Mailing List flyrotary@lancaironline.net Message #38385
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Duct inlets was Oil Cooer air flow
Date: Fri, 13 Jul 2007 15:13:15 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Al, here is a couple of diagrams of intakes similar to yours from a series of articles on cooling that was published some time ago.  But, may have some applicability to your situation.
 
According to its design parameters .  Your exit area should be greater than 115% (with flap closed - looks like you're OK there), your length (L)  of duct appears to be at least as long as the height of your core .  You duct entrance should be between 1/6 and 1/3 of your core height which if it were the stock 4" high oil cooler means your inlet height should be between 1/2" and 1.33" in height, I think you are OK there as well.   The only thing that I can see that would appear to be in conflict with these design parameters would appear to be you have not inlet stand-off and the boundary layer ingestion may be your problem. 
 
In the Wing Installation.gif  file you can see where they are using a turning vane very much as you proposed, so I may have been more pessimistic than correct in my previous e mail about the effectiveness of the vane.  So, with this, I would definitely say - "Try the Vane!"
 
ED
 
 
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster