X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [67.8.178.154] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 5.0.9) with HTTP id 1070010 for lml@lancaironline.net; Sun, 16 Apr 2006 11:05:36 -0400 From: "Marvin Kaye" Subject: Re: [LML] Re: TSIO-550 Turbo setup for non-pressurizedLlancairs To: lml X-Mailer: CommuniGate Pro WebUser v5.0.9 Date: Sun, 16 Apr 2006 11:05:36 -0400 Message-ID: In-Reply-To: <1f29b94e4dfd8f1f00823c8331ceb058@advancedpilot.com> References: <1f29b94e4dfd8f1f00823c8331ceb058@advancedpilot.com> MIME-Version: 1.0 Content-Type: text/plain; charset="windows-1252"; format="flowed" Content-Transfer-Encoding: 8bit Posted for Walter Atkinson : Rick: I think there may be one error in your assumptions about the turbo at low MPs during descent. I could be wrong, but the compression ratio of the turbine is always a set value. At low MPs, you just have less of that raised temp air. The heat rise from the compression of the gas should remain pretty constant. What am I missing? (I'm anxiously awaiting the response from Craig to your 10 long questions! ) Walter