Return-Path: Received: from [65.33.85.197] (account ) by logan.com (CommuniGate Pro WebUser 4.1b1) with HTTP id 2081573 for ; Thu, 20 Mar 2003 18:13:59 -0500 From: "Marvin Kaye" Subject: Re: [FlyRotary] Re: Oil cooler in the radiator? To: flyrotary X-Mailer: CommuniGate Pro WebUser Interface v.4.1b1 Date: Thu, 20 Mar 2003 18:13:59 -0500 Message-ID: In-Reply-To: <00ef01c2ef33$c9b443c0$1702a8c0@WorkGroup> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Ed Anderson" : Neil's radiator was 6" thick which may have been a bit too thick. Also, Neil has his radiator install a la P51 Mustang style which may have had something to do with it. He never flew with that installation, so don't know how it may have done with more airspeed. But, I must admit I would be hesitant to go thicker than 4" depending on the fin density. Since, a number of us have sucessfully operated with the GM evaporator cores 3.25" thick and the fins are packed denser than a normal radiator, I would think that any thickness up to this should be OK. Perhaps not optimum, but I don't know how what optimum would be. While not a precise data collection method, I have held my hand behind the 3.25" GM cores and with the prop at idle, there is a great deal of hot air exiting the radiator. It would be great if we had a wind tunnel to see what a optimum width/thickness ratio might be from say 80 - 220 mph. Ed Anderson