X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 50 [XX] Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 25 Apr 2007 15:41:58 -0400 Message-ID: X-Original-Return-Path: Received: from smtp4.na.baesystems.com ([63.164.202.13] verified) by logan.com (CommuniGate Pro SMTP 5.1.8) with ESMTP id 2003795 for lml@lancaironline.net; Wed, 25 Apr 2007 11:17:46 -0400 Received-SPF: none receiver=logan.com; client-ip=63.164.202.13; envelope-from=Christopher.Zavatson@baesystems.com Received: from BLUMS0022.bluelnk.net (blums0022.na.baesystems.com [10.40.96.145]) by smtp4.na.baesystems.com (8.13.6/8.13.6) with ESMTP id l3PFGmJP029986 for ; Wed, 25 Apr 2007 11:16:48 -0400 (EDT) Received: from GLDMS00006.goldlnk.rootlnka.net ([10.44.64.12]) by smtp1.na.baesystems.com (8.13.6/8.13.6) with ESMTP id l3PFGnC8028213 for ; Wed, 25 Apr 2007 11:16:49 -0400 (EDT) Received: from gldms10602.goldlnk.rootlnka.net ([10.64.39.19]) by GLDMS00006.goldlnk.rootlnka.net with Microsoft SMTPSVC(6.0.3790.1830); Wed, 25 Apr 2007 11:16:49 -0400 Received: from GLDMS10607.goldlnk.rootlnka.net ([10.64.39.20]) by gldms10602.goldlnk.rootlnka.net with Microsoft SMTPSVC(6.0.3790.1830); Wed, 25 Apr 2007 08:16:48 -0700 X-MimeOLE: Produced By Microsoft Exchange V6.5 Content-class: urn:content-classes:message MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Subject: RE: [LML] Cooling Drag X-Original-Date: Wed, 25 Apr 2007 08:16:45 -0700 X-Original-Message-ID: In-Reply-To: X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: [LML] Cooling Drag Thread-Index: AceGvpHVA5sAPVNbTaqCUG1FDlbOWgAge+tg References: From: "Zavatson, Christopher J \(US SSA\)" X-Original-To: "Lancair Mailing List" X-OriginalArrivalTime: 25 Apr 2007 15:16:48.0797 (UTC) FILETIME=[BE93CCD0:01C7874C] Art, <> Yes, but on a 360 not the IV. =20 The principles are the same but being turbo charged changes your cooling demands with altitude. Normally aspirated engines have the advantage of heat generation falling off with altitude. Reducing your exit area will reduce your cooling drag. You will see an increase in pressure below the engine. Your CHTs will rise, but you have margin there. Reducing exit area doesn't mean just blocking off the exit, it must be done smoothly otherwise you will reduce airflow by simply adding losses. =20 On my 360 the biggest improvement came with the conversion to a hard plenum which cut cooling drag in half. That provided a 5 kts increase in cruise speed. While even more speed is possible, I like having low CHTs.=20 Chris Chris Zavatson N91CZ 360std www.N91CZ.com =20