Return-Path: <JJJOHNSON@ACCESSCOMM.CA>
Received: from qmail.accesscomm.ca ([204.83.142.82] verified)
  by logan.com (CommuniGate Pro SMTP 4.1.5)
  with SMTP id 2631490 for flyrotary@lancaironline.net; Fri, 10 Oct 2003 10:05:44 -0400
Received: (qmail 12272 invoked from network); 10 Oct 2003 14:05:44 -0000
Received: from cust140-67.weyburn-leg.accesscomm.ca (HELO Jarrett) (216.174.140.67)
  by qmail.accesscomm.ca with SMTP; 10 Oct 2003 14:05:44 -0000
Message-ID: <005b01c346eb$e73eb050$8200a8c0@Jarrett>
From: "JJ JOHNSON" <JJJOHNSON@ACCESSCOMM.CA>
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
References: <list-2630908@logan.com>
Subject: Re: [FlyRotary] Re: Calculation of Rotary Power and Cooling  Capacity
Date: Thu, 10 Jul 2003 08:02:29 -0600
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

Ed, Thanks very much for this great tool. I'm wondering if you could tell me
what the normal fuel/air ratio is when I opened the file it was set at 13
'parts air' and I'm wondering what that is in Specific fuel burn numbers?
.55?  Anyway thanks again for sharing your program.

Jarrett Johnson