Mailing List flyrotary@lancaironline.net Message #37429
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Emailing: DHDUCT.jpg
Date: Mon, 28 May 2007 11:05:08 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Dennis,
 
Sometimes a picture is worth a thousand words (and other times not {:>)), but here are some of my thoughts on your cooling situation. 
 
Here is what I think may be the problem areas:
 
1.  Top part of radiator appears to have its exit area impeded by motor/oil pan.  There air flow through this part of your radiator is probably less than idea.
2.  I can not tell from your photos but I suspect the duct may not be optimized for minimizing separation or turning the air flow for better entry into the cores.
3.  Diverter at the lip of you inlet will almost certainly cause perturbed airflow in the upper part of the duct and may affect the lower duct as well particularly at climb attitudes.
 
So here are some suggestions - only you can decide what seems worthwhile to you.
 
Here is a rough sketch DHDUCT.jpg of what I believe may be a suitable duct profile for you installation.  The outermost green lines on top and bottom is the outside wall profile of the proposed duct.  The inner green line represent my idea of what you divider should approximate.  Note that the lip of the divider does NOT go all the way to the mouth of your inlet.
 
Here are some of my thoughts behind it.
 
First, due to the relatively poor air flow you are probably getting at the upper end of your radiator (due to blockage by engine/oil pan/ mount etc,  you do not want to "waste" much of your airflow trying to push it through there.  Some - yes, but I think focusing on getting the majority of your air to flow through the "good" part of your radiator is crucial.
 
I would divert no more than 1/4-1/3 (at most) of the air flow to the upper part where I have the smaller of the diversion channel drawn.  Lets use the bulk of the air through the part of your radiator that has a better exit path.   That is why the lower diversion chamber is the larger of the two.
 
The curves of the duct/divider before the core is important.  It will tend to help curve your airflow so that it enters the core/holes in a straighter line - at least some of it.
 
This is fairly important - the divider is not started at the entrance but should start approx 1/3 of the distance from you inlet (in a straight line) to your core.  The reason for this is if you put the lip of the divider in the mouth of the inlet, you will surely get disturbed airflow in the duct - particularly in a climb attitude.  
I sketched in "Diverter Air flow.jpg"  what is likely happening to you air flow with the diverter.  Figure 1 is straight and level and assuming your air diverter is parallel to the air flow.  Figure 2 shows what you would like to have happen - the air nicely curves around and into your duct at any attitude  Figure 3 shows what is likely to be happening if the entering air and your diverter are not parallel (particularly like  in a climb).  The sharp edge of the diverter in the mouth of the inlet is creating vortices which is adversely affecting the flow in the upper part for sure and may be also affecting the flow in the lower part of your diverter.
 
 That is probably the primary reason (in my opinion) your cooling got worst after putting the divider in. 
 
By putting the lip of the diverter back in the inlet further,your are letting the airflow into your duct stabilize for a distance, the divider will then see the air (or vice versa) at nearly a straight on angle (in other words the divider will stay parallel to you duct airflow) more or less independent of the angle of your inlet to the air flow (at least in theory).  Also, if possible put some rounding on the lip of the diverter - sharp edges are very likely to cause vortices.
 
These thoughts are just that - SWAGS as to what might be the problem and what you might try to do about it. 
 
Hope it helps
 
Ed
 
 
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