 1/2" >perhaps 3" dia tube. Unfortunately, I had little success in finding 3" dia >SS discs at least .062 thick. So I did not go down the 3" path. A cross-over pipe is significantly different than combining the two tubes with a wye. Its length and positioning provide a set of resonances that can help damp the sound. The length of the cross-over itself combined with the length of pipe between the engine and the cross-over tee, and the length of pipe from the tee to the first muffler baffle all play a role. Not a simple system by any means. Perhaps one could nickel plate a section of 4130 airfoil shaped tubing for the cross-over.