Return-Path: Received: from mail.viclink.com ([66.129.220.6] verified) by logan.com (CommuniGate Pro SMTP 4.1b9) with ESMTP id 2475437 for flyrotary@lancaironline.net; Tue, 15 Jul 2003 00:34:45 -0400 Received: from viclink.com (p102.AS1.viclink.com [66.129.192.102]) by mail.viclink.com (8.11.7/8.11.7) with ESMTP id h6F4Yet22890 for ; Mon, 14 Jul 2003 21:34:41 -0700 (PDT) Message-ID: <3F138452.8000004@viclink.com> Date: Mon, 14 Jul 2003 21:34:26 -0700 From: Perry Mick User-Agent: Mozilla/5.0 (Windows; U; Win95; en-US; rv:1.0.1) Gecko/20020823 Netscape/7.0 X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: Engine Failure Report from Chuck Dunlap References: Content-Type: text/plain; charset=us-ascii; format=flowed Content-Transfer-Encoding: 7bit X-RAVMilter-Version: 8.4.3(snapshot 20030217) (mail.viclink.com) Ed Anderson wrote: > > > >Also, not certain that a turbo sized for a two rotor exhaust flow would get >sufficient exhaust mass flow from only one rotor to produce boost. Guess >its something Rusty can check out for us. > >Ed Anderson > > > > Ed, this was my experience in the turbo car. When the rear rotor went, there was no turbo action. -- Perry Mick