Okay.... I know who you two Yahoo's are.... enjoy you both and know where
this isn't going....I don't understand a Lick of what your talking about....
I am enjoying the fact that you respect each others opinion thou...
To fill some of our newer folks in on how this really works.... Dave is a
Practical application type engineer and Mayf is a real live rocket
scientist.... as in a recent drop out ( retired ) Huntsville Alabama
community Rocket guy....
Dave know's what works.... he is not simply shooting something down... he is
saying in his Northeastern kinda way.... " Hey bud take a look at this" and
Mayf is a purvaer ( sp ) of Fact.... if you can't prove it on a chalk board
it's simply not the way it is.... Not a Show me sorta thing.... simply Mayf
loves the theoretical math associated with the problem and enjoys working it
out in his mind....and then on paper.... then putting that knowledge into
usable hands on applications....
Just don't wait on them to move the Cooler!!!!....
Keith
----- Original Message -----
From: "DrMayf" <drmayf@teknett.com>
To: "Dave Dahlgren" <ddahlgren@snet.net>
Cc: <land-speed@autox.team.net>
Sent: Sunday, June 10, 2001 3:01 PM
Subject: Compression Ratio (was Re: Mayf's REAL website)
> Dave...
>
> other wise the math needs to be buffed up a bit as it does not match
> > test data.
>
> Sure would love to see real test data. You got some cylinder heads with
> pressure transducers in 'em? If so, can we correlate the pressures to the
> otto cycle P-V diagrams and to crank rotation? I am certain that my chalk
> board math is not the real world, but I haven't seen better yet. For
> instance I have no idea what the cylinder pressure is during the final
> compression , ignition, stroke and finally exhaust stroke. What kind of
back
> pressure do your turbos run at? I need real data to continue developing
the
> math.
>
> mayf, the ignorant desert rat
>
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