Return-Path: Received: from [24.25.9.101] (HELO ms-smtp-02-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2897277 for flyrotary@lancaironline.net; Fri, 19 Dec 2003 10:58:24 -0500 Received: from o7y6b5 (clt78-020.carolina.rr.com [24.93.78.20]) by ms-smtp-02-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id hBJFwKAc003625 for ; Fri, 19 Dec 2003 10:58:22 -0500 (EST) Message-ID: <000601c3c648$6aed7e00$1702a8c0@WorkGroup> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: evap core versus radiator Date: Fri, 19 Dec 2003 10:54:42 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1106 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 X-Virus-Scanned: Symantec AntiVirus Scan Engine Subject: [FlyRotary] Re: evap core versus radiator > Posted for "sqpilot@earthlink" : > > Hi, Kelly.....I found the core at AutoZone. I went to look at one, and the > information in their catalog was incorrect. The length and width were > correct, but the actual core thicknes was not 4 inches. It is 3 inches. If > you would like, I can go back to AutoZone and take a look at their catalog for > the part number. If I recall correctly, the unit fits 2000 and 2001 Chevy > light trucks. Hope this helps. Paul Conner > > >> FWIW. I've been playing around with the equations in K&W and finally beginning to understand some of them. Of interest, I cut apart one of the GM Cores to get some better accuracy on the core dimensions particularly fin separation and thickenss. In any case, when you plug the GM core values in to the K&W equation for a cooler block size cooling 160HP at 120MPH and assuming losses in the diffuser and ducts (real world consideration), the required core size for one GM core comes out to 94.9 in^2 core area. Since the GM core (94.5 in^2) has slotted fins, the optimum thickenss which calculates out to 6.87" for smooth fins can be reduced to 2.8". (Slotted or corrugated fins have a dramatic effect in reducing cooler core size required). So a 9x10.5x3.6 GM core turns out to be pretty close to what the equations indicate in required for that power and airspeed. Actually perhaps a bit thicker at 3.64 inch than optimum at 120 MPH according to the equations. So the 3" thick core could be a bit closer to optimum if using a GM type core than the 3.6" core for 120MPH cooling and would probably improve cooling in the take-off and initial climb phase where there is less dynamic pressure to force air through the cores. This not a recommendation at this time, just an observation Ed Anderson. A Ed Anderson RV-6A N494BW Rotary Powered Matthews, NC eanderson@carolina.rr.com