Return-Path: Received: from rwcrmhc13.comcast.net ([204.127.198.39] verified) by logan.com (CommuniGate Pro SMTP 4.3c3) with ESMTP id 812957 for flyrotary@lancaironline.net; Sun, 20 Mar 2005 20:19:36 -0500 Received-SPF: none receiver=logan.com; client-ip=204.127.198.39; envelope-from=rlwhite@comcast.net Received: from quail (bgp01386375bgs.brodwy01.nm.comcast.net[68.35.160.229]) by comcast.net (rwcrmhc13) with SMTP id <2005032101185101500eobsie>; Mon, 21 Mar 2005 01:18:51 +0000 Date: Sun, 20 Mar 2005 18:18:51 -0700 From: Bob White To: "Rotary motors in aircraft" Subject: Re: [FlyRotary] Re: BMW and EWP Message-Id: <20050320181851.6efad29e.rlwhite@comcast.net> In-Reply-To: References: X-Mailer: Sylpheed version 1.9.6 (GTK+ 2.4.9; i686-pc-linux-gnu) Mime-Version: 1.0 Content-Type: text/plain; charset=US-ASCII Content-Transfer-Encoding: 7bit Hi Al, Could you say a few words about how you determined what the optimum flow requirements for aircraft use shoud be. If it's in the archives, just a pointer to the message(s) would be enough. That's one of the factors I would like to understand better before firing up my nice new engine with a low flow cooling system. Bob W. On Sun, 20 Mar 2005 14:30:39 -0800 "Al Gietzen" wrote: > I have reported here 3 or 4 times before that I have measured the flow > through my engine and the dyno cooling loop provided by the engine driven > pump; and it correlates quite well with what I calculated the flow > requirements to be for something near optimum for aircraft use. > -- http://www.bob-white.com N93BD - Rotary Powered BD-4 (real soon)