Return-Path: Received: from fed1mtao04.cox.net ([68.6.19.241] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2880244 for flyrotary@lancaironline.net; Sun, 07 Dec 2003 12:49:22 -0500 Received: from BigAl ([68.107.116.221]) by fed1mtao04.cox.net (InterMail vM.5.01.06.05 201-253-122-130-105-20030824) with ESMTP id <20031207174920.PYHP3905.fed1mtao04.cox.net@BigAl> for ; Sun, 7 Dec 2003 12:49:20 -0500 From: "Al Gietzen" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] Re: K&M and Thick Radiators Date: Sun, 7 Dec 2003 09:49:27 -0800 Message-ID: <001301c3bcea$7593de60$6400a8c0@BigAl> MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.4024 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 In-Reply-To: Importance: Normal Very nice picture of the test fixture, Al. Is there any meaningful way to test a NACA duct with this setup? Ernest; No, the test setup doesn't test the effectiveness of the intake scoop, it just puts the blower output into the scoop. It provides data on the air-side flow characteristics of the radiator - pressure drop and flow distribution in the core. For me it confirmed that the pressure drop across the core was low enough that there should be considerable margin in the pressure recovery in the duct (scoop); and allowed me to install baffles in the curved duct to get a relatively uniform flow distribution over the radiator area. Al