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Date: Mon, 26 Sep 2011 10:24:37 -0700 (PDT)
From: Kelly Troyer <keltro@att.net>
Reply-To: Kelly Troyer <keltro@att.net>
Subject: Re: [FlyRotary] Re: Boost
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
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Good to have you back John !!.......................<:)=0A=0A=0AKelly Troye=
r=0A"DYKE DELTA JD2" (Eventually)=0A"13B ROTARY"_ Engine=0A"RWS"_RD1C/EC2/E=
M2=0A"MISTRAL"_Backplate/Oil Manifold=0A"TURBONETICS"_TO4E50 Turbo=0A=0AFro=
m: John Slade <jslade@canardaviation.com>=0ATo: Rotary motors in aircraft <=
flyrotary@lancaironline.net>=0ASent: Monday, September 26, 2011 9:54 AM=0AS=
ubject: [FlyRotary] Re: Boost=0A=0AOn 9/26/2011 10:16 AM, Dave wrote:=0A> O=
k... so 7.5 psi boost RELATIVE (referenced to sea level ambient) is equal t=
o about 22 psi boost ABSOLUTE (referenced to zero)=0AWell, the word "boost"=
 infers additional over ambient to me. 44 is about my max too. I couldn't u=
se that much at altitude without exceeding VNE, but the engine really doesn=
't care what the 'local' ambient pressure is - just the actual MAP.=0A=0AWo=
w - I'm so excited - my posts aren't being rejected by the host any longer.=
 Woo hoo!=0AWhoever fixed it - thank you!=0AJohn=0A=0A=0A--=0AHomepage:=A0 =
http://www.flyrotary.com/=0AArchive and UnSub:=A0 http://mail.lancaironline=
.net:81/lists/flyrotary/List.html
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<html><body><div style=3D"color:#000; background-color:#fff; font-family:ar=
ial, helvetica, sans-serif;font-size:10pt"><div style=3D"RIGHT: auto"><SPAN=
 style=3D"RIGHT: auto">Good to have you back John !!.......................=
&lt;:)<VAR id=3Dyui-ie-cursor></VAR><BR style=3D"RIGHT: auto" class=3Dyui-c=
ursor></SPAN></div>
<DIV></DIV>
<DIV>&nbsp;</DIV>
<div>Kelly Troyer<BR><B><FONT size=3D4>"DYKE DELTA JD2"</FONT> <FONT size=
=3D1>(Eventually)</FONT></B></div>
<div>"13B ROTARY"_ Engine<BR>"RWS"_RD1C/EC2/EM2<BR>"MISTRAL"_Backplate/Oil =
Manifold</div>
<div>"TURBONETICS"_TO4E50 Turbo</div>
<div><BR></div>
<DIV style=3D"FONT-FAMILY: arial, helvetica, sans-serif; FONT-SIZE: 10pt">
<DIV style=3D"FONT-FAMILY: times new roman, new york, times, serif; FONT-SI=
ZE: 12pt"><FONT size=3D2 face=3DArial>
<DIV style=3D"BORDER-BOTTOM: #ccc 1px solid; BORDER-LEFT: #ccc 1px solid; P=
ADDING-BOTTOM: 0px; LINE-HEIGHT: 0; MARGIN: 5px 0px; PADDING-LEFT: 0px; PAD=
DING-RIGHT: 0px; HEIGHT: 0px; FONT-SIZE: 0px; BORDER-TOP: #ccc 1px solid; B=
ORDER-RIGHT: #ccc 1px solid; PADDING-TOP: 0px" class=3Dhr contentEditable=
=3Dfalse readonly=3D"true"></DIV><B><SPAN style=3D"FONT-WEIGHT: bold">From:=
</SPAN></B> John Slade &lt;jslade@canardaviation.com&gt;<BR><B><SPAN style=
=3D"FONT-WEIGHT: bold">To:</SPAN></B> Rotary motors in aircraft &lt;flyrota=
ry@lancaironline.net&gt;<BR><B><SPAN style=3D"FONT-WEIGHT: bold">Sent:</SPA=
N></B> Monday, September 26, 2011 9:54 AM<BR><B><SPAN style=3D"FONT-WEIGHT:=
 bold">Subject:</SPAN></B> [FlyRotary] Re: Boost<BR></FONT><BR>On 9/26/2011=
 10:16 AM, Dave wrote:<BR>&gt; Ok... so 7.5 psi boost RELATIVE (referenced =
to sea level ambient) is equal to about 22 psi boost ABSOLUTE (referenced t=
o zero)<BR>Well, the word "boost" infers additional over ambient to me. 44 =
is about my
 max too. I couldn't use that much at altitude without exceeding VNE, but t=
he engine really doesn't care what the 'local' ambient pressure is - just t=
he actual MAP.<BR><BR>Wow - I'm so excited - my posts aren't being rejected=
 by the host any longer. Woo hoo!<BR>Whoever fixed it - thank you!<BR>John<=
BR><BR><BR>--<BR>Homepage:&nbsp; <A href=3D"http://www.flyrotary.com/" targ=
et=3D_blank>http://www.flyrotary.com/</A><BR>Archive and UnSub:&nbsp; <A hr=
ef=3D"http://mail.lancaironline.net:81/lists/flyrotary/List.html" target=3D=
_blank>http://mail.lancaironline.net:81/lists/flyrotary/List.html</A><BR><B=
R><BR></DIV></DIV></div></body></html>
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