Mailing List flyrotary@lancaironline.net Message #41832
From: Al Gietzen <ALVentures@cox.net>
Subject: Oil Cooler re-visit
Date: Sat, 8 Mar 2008 08:15:41 -0800
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>

Today I did my ‘morning after’ check and cross check on my analysis of the flow data I presented yesterday. My calculation of the flow through the core based on the exit velocity profile wasn’t consistent with a check of diffuser ratio and average velocity . . . short story is – I had made a mistake. I had compensated for the flow area taken up by the tubes twice; once in each of two steps of the calculations.

 

Making that correction, if the data is to be believed, is that the calculated flow through the core is 93% of the air approaching the entrance of the scoop.  The flow distribution isn’t the greatest, but considering that the outside two rows of fins where the flow is slow have a tube on only one side, there isn’t much to be gained by a better distribution.

 

I’ll be looking further into what is then the mystery of why the cooling capacity is lower than expected.  Meanwhile, it appears that the oil/coolant heat exchanger is the plan of choice.

 

Maybe the reason the Lyc oil cooler install worked so well was that the Lyc didnt need much cooling in the first place

 

 Not convinced that its a useful reference point unless he did what you did and actually measured pressure differential across the cooler.

 

Mike Wills

Mike;

 

I agree with your assessment.  I was looking forward to meeting you last Wed. Sorry you couldn’t make it.  Another time.

 

Al

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