Mailing List flyrotary@lancaironline.net Message #18320
From: Russell Duffy <13brv3@bellsouth.net>
Subject: RE: [FlyRotary] Re: EWP Test Results/DRAG
Date: Thu, 3 Mar 2005 13:26:10 -0600
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>
Message
We all agree that the EWP flows less than the standard pump by alot (maybe only half to 1/3th as much?). 
 
For the EWP's we're trying, I agree, but they do make larger EWP's.   At the same time, I think most of us can agree that the stock pump flows too much for what we're doing.  Why would anyone slow it down by changing pulleys if it really needed to be flowing that much. 
 
But if you have less flow then the radiator MUST be larger for the engine to obtain equal cooling. 
 
Technically, I agreed, but the difference in size might be insignificant, depending on how much you change the flow. 
 
   This equates to more drag.  Now does the EWP save more energy than the ~3HP the mechanical pump uses even when the extra cooling drag in factored?  In other words, does the EWP save 3HP worth of cooling drag?  I suspect that the mechanical pump is more effecient but can't prove it.  Bill, Al, Ed and some of the engineers can probably give us a good idea though (and have).  No numbers here, I'm just trying to piont out the real issue  
 
Following this same line of reasoning, you can install an eccentric shaft pulley the size of a steering wheel, and then replace your radiator with an oil cooler from a Lycoming.  You'd be almost drag free  :-)
 
What I would like to see, is a dyno run, where everything is held constant with the exception of the water (better make it Evans) flow rate.  I'd be willing to bet that the relationship between equilibrium temp, and flow rate will not be a straight line.  I would expect that it's more of an exponential shape.  My guess is that the stock pump flow rate is located far out on this curve, such that a 10 gpm change won't make hardly any diff in temp. 
 
OK all you engineers, really let me have it now :-)
 
Cheers,
Rusty (I'll abuse Ernest later)
 
 
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