Return-Path: Sender: (Marvin Kaye) To: lml Date: Tue, 18 Mar 2003 00:59:16 -0500 Message-ID: X-Original-Return-Path: Received: from imo-r04.mx.aol.com ([152.163.225.100] verified) by logan.com (CommuniGate Pro SMTP 4.1b1) with ESMTP id 2070731 for lml@lancaironline.net; Mon, 17 Mar 2003 22:33:50 -0500 Received: from Newlan2dl@aol.com by imo-r04.mx.aol.com (mail_out_v34.21.) id q.192.175ea4e8 (4196) for ; Mon, 17 Mar 2003 22:33:44 -0500 (EST) From: Newlan2dl@aol.com X-Original-Message-ID: <192.175ea4e8.2ba7ed98@aol.com> X-Original-Date: Mon, 17 Mar 2003 22:33:44 EST Subject: Re: [LML] Re: Decibels X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailer: 7.0 for Windows sub 10637 Hi Wendell You bring up a valid point. Active noise reduction might be a good way to go but it would cost a lot. And you also bring up another good point. Air coming in will be an acoustic leak. The probelm with active noise cancallation is that it is very expensive to set up in your plane and it doesn't deaden all frequencies. If it did, you wouldn't hear anything from them except those frerquencies which were not matched by the amplitude of the ANR or conversely, by being of a higher amplitude. They also need to be tuned for each installation. The problem with trying to eliminate the noise only from around the head level is that the noise comes from all over. And it is also often coming from the skins of the fuselage acting like a drum head. So vibration from the engine or boundary layer can excite the skin and act like a speaker, turning vibration into noise and transmitting it elsewhere. Hopefully, the acoustic tests I'm hoping to start on soon can give some real numbers to it and also help us make informed decisions as to weight /noise/dollar trade-offs. Dan Newland