Do you want this big green box to go away? Well here's how...

Click here for full update

Wildcat! photo archives restored.

Click here for full update

Donors can now disable ads.

Click here for instructions

Add yourself to the user map.

Click here for instructions

SR Chevy Cowl/Cooling design and cabin heat

Converted from Wildcat! database. (read only)
Mike Kimball

SR Chevy Cowl/Cooling design and cabin heat

Post by Mike Kimball » Sat Feb 18, 2012 9:50 am

One way is described in the link that Ken had in one of his emails.
Basically, these guys that had an RV-6A with a Suburu engine just kept
adding small radiators until they had enough. OK, that's a terrible way to
do it. But they did mention some good tidbits like the fact that thicker
cores are bad. It's better to have a longer, wider rad than one that is
thicker (i.e., having more cores). But space requirements may force you
into more cores to make it fit. You can also glean some info by looking at
the total area and volume numbers they came up with. Compare that to the
size of their engine to the one you want to use and you might start getting
in the ballpark. I also plan to look at automotive installations and the
total area and volume used for engines my size. Of course, the way you flow
the air through the rad will have a big effect on how big the radiator needs
to be. The greater the pressure differential you can manage between the
inlet and outlet, the smaller the rad will need to be. Hey, we're
definitely experimenters here when using non-standard engines. We'll all
probably have to just try different sizes, airflow designs, etc. just like
they did unless we just get lucky the first time. Of course, you can spend
the rest of your life trying to optimize the system for lowest drag achieved
with sufficient cooling in all phases of flight, or you can stop when the
system provides sufficient cooling and not try to tweak out another knot or
two. I had a Murphy Renegade Spirit with a Rotax 912 that was definitely
running too hot. So one day I totally removed all the carefully made
baffling around the engine, leaving the entire engine compartment wide open
under the round bump cowl leaving a big open hole in the cowl behind the
prop. Temps came way down and I never had another problem, even though I
was flying all over the Australian outback with outside air temps well over
100 degrees F. Don't ever do this with a Lycoming, but it worked for the 912
Renegade. I may have lost a knot or two but with the Renegade you'd never
notice anyway.

Mike

-----Original Message-----
From: mike.davis@dcsol.com [mailto:mike.davis@dcsol.com]On Behalf Of
rickhm@comcast.net
Sent: Tuesday, December 14, 2004 10:09 AM
To: rebel-builders@dcsol.com
Subject: Re: SR Chevy Cowl/Cooling design and cabin heat


A question that I have long pondered is how do you determine the size
(widthxheight) of your radiator. There are so many variables here that are
hard to predict. Thickness of the radiator, density of cooling fins within
the radiator, airflow, etc. I finally concluded you just give it a try and
see what you get. A more analytical approach I would prefer. Any thoughts?

-------------- Original message --------------
Actually I'm not sure what the RV6 did but I have uploaded two of my old
pix. The backs (inside?) of the side ramps continues forward inside the
cowl about 6 or 8" so hopefully the exit air picks up speed as it nears
the exit. The rads in the nosebowl thing on the RV6 has packaging
advantages but it doesn't seem to work for everyone and it is a far from
optimum solution. There is not enough room (length) for reliable
pressure recovery in the intake duct and the intake is closer than
usually desireable to the prop among other things.

The opening just below my spinner is ducted to the heater core and there
is a 5" muffin fan to assist while on the ground to make sure the
windshield stays clear. It was the highest power 5" muffin that I could
put my hands on and I think it draws about 0.8 amp.

Yes I'd have also put the rad below the oil pan if I could have fit it
in but now that it is done I do like not having the rad in the way when
working on the engine. I had to exit the exhaust out the far side of the
cowl to keep it away from the cooling air intake.

Ken

Mike Kimball wrote:
Heater core in the cabin just like a car was my first thought. All those
other thoughts came later. After all your comments and more thought I
think
the ideal system would be to have the heater core and the fan in the
cabin.
(At first I was trying to avoid coolant in the cabin since I can still
smell
leaked coolant in my Mustang's carpet when it's warm outside.) Then I
would
just need two holes in the firewall for the coolant hoses. But looking at
the available space on the cold side of the firewall I don't know if
there
is enough room. I am excited about the comment on using a computer fan. I
had been envisioning much larger fans as found on cars. I could probably
even rig a rheostat to vary the fan speed. I will also check out the
heater
core sources mentioned by a couple of contributors. I would like to run
dedicated ducting to the back seat area but right now I'm putting that in
the "too hard and I want to get flying" box. So I am going to progress
with
the idea of mounting the fan and heater core in the middle of the
firewall,
inside, with an air box with five outlets. One pointing right down the
middle to hopefully send warm air towards the back, two outlets to the
side
for the front passengers, and two outlets for the windshield defrost. If
humidity from using inside air is a problem I'll have to cross that
bridge
when I come to it. By circulating air from inside the cabin that should
pretty much eliminate the possibility of CO.

As for the radiator - I think I'll progress with mounting it below the
oil
pan somewhere. I think the comment about ducting air to it and then
having
a separate system for general air circulation around the engine is good.
About the "tapered flush side cowl exits (acceleration ramps)", do you
have
any pictures Ken? It's probably similar to the ones used on the RV-6A in
the article you pointed out for me to read. Thanks.

Mike





-----------------------------------------------------------------
List archives located at: https://www.dcsol.com/login?mode=HTML
username "rebel" password "builder"
Subscription services located at:
https://www.dcsol.com/public/code/html-subscribe.htm
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------



-----------------------------------------------------------------
List archives located at: https://www.dcsol.com/login?mode=HTML
username "rebel" password "builder"
Subscription services located at:
https://www.dcsol.com/public/code/html-subscribe.htm
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------






-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

LisaFly99

SR Chevy Cowl/Cooling design and cabin heat

Post by LisaFly99 » Sat Feb 18, 2012 9:50 am

In a message dated 12/14/2004 1:12:40 PM Central Standard Time,
rickhm@comcast.net writes:

A question that I have long pondered is how do you determine the size
(widthxheight) of your radiator. There are so many variables here that are hard
to predict. Thickness of the radiator, density of cooling fins within the
radiator, airflow, etc. I finally concluded you just give it a try and see what
you get. A more analytical approach I would prefer. Any thoughts?



RICK MIKE ALL
_http://www.rondavisradiators.com/_ (http://www.rondavisradiators.com/)
_http://www.novak-adapt.com/knowledge/cooling.htm_
(http://www.novak-adapt.com/knowledge/cooling.htm)
_www.rondavisradiators.com_ (http://www.rondavisradiators.com)

_www.novak-adapt.com_ (http://www.novak-adapt.com)
Don't know if theses links will go through, but verry good info on cooling.
Ron Davis is the best. at custom rads. And he'll work with you on size and
space limitiations. Been there with a Subaru.
PDSmith




-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------

Ken

SR Chevy Cowl/Cooling design and cabin heat

Post by Ken » Sat Feb 18, 2012 9:50 am

Mostly from sorting through the Contact articles, I liked the starting
point of 2 cubic inches of rad core volume and 1 square inch of rad core
face area that one author recommended as a reasonable starting point.
For our speed range and some ground cooling I like a two inch thick rad
with 1" wide aluminum tubes and somewhere around a dozen to 14 fins per
inch with a low louvre angle so ground cooling is possible. It appears
that will cool the engine easilly unless something major is wrong such
as inlet air getting partially heated by the exhaust or really really
bad duct design. A good duct lets the incoming air slow down (while
recovering pressure) passes it through the core and then lets the air
speed back up (as the pressure drops back towards ambient) for
discharge. The outlet is usually larger than the inlet of course since
the heated air has more volume

A 3" thick custom core is workable and lower total drag but much less
unforgiving of poor duct design and generally more suitable for faster
aircraft I believe. It is probably still easier to force air through a
3" custom core though than through the air conditioner evaporator cores
that some folks successfully use.

The louvre angle is probably not something that you can specify but a
high angle on dense air conditioner evaporator fins make it very
difficult to get air flow without a fan on the ground as those are
designed to work in conjuction with a centrifugal fan and significant
pressure drop. I didn't know what a louvre angle was when I started this
but the fins have little cutout flaps in them that direct air sideways
through the fin.

Yet another consideration is whether you can dump heat from the cabin
heater (you'll probably have a fan on that) overboard to supplement
ground cooling.

Ken
please remember the usual caveat that all the above is not from first
hand experience - it's just a summary of some of what I think (hope) I
learned when I designed mine...

rickhm@comcast.net wrote:
A question that I have long pondered is how do you determine the size (widthxheight) of your radiator. There are so many variables here that are hard to predict. Thickness of the radiator, density of cooling fins within the radiator, airflow, etc. I finally concluded you just give it a try and see what you get. A more analytical approach I would prefer. Any thoughts?

-------------- Original message --------------





-----------------------------------------------------------------
List archives located at: https://mail.dcsol.com/login
username "rebel" password "builder"
Unsubscribe: rebel-builders-unsubscribe@dcsol.com
List administrator: mike.davis@dcsol.com
-----------------------------------------------------------------


Locked