Mailing List flyrotary@lancaironline.net Message #3207
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: DIE Power Calculations
Date: Mon, 22 Sep 2003 11:54:37 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Appreciate you correcting my misperception, Jim

   Like I say,  live and learn every day - or it sure becomes boring {:>)

Ed


Ed,
It's counter intuitive as all hell.  Took me a long time to accept it, and
very
few people who don't flail around in the stratosphere know about that.  If
you
were to look at a plot of atmospheric temperature against altitude, you'd
see
that temperature decays at the adiabatic lapse rate from the surface to
the
tropopause (about 36k', standard day) at which point it stabilizes at
something
around -45F for the next dozen miles or so.  Speed of sound stabilizes in
the
stratosphere at about 450 kts.

From my catalog of "Little Known Facts About Unknown People" .... Jim S.
--
Jim Sower
Crossville, TN; Chapter 5
Long-EZ N83RT, Velocity N4095T


Ed Anderson wrote:
Ok, Jim

>
> Must have been asleep in that part of class.  I knew that in the
atmosphere
> the density is dependent on the air temperature and the speed of sound
is as
> well.  I guess I am still somewhat surpised that if you pressurized a
gas
> say to 10-20 atmospheres that speed of sound would not be increased
(even
> after you let it cool off from the compression heating).  But, you live
and
> learn every day.
>
> I agree that having the intercooler before the throttle body would
eliminate
> it from any possible disruption of the DIE FAW.  Also agree that
anything
> you do to stabilize intake manifold air temp would also stabilize the
rpm at
> which DIE occurs.
>
> Thanks Jim, I stand corrected.
>
> Ed
>
> >>  Homepage:  http://www.flyrotary.com/
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