We would all enjoy looking over your work. Please submit photos
and explanations.
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