Mailing List flyrotary@lancaironline.net Message #41843
From: Al Gietzen <ALVentures@cox.net>
Subject: RE: [FlyRotary] Re: Cooling the 20B
Date: Sat, 8 Mar 2008 16:35:13 -0800
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>

I'm really glad that you are flying and getting such good numbers Al. I can't wait to get my 20B in the air. By the way that Spal fan IS one of the good ones. Do you remember what you paid for it? You may have a chaotic enough exit on your plane (exhausting through the prop) that the turbulence and any restriction is moot? It seems to me that the typical tractor exit will be harder to blend with the airstream, but I may be incorrect in that thought.

Bill Jepson 

Bill;

The price of the fan was on that link I sent – I think it was $118 from Jaycore.  And I mistakenly said it had 4 blades – it has 5.

You raise an interesting point about the drag effect of the air exit. It is a different story having the exit into the prop. Normally when we dump the air out of the back of a rad into the cowl we’ve pretty much lost  it’s energy and it hard to get it back in any efficient way when putting it back into the air stream. If you exit into the prop you give the prop some lower energy air to accelerate, so maybe it improves prop efficiency? Or maybe not.

One of the interesting things I learned in the recent air flow measurements came unplanned.  In the second run we had left open a couple of manometer connections inside the cowl.  I was surprised to see that they were reading about 5 ½” at 150 KIAS.  So that is pressure left over after passing through the in-cowl radiator that is accelerating the air out the ports at the back; where there is already negative pressure created by the prop.  That could help reduce the cooling drag.

Al

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