Return-Path: Received: from [161.88.255.139] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.2.4) with HTTP id 452175 for lml@lancaironline.net; Mon, 04 Oct 2004 13:24:59 -0400 From: "Marvin Kaye" Subject: Re: [LML] Ada cooling To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.2.4 Date: Mon, 04 Oct 2004 13:24:59 -0400 Message-ID: In-Reply-To: <07E853AA-1615-11D9-95ED-000D933276F6@advancedpilot.com> References: <07E853AA-1615-11D9-95ED-000D933276F6@advancedpilot.com> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for Walter Atkinson : As some of those who attended will be able to tell you, it's tough to explain concisely. This group was there for five and a half hours of detailed instruction, 65 slides and live demos via video and had the ability to ask questions and pick our brains during the breaks. That's a lot to put into an e-mail! I'm not trying to be evasive. (If that were the point, we wouldn't have done a free Saturday program and I wouldn't have flown from Baton Rouge at my own expense to help. ) I just don't know how to answer it in simple terms, other than to say that you have to get the air to go where it's needed and restrict the air where it's not needed. It's needed most on the UNDER cylinder fins. The best advice I have is to look at a Cirrus. They got it 98% right. They missed two points that do make a difference, but they have the best factory baffling I've seen. If you baffled a Lancair to look like a Cirrus under the hood, you'd be a long, long way toward the right answers. Walter