Return-Path: Sender: (Marvin Kaye) To: flyrotary Date: Thu, 20 Mar 2003 17:20:05 -0500 Message-ID: X-Original-Return-Path: Received: from droid2.spawar.navy.mil ([128.49.192.70] verified) by logan.com (CommuniGate Pro SMTP 4.1b1) with ESMTP id 2081137 for flyrotary@lancaironline.net; Thu, 20 Mar 2003 11:25:25 -0500 Received: from WILLSM (willsm-pc.spawar.navy.mil [128.49.207.112]) by droid2.spawar.navy.mil (8.11.6/8.11.6) with ESMTP id h2KGPDQ17490 for ; Thu, 20 Mar 2003 08:25:13 -0800 X-Original-Message-Id: <4.2.0.58.20030320083905.014edd98@mailsd1.spawar.navy.mil> X-Sender: willsm@mailsd1.spawar.navy.mil X-Mailer: QUALCOMM Windows Eudora Pro Version 4.2.0.58 X-Original-Date: Thu, 20 Mar 2003 08:42:38 -0800 X-Original-To: "Rotary motors in aircraft" From: Mike Wills Subject: Re: [FlyRotary] Re: Oil cooler in the radiator? In-Reply-To: Mime-Version: 1.0 Content-Type: text/plain; charset="us-ascii"; format=flowed X-MailScanner: Found to be clean At 09:15 AM 3/20/2003 -0500, you wrote: >Posted for Fred Breese : > >Rusty, Increase the radiator thickness to around 4"(this is why Tracy's >airplane works so well) and your cowling clearance problems will go away. This is the approach Neil used on his failed experiment with his Lancair and Setrab oil/water exchanger. Maybe his problem was due to airflow issues, but the arguments I've heard against extremely thick radiators make good intuitive sense to me. If at all possible I'd attempt to gain core volume by increasing frontal area before adding thickness. Mike Wills