Return-Path: Received: from [216.244.30.90] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.1.8) with HTTP id 2881750 for flyrotary@lancaironline.net; Mon, 08 Dec 2003 10:41:39 -0500 From: "Marvin Kaye" Subject: Re: [FlyRotary] Re: K&M and Thick Radiators To: flyrotary X-Mailer: CommuniGate Pro WebUser Interface v.4.1.8 Date: Mon, 08 Dec 2003 10:41:39 -0500 Message-ID: In-Reply-To: <002301c3bd17$2fd56ec0$0000a398@Carol> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "sqpilot@earthlink" : > Ok, Paul. Based on my back of the envelope calculations at a fuel burn of > 8.5 gph with that size radiator, you would need an airspeed of around 142 > mph to provide adequate air mass flow. Hi, Ed.....the aircraft should reach rotation speed of 90 mph hopefully by mid-field (1500 feet), and right after rotation and gear retraction, you set up for a 120 mph climb. Sounds like I need to re-figure to get a radiator that might cool at 120 mph in a climb. George Graham, whose aircraft is very similar to mine, said he can take off and climb at 1/2 throttle. Don't yet know what rpm that turns out to be, or how much horsepower. I'll keep plugging away at this until I find a reasonable "starting" size for my radiator. I've already collected 3 intake manifolds.....don't want to start collecting radiators. I will leave that to Rusty. Thanks again for your valuable input. Paul Conner