X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from vms046pub.verizon.net ([206.46.252.46] verified) by logan.com (CommuniGate Pro SMTP 5.1.9) with ESMTP id 2074733 for flyrotary@lancaironline.net; Wed, 30 May 2007 11:02:11 -0400 Received: from [71.99.193.242] by vms046.mailsrvcs.net (Sun Java System Messaging Server 6.2-6.01 (built Apr 3 2006)) with ESMTPA id <0JIV00I2S0F6EQA3@vms046.mailsrvcs.net> for flyrotary@lancaironline.net; Wed, 30 May 2007 10:01:55 -0500 (CDT) Date: Wed, 30 May 2007 11:06:57 -0400 From: Finn Lassen Subject: Re: [FlyRotary] James Cowl - RV-7a - Renesis - Cooling In-reply-to: To: Rotary motors in aircraft Message-id: <465D9311.3090405@verizon.net> MIME-version: 1.0 Content-type: text/plain; charset=ISO-8859-1; format=flowed Content-transfer-encoding: 7bit References: User-Agent: Thunderbird 1.5.0.10 (Windows/20070221) Hi Dennis, Hans already mentioned this in passing, but I want to emphasize it: How well are the radiators sealed against the cowling and in between each other? Seeming small cracks or openings can make a big difference. Finn Dennis Haverlah wrote: > I had very marginal cooling on my first and second flight - RV 7A, > James cowl, Griffin Scirocco aluminum double pass water radiator with > a Mazda 1989? RX-7 oil cooler. Water radiator fin size - 22LX13WX2.5T > inches. Oil - 19LX4.5WX 2T inches. The radiators are mounted > side-by-side under the engine and are at about 25 - 30 degree to the > inlet air flow. (The air must turn 60-65 deg to flow through the > radiators) See photos 1 and 2. After my first 2 flights, I > constructed a divider/duct to provide a duct for the engine combustion > air to make the sharp turn 90 deg. up after the inlet to get to the > filter. The bottom of this duct was also supposed to provide a duct > wall for the air going to the radiators. See photo 3. Two flights > demonstrated this really hurt - not helped - my cooling. Now I can > barely take off and fly the pattern before getting up to 210 - 215 on > oil and water. The divider duct took out about 8-10 sq. in. of inlet > area but removed the engine combustion air requirement form the > remaining inlet air going in the larger inlet.