Mailing List flyrotary@lancaironline.net Message #62951
From: Terry <flyrotary@lancaironline.net>
Subject: Re: [FlyRotary] Re: Cooling
Date: Wed, 16 Nov 2016 05:48:58 -0800
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Steve, Charlie, et al
Look up a reference to Peter Garrison and his work on Melmoth for some interesting cooling insight.

Terry Adams
KSCK
Thorp T18C

On 11/16/2016 5:36 AM, Charlie England wrote:
Steve,

There are some very good articles on cooling drag on the CAFE Foundation web site. One thing they mention is that the most efficient exit is a 'bluff body'. I believe the info is in 'Local Flow 2' on the site:

There was some work done here in the USA many years ago that showed inlet size can be relatively non-critical to drag, as long as the shape of the inlet lip is done correctly. The technique was to regulate total flow through the system with an exit flap. The concept was to use 'external diffusion', where the air was slowed at the opening, instead of inside the cooling duct. Testing showed that there was little difference in total drag, but duct construction was simplified since shape/surface finish were not as critical (air was already moving slowly when it entered the duct). I think Tracy played with the technique a bit on the RV-8; perhaps he can add some info.

Charlie

On Wed, Nov 16, 2016 at 6:21 AM, Stephen Izett <flyrotary@lancaironline.net> wrote:
Thanks Finn
I had forgotten the this previously was the plan.
Steve
On 16 Nov. 2016, at 7:55 pm, Finn Lassen <flyrotary@lancaironline.net> wrote:

Don't forget the rather simple option of extra cooling by a mist of water sprayed on the radiators. A little tank with water and a windshield wiper pump. Good for long taxiing and takeoff.

Certainly not a bad option for first flight.

Finn

On 11/15/2016 4:23 PM, Stephen Izett wrote:
Hi Bill
At this point there are no cowl flaps. I tried to create some space for them should we need to increase exit volume.
I think I'd be really happy with those temps.

The cowl exits are ramps. When the front gear is down there is significantly more exit area.
There is about 36in2 of exit area (Gear door closed). 
Inlet area is currently 17in2 (right cheek) feeding water exchanger and 7in2 (lower round intake) feeding oil cooler. 7in2 of Left cheek feeds air into the filter / throttle body, leaving about 10in2 of the left cheek blanked off at present.

The Prop is a second hand electric adjustable from New Zealand. They are no longer available. Its performance is unknown at this stage. The design was taken over by Phil at  www.sprintaero.com .

Have you heard of anyone using electric fans for on the ground running?

Cheers
Steve Izett





On 15 Nov. 2016, at 11:26 pm, Bill Bradburry <flyrotary@lancaironline.net> wrote:

Steve,
 
You could try using SCAT ducting to route any unused inlets over to the water to improve the volume of air.  What do your cowl exits look like?
In order to really know how everything is working you are going to have to fly.  It will be difficult to do a full power takeoff and then go into high speed cruise and have the cooling work perfectly for both conditions unless you have cowl flaps or some manner of controlling the air.  I currently accept 210-220 on takeoff in order to get 180-190 in cruise.
 
That plane is going to be fast!  It looks like 200K just sitting in the hangar!
 
What prop is that?
 
Bill 
 

From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] 
Sent: Tuesday, November 15, 2016 3:13 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Cooling
 
Hi there Bill.
The water exchanger is ~540 cubic inch in capacity and fed from the right cheek via a rotating trumpet shaped diffuser which in turn feeds a wedge. The oil exchanger is a turbo RX7 unit of 190 cubic inch capacity and fed via a trumpet/wedge diffuser fed from below the spinner.
I’ll send some pictures separately as they are together to large.

 
Cheers
Steve Izett
 
<image001.jpg>
 
 
 
 


On 15 Nov. 2016, at 1:00 pm, Bill Bradburry <flyrotary@lancaironline.net> wrote:
 
Steve,
Can you share any photos of your cooling install?  Oil and water.

Bill 

-----Original Message-----
From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] 
Sent: Monday, November 14, 2016 4:21 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Cooling

Hi guys.
The Glasair SIIRG is near completion and we are taxi testing.
The OAT is rising as we enter summer. Yesterday was 37C ~ 100F.
She can idle forever with water stabilising below 220F and oil below 180F if
the OAT is below 70F but not sure yet about the warmer days.
I'm wondering about 3 options and would value your experience and thoughts:
1. Route some more air from the left cheek into the water heat exchange
diffuser currently fed by the right cheek. I am currently only using 50% of
the left cheek (Blanked off). The other 50% of the left cheek feeds air to
the engine. The air is likely not to want to do the gymnastics required to
travel the path available. 
2. Install another small core fed by the available left cheek air with water
from the heater outlet. This would make for easy plumping as far as the
water system. I'm not sure how much heat we could reject from that small
diameter heater outlet?
3. Install an electric fan on the main exchanger for extended on the ground
running. Main concern with fan is, what happens when cruising at up to
200Knots? 

Appreciate you feedback

Steve Izett
Glasair SIIRG Genesis 4 port RD1C EC2
Perth Western Australia


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