Return-Path: Received: from [65.54.169.73] (HELO hotmail.com) by logan.com (CommuniGate Pro SMTP 4.1b8) with ESMTP id 2429817 for flyrotary@lancaironline.net; Sun, 15 Jun 2003 13:45:51 -0400 Received: from mail pickup service by hotmail.com with Microsoft SMTPSVC; Sun, 15 Jun 2003 10:45:50 -0700 Received: from 67.243.12.125 by bay3-dav43.bay3.hotmail.com with DAV; Sun, 15 Jun 2003 17:45:50 +0000 X-Originating-IP: [67.243.12.125] X-Originating-Email: [lors01@msn.com] Reply-To: "Tracy Crook" From: "Tracy Crook" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Turbo Calculator for the Rotary engine. Date: Sun, 15 Jun 2003 13:46:51 -0400 Organization: Real World Solutions Inc. MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1158 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Message-ID: X-OriginalArrivalTime: 15 Jun 2003 17:45:50.0498 (UTC) FILETIME=[F5CB9820:01C33365] Ed, Sounds like a must-have program if you are contemplating a turbo installation. I'm surprised it works correctly with 80 CID plugged in. One of the few things I have agreed with Paul Lamar on is that the 13B is equivalent to a 160 CI 4 cyl piston engine in terms of CFM of intake & exhaust volume. Perhaps the program is aware of the characteristics of the rotary and knows this relationship? Tracy ----- Original Message ----- From: "Ed Anderson" > > You do have to give the program an NA starting point like 80 CID and 160HP > for the rotary. I've checked a couple of the numbers and they come out > correct. > > Ed Anderson > Matthews, NC > RV-6A N494BW > eanderson@carolina.rr.com