Return-Path: Received: from ms-smtp-03.southeast.rr.com ([24.93.67.84] verified) by logan.com (CommuniGate Pro SMTP 4.1.3) with ESMTP id 2587562 for flyrotary@lancaironline.net; Sun, 21 Sep 2003 01:23:30 -0400 Received: from nc.rr.com (cpe-024-211-183-088.nc.rr.com [24.211.183.88]) by ms-smtp-03.southeast.rr.com (8.12.5/8.12.2) with ESMTP id h8L5LF4R027662 for ; Sun, 21 Sep 2003 01:21:15 -0400 (EDT) Message-ID: <3F6D33CD.4060408@nc.rr.com> Date: Sun, 21 Sep 2003 01:14:53 -0400 From: Ernest Christley User-Agent: Mozilla/5.0 (X11; U; Linux i686; en-US; rv:1.1) Gecko/20020826 X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] DIE Power Calculations References: Content-Type: text/plain; charset=us-ascii; format=flowed Content-Transfer-Encoding: 7bit Ed Anderson wrote: > > Of course, that slide does not tell you anything about the inner workings of > the DIE, come to Shady Bend if you get the chance. The rest will have to > wait a tad bit longer. I did say it was a teaser! Ed, I won't be able to get to places like Shady Bend until I get an airplane built, so that's my excuse, but you have me thinking about some other recent post. High HP equates to higher fuel burn. Where you REALLY want that HP is in the climb. Once you're at cruise, the extra HP and associated fuel burn really buys you very little additional speed. Is the DIE effect controllable enough to get some extra oomph on takeoff, and then dissappear at cruise settings? -- http://www.ernest.isa-geek.org/ "Ignorance is mankinds normal state, alleviated by information and experience." Veeduber