Mailing List flyrotary@lancaironline.net Message #44904
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: RE: [FlyRotary] Re: HP was : Mark's BBQ Run / 20B numbers
Date: Sat, 24 Jan 2009 10:23:11 -0500
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>

Thanks, Al, for the clarification – yes.  Absolute Manifold pressure = Ambient pressure + Boost Pressure.  I see  what led to the confusion, I referred to the absolute manifold pressure as   total boost pressure when I was thinking total pressure of which boost pressure is only one component.

 

Bob, I Must need more coffee in the morning – oops, that excuse won’t work - as I sent that e mail in the afternoon {:>). 

 

Appreciate you catching my error.

 

Ed

 


From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Al Gietzen
Sent: Saturday, January 24, 2009 12:53 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: HP was : Mark's BBQ Run / 20B numbers

 

I’m sure he meant 60” MAP; 30” boost.

 

Al

 

 

Hay, Ed, I always thought 15 Psi boost was about only 30" Hg of boost-atmospheric pressure (about 15 Psi) equals only (about ) 30" Hg. Where did I go wrong?

----- Original Message -----

From: Ed Anderson

Sent: Friday, January 23, 2009 2:10 PM

Subject: [FlyRotary] Re: HP was : Mark's BBQ Run / 20B numbers

 

Should be a fire belching dragon of an engine at over 15psi, Greg.

 

 15 Psi boost would be roughly 60” Hg of boost which at an A/F ratio of 12 (assume you would run it a bit rich at those boost levels) would give at 6000 rpm approx 550 HP burning 51 gph (more power  at high rpm and boost naturally)  and producing a total of  25000 BTU/Min of heat to be dumped through the radiator and oil cooler.  Boy, you will produce more heat energy that gets dumped through your oil cooler (8484 BTU/Min) than my total (coolant and oil heat) entire engine puts out.  Hope you have big radiators and oil cooler {:>).



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