Mailing List flyrotary@lancaironline.net Message #38753
From: M Roberts <montyr2157@alltel.net>
Subject: Oil cooler inlet-what next?
Date: Fri, 27 Jul 2007 13:17:34 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Al,
 
I think that you should pursue one problem at a time until you have exhausted the chance of any improvement on that front.
 
You have too many variables and you are not eliminating any in these tests. You are merely making unknown possible improvements/detriments to lots of problems all at once.
 
From what I can tell, you should be getting more static pressure at the core than you are even with the BL problem and the wall being a non-ideal shape (as you stated). This could be due to leakage, or it could be due to separation and duct stall due to the boundary layer ingestion problem. There is no way to know for sure with the info you have.
 
I am not convinced by the 9 in of water 5/8 from the surface that you should get 6 in at the cooler face. Absent a methodical rake test from the wing out to below the scoop, and all along the front of the scoop it is impossible to make much of conclusion from one point of data. What is it at .25 in from the surface, along the entire length? If 1/4 of your duct has slow boundary layer air going into it (which unfortunately is the poorly contoured surface of the duct) you may have a disaster for flow inside the duct. If the flow separates from the top wall, the unseparated high energy flow will not diffuse properly. What is happening at the end of the duct towards the wheel well? All unknown variables.
 
First order of business is eliminate ANY chance of leakage past the cooler. Eliminate this variable first. This includes the area near the tanks where there is no core, only tubes. This should be sealed up completely as well as the perimeter of the core. Then retest with no other changes. Make sure you use the same location for your manometer and use foam around the end of the tube. That way your data will be apples to apples.
 
Once armed with this info you can proceed to the next step. If it were me, I would fix the duct contour (no gaps in the metal allowed) and then retest. Then I think I would try a mixing divider vane in the inlet before the change in curvature. That way the high energy air is mixed with the low energy air BEFORE it has to begin diffusion. If this fails I would move on to sealing the gear door and external VGs
 
Forget about quick fixes and start killing rats until you find the one causing the majority of the problem. Right now you are only "wounding" or perhaps missing "the" rat all together while flailing at them with a big blunt instrument. Get out the rifle and kill them (verifiably, unquestionably dead) one by one until the problem is solved. ;-)
 
I hate rats.
 
Monty
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