Abrasive flow finishing

Gordon Couger gcouger at ionet.net
Thu Dec 18 09:12:31 GMT 1997


Turbulant flow is one of the all time difficult quesions. I find it
fascinating to
observe.

I have done some thinking since th last post. I am not sure which is
desirable
in a FI engine. Turbulance makes great sense in carborated mill. The object
is to get it to the dance with as little drag as is possible. We can deal
with
laminar flow and we can deal with turbulant flow but where the overlap we
have
problems. I woul likd to plead off as nievie young student led astray I was
well
old enough to knowbetter but I kissed up to a phd cllass on baysiam
statotostocw/

Afert touse two I can prove water rims up hill amd a gppd deal more .  In
those
I leanred that in opne channdl flow you cam up with factors of 8 and they
ase close e
cloes thy call it one. And then bayes methded you couodlany thintg ot any
thing,

I gog a ;ote mau;d;m

I read in an article on the net (or was it a magazine)somewhere about the
surface texture of ports in a cylinder head. It was something about the
benefits of porting. What they mentioned was that the exhaust side would
benefit most from having a smooth finish vs the intake.  One reason
mentioned for leaving the intake side unpolished is to help the turbulance
effect which serves to homogenize the fuel mixture for more thorough
combustion and thus better power. If I find the article again I will post
the address here so that who ever is interested may read it too.

----------
From: Dan
Sent: Wednesday, December 17, 1997 12:35 PM
To: diy_efi at efi332.eng.ohio-state.edu
Subject: Re: Abrasive flow finishing

I read an article recently in Design News concerning skin
friction drag reductions.  They quote another article in
Nature where skin friction drag was reduced by 13% on
aerodynamic surfaces by adding random small bumps to
the surface (vs a smooth surface).  Design News was considering
the fuel reduction costs possible for typical commercial aircraft.
A 13% skin friction drag equates to about a 6.5% overall
drag reduction.  Big numbers when a 1% drag reduction saves
a typical commercial aircraft about $100,000 annually in fuel
costs.

The idea is similar to the dimples used on golf balls which
enable the golf balls to fly farther than undimpled
balls.  I wonder what this might mean for engine intakes and
exhausts?  Maybe an extrude honing type smooth surface is
not the ideal surface even when injectors are near the valves.

The dimples have to be in a random pattern, else you increase
drag.  The theory is that random dimples (or chevrons) reduce
bursting near an aerodynamic surface.  Busting is caused by
low speed air streaks near the wall and is believed to be
responsible for creating intense turbulence.

Comments?

Dan L






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