Mailing List flyrotary@lancaironline.net Message #26337
From: David Leonard <wdleonard@gmail.com>
Subject: Re: [FlyRotary] Re: Another great flying day = another day of troubleshooting
Date: Mon, 5 Sep 2005 09:57:05 -0700
To: Rotary motors in aircraft <flyrotary@lancaironline.net>

 Actually, Dave you had a higher pressure ratio (manifold to ambient) at 10,000 feet with 26" boost than at sea level with 36".  At sea level the pressure ratio would be 36/29.92 = 1.20.  At 10,000 ft ambient pressure = 20.57 " hg , so the pressure ratio would  be 26/20.57 = 1.26.  Not much greater, but it was higher by approx.1.23" Hg. (1.20 -1.26 = .06 *20.57 = 1.234" Hg).

Ed A

Right.  But what does the plug know about the ambient pressure?  I thought that it was just the absolute density of the charge that was contributing to SAG.

--
Dave Leonard
Turbo Rotary RV-6 N4VY
http://members.aol.com/_ht_a/rotaryroster/index.html
http://members.aol.com/_ht_a/vp4skydoc/index.html
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