Mailing List flyrotary@lancaironline.net Message #41889
From: Tracy Crook <tracy@rotaryaviation.com>
Sender: <rwstracy@gmail.com>
Subject: Re: [FlyRotary] Re: Emailing: Inclinded Radiators.doc
Date: Mon, 10 Mar 2008 11:59:57 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Yeah, I was wondering about that myself.  Did they fill up the gap left by the rad as it was inclined by using a bigger rad?  If so, the rad was not a fixed factor so the data is not too meaningful.  Ignoring that is like ignoring the angle and saying that a bigger rad gave them 30% more cooling.  Well Duh.. :>)
 
Tracy

On Sun, Mar 9, 2008 at 8:16 PM, Ernest Christley <echristley@nc.rr.com> wrote:
Ed Anderson wrote:
> Sorry, Al, there was not any more to be had out of that document.  I can understand that all angles of inclination may not be equal - in heat transfer or drag, but must admit I was surprised to find that 55deg supposedly provided 30% more heat transfer and 20% less drag than one perpendicular to the air flow.  It would be interesting to find out the source of such a conclusion - I mean the graph looks like it comes from somewhere{:>)
>
The last sentence is interesting, and may be the key to their finding:

Due to the use of larger radiator, weight incensement finally eliminates
the benefits gained by an inclined radiator...

So it appears that they have a set amount of room for a radiator.  Set
vertical, the rad is small doesn't cool well and the air is still moving
fast so it makes a lot of drag.  Lay it over, and you increase the
frontal area and increase radiator volume.  The air has expanded, thus
moving slower, reducing drag.

We tend to start with a required amount of cooling, and let that lead us
to how much radiator we need.  We design that in, whatever it takes.
This approach starts with a given volume, and looks to fill it with the
most cooling possible.

--

http://www.ronpaultimeline.com



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