X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 26 Sep 2005 23:19:52 -0400 Message-ID: X-Original-Return-Path: Received: from smtpauth04.mail.atl.earthlink.net ([209.86.89.64] verified) by logan.com (CommuniGate Pro SMTP 5.0c2) with ESMTP id 734218 for lml@lancaironline.net; Mon, 26 Sep 2005 21:51:34 -0400 Received-SPF: none receiver=logan.com; client-ip=209.86.89.64; envelope-from=lancair403@earthlink.net DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=dk20050327; d=earthlink.net; b=Lr81aGUERIn6WdkPAmFPzSCwEiAq1ZdhwAKLwcaew3LzQDz8G3PU52ikjrpZNvOX; h=Received:Message-ID:X-Priority:Reply-To:X-Mailer:From:To:Subject:Date:MIME-Version:Content-type:X-ELNK-Trace:X-Originating-IP; Received: from [4.153.190.29] (helo=earthlink.net) by smtpauth04.mail.atl.earthlink.net with asmtp (Exim 4.34) id 1EK4cL-0005UI-SQ for lml@lancaironline.net; Mon, 26 Sep 2005 21:50:50 -0400 X-Original-Message-ID: <410-2200592271504631@earthlink.net> X-Priority: 3 Reply-To: lancair403@earthlink.net X-Mailer: EarthLink MailBox 2005.1.47.0 (Windows) From: "william rumburg" X-Original-To: "Lancair Mailing List" Subject: RE: [LML] Re: Engine Cooling and Cabin Heat X-Original-Date: Mon, 26 Sep 2005 21:50:46 -0400 MIME-Version: 1.0 Content-type: text/plain; charset=US-ASCII X-ELNK-Trace: 27715828ce90b1c1624ea3431430cac6239a348a220c2609a7cc9dc3c0336cd205fd4b2b1e3c8458666fa475841a1c7a350badd9bab72f9c350badd9bab72f9c X-Originating-IP: 4.153.190.29 Chris- Although air-cooling of an engine is a simple concept (the transfer of engine heat to the air mass flowing over the engine), it does grow complex considering air flow dynamics and the many variables of a cowled engine. The 2.25 square inch cabin heat valve represents approximately 6% of the two 4" circular air inlets and I know its unlikely that eliminating it would improve engine cooling by that same 6%. It is, however, potential engine cooling air just thrown away when not in use and would be an easy check to block off the opening. I'd like to have CHTs no more than 380 on climb out and 340-360 in cruise. Bill Rumburg N403WR (Sonic bOOm) > Bill, > <> > > Why not perform a quick test to check the impact. Go on a reference flight and record; ALT, MP, OAT, RPM, EGTs, CHTs, and the price of avgas. Now block off the cabin heat inlet. You'll also want to disconnect the tubing at the heat muff so that you don't get a bunch of stagnant hot air in there. On the test flight reestablish the same flight conditions as closely as possible and take you readings. > > Chris Zavatson