Return-Path: Received: from smtp3.netdoor.com ([208.137.128.157] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 3084052 for flyrotary@lancaironline.net; Wed, 17 Mar 2004 22:46:39 -0500 Received: from netdoor.com (port329.jxn.netdoor.com [208.148.193.29]) by smtp3.netdoor.com (8.12.10/8.12.1) with ESMTP id i2I3kYka025079 for ; Wed, 17 Mar 2004 21:46:34 -0600 (CST) Message-ID: <40591B9A.1070902@netdoor.com> Date: Wed, 17 Mar 2004 21:46:34 -0600 From: Charlie & Tupper England Reply-To: cengland@netdoor.com User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.4) Gecko/20030624 Netscape/7.1 (ax) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Rev-2 Runs! References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-Spam-Score: 0.1 X-Scanned-By: MIMEDefang 2.31 (www . roaringpenguin . com / mimedefang) Finn Lassen wrote: > No, they're left open. At the time I didn't realize one is supposed to > install bulkheads there. All I have is a strip of 1.5" wide .040 alu > lying flat following the cowl curve around. Stabilizes the cowl exits > a bit. > > You have the fiberglass extensions? Want to sell them cheap? > > Finn > > Russell Duffy wrote: > >> Hey Finn, I know you don't have the cowl extensions on your plane, >> but do you have the rear of the cowl cheeks blocked off, or are they >> open? I'm thinking they're probably blocked off, but I can't recall >> for sure. I looked at installing mine today, and realized that it >> was going to require significant work, since the rear cheek bulkhead >> doesn't come close to fitting. > > FWIW, the CAFE Foundation's research has shown that using a cooling exit shape very similar to Finn's cheek exits might be the most efficient way to get air out of the cowl. Charlie