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Tom and Jerry,
Grayhawk is piping up even when Tom is right.
Generally,
KIAS Hg."
150 1.1
175 1.5
200 2.0
225 2.5
250 3.1
These numbers are not theoretical since this is how the pitot/static
system converts ram pressure differential into indicated airspeed.
I get very confused about all these engine configurations. I have an IO 320
B with a 9:1 CR. The sump was modified to accept the throttle body on the
front where the 1&2 exhaust crossover to 2 into 1 under the sump along
with the 3&4 just behind the sump and where both exit on the pilot
side. It is very tightly packed under the cylinders making cooling more
difficult. My ram air intake is smooth walled (plumber's sleeve connection
from cowl to throttle) of decreasing, then constant diameter all the
way to the throttle - no filter, no airbox. I see very close to the
calculated rise although it is difficult to measure as the absolute pressure
sensor used in the intake system is not like the TSO'd measurement of
atmospheric ambient pressure.
The only true measurement is to fly side by side thru the same air
mass.
Grayhawk
In a message dated 5/15/2008 1:27:53 P.M. Central Daylight Time,
tnthibault@raytheon.com writes:
Jerry,
Chris was a little too strong in saying that
cowling mods are a must. I did it without required mods. The
starting point was an IO-360B1F. The pan was replaced with one from a
B1B (aft facing fuel injection servo). Performance Aero Engines mods
that sump to put the entrance on the front. It is true that you need a
custom exhaust. Mine is a four-into-two-into-one that exits on the pilot
side. The crossover is under the much shallower pan. The only
reason I had a cowl mod is that I wanted to have a Legacy style tunnel exit
and I wanted the total exit area to be smaller. The cowling sides were
unaffected. The larger question is how much benefit is to be gained by
forward facing induction. Before you change anything, observe what your
engine off manifold pressure is and then immediately go fly. Try to find
a nearby place with low enough elevation that you can safely fly, flat out, at
your field elevation. Record what your highest manifold pressure is at
that time.
Pipe up right
here Grayhawk if I am wrong, but I think the theoretical maximum ram air
pressure gain obtainable is about 2" of mercury. So if you record more
than an one inch of MAP above what you had before engine start, you already
have a pretty good induction system. Getting more is really tough.
When you move the servo forward there is very little room to have an
expanding air box to convert that high velocity air into increased MAP.
The updraft actually does pretty well, even though it looks like it
shouldn't. With a great deal of effort, I have built an expanding airbox
on the front of my engine and I do get between 1.5 and 2 inches above ambient,
but it was a huge amount of work. It is definitely producing some speed
increase. Hard to tell how much, because the airplane is in the middle
of many drag reduction mods and half un-painted right now. Too late for
this year's racing season, but there is always next year. BTW, in the
current, very dirty configuration, I get better than 210 Kts flat out at 2700
on 180 HP at 4500 DALT.
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