Ed had asked the following:
I still believe you need to divide you plenum vertically - have you
tried that, I know you tried several things, but I don't recall whether
you tried that approach. Perhaps as you suggested having more exit
opening would help as well as your cowl pressure seemed a bit high near
your core exits.
Ed
You asked if I had divided my inlet plenum to divert more of the water
cooling air into the oil cooler. The attached picture shows a 1/8 inch
thick foam board with a thin layer of glass cloth covering it. I
installed the diverter and flew several times. No measurable
improvement was noted. It probably helped some but I needed quite a
bit more! The picture also shows some white vanes I installed on the
rear half of the oil cooler - left side in plenum. I had thought that
the air flow was having to make too big a direction change at the
radiator face. The vanes did not improve cooling of the oil
significantly either. Bobby H. brought over a spare radiator and we
tested it on our improvised wind-tunnel at 90 deg. to the air stream
and 30 deg to the air stream. The duct leading to the radiator was
shaped so that the radiator surface area receiving the air flow was
kept the same in both tests. Using a very sensitive velocity measuring
device Bobby provided we found that the exit velocity was 28.7 mph at
90 deg - in this test the air went straight through the radiator fins.
With the radiator at 30 deg. to the air stream the air had to turn 60
deg to go through the radiator. The air speed behind the radiator at
30 deg was 28.0 mph. This test proved my suspicion that the radiator
fins were causing turbulent flow at the surface of the radiator was
WRONG! This was Good News to me because it meant my
oil/water cooling system probably could be made to cool without major
redesign.
I have made 3 flights recently with static pressure, dynamic pressure
and temperature probes under the cowl. After reviewing the data, I
made a change to the cowl outlet area and flew again. The cooling was
GREAT. My oil/water cooling system will work. I'll post
pictures and results soon. I need to do some more flight tests to
determine if I will need any sort of cowl flap or not. My water was
much cooler and the oil stayed below 210 deg. F. while climbing at 25
in MP. to 6500 ft. Also additional tests may show that I can blank off
some of the water radiator surface to force more air into the oil
cooler. Only testing will tell!
Some time ago I modified the James cowl by cutting the upper inlet hole
just below the spinner. This opening provides combustion air to the
engine. A fiberglass plate was installed to separate this combustion
air inlet from the oil/water plenum. This increased my manifold
pressure in cruise significantly.
Ed Anderson wrote:
Ed
100_1844 (Small).JPG
|