We would all enjoy looking over your work.
Please submit photos and explanations.
Art
--- On Fri, 1/16/09, Fred Moreno <fredmoreno@optusnet.com.au>
wrote:
From: Fred Moreno
<fredmoreno@optusnet.com.au>
Subject: [LML] FW: [LML] Lancair IV bragging rights - drag reduction
suggestions?
To: lml@lancaironline.net
Date: Friday, January 16, 2009, 7:01 AM
Would you care
to offer up a drag reduction prioritize list of improvements
you have made ?
Tough question, Richard. I can not quantify a lot of
the changes because I made most of them during construction so no comparison
testing was possible. And I made LOT
of changes.
I believe that the biggest improvement is also the most
difficult: a complete re-engineering of the engine cooling air flow pathway
from modified inlets to plenum to patched air leaks, to adjustable cowl flaps
that control the outlet area and exit velocity. Total time
invested with endless attention to detail in this area: maybe 1000
hours. It is not recommended. Go flying instead.
But I would recommend the following place to start:
leakage of cooling air from the high pressure area above the engine.
When you start looking for leaks, they are EVERYWHERE. Some are very
small but numerous, some are large, all are parasitic. You want the air
to flow between all the fins, full path length (no short cuts), and the oil
cooler, and no where else.
Smiley's NASA work in the 80's showed that the stock
factory installation (a turbo Piper Aztec with 250 HP Lycoming engines) of
baffles, rubber and sheet metal typically leaked 50% of the required cooling
flow. That is, if you need 100% to cool the engine, 150% was going into
the inlets and out the outlets, pure waste in momentum drag.
Most installations I have seen look OK on first blush, but
with very close inspection, virtually all leak like sieves. It takes
extreme attention to detail and a lot of patience to minimize the
leakage. But the benefits of fixing are substantial: reduced drag, and
much cooler operating temperatures.
When racing with Brent Regan and in studying many other
aircraft and collecting anecdotal data from many, I concluded that a well
built, smooth, tight fitting Lancair IV had little room for improvement
behind the firewall, so most of my work was in front of it.
If there is enough interest, I will develop a picture
catalog of all the drag reduction modifications I have made together with
some descriptive words so other builders can pick and choose what they want
to use. Some changes are easy. Some are very time consuming.
And because I started with many of the mods in place, I can not separate out
the individual benefits. But if enough people are interested, I will
compile a catalog and let Marv put it into the archives.
Fred Moreno
-----Original Message-----
From: marv@lancair.net [mailto:marv@lancair.net]
Sent: Friday, 16 January 2009 3:34 AM
To: lml
Subject: Re: [LML] Lancair IV bragging rights
Posted for "Richard T. Schaefer"
<schaefer@rts-services.com>:
Sounds great .
Would you care to offer up a drag reduction
prioritize list of improvements
you have made ?
> Now that summer is well established Down Under, I was
able to conduct some
> more flight testing. The air is smooth, winds
gentle, and the bugs have
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