Mailing List flyrotary@lancaironline.net Message #36878
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: Pinched Duct
Date: Mon, 7 May 2007 08:08:24 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
I understand, Al.  I always appreciate your input and viewpoint. 
 
One reason I throw out the information and my "logic" is so that others can examine and critique - it would be nice if I knew it all, but, sigh! I am under no delusion that I do.  You certainly bring up food for thought and I would suggest any who may considered adopting the "Pinched" duct give serious consideration of your viewpoint.
 
External diffusion is undoubted a factor - as it is in most forward facing ducts .  I do agree that any time you accelerate air your incur greater loses, my take was that  accelerating the boundary layer delayed separation and the adverse effects so caused.  That  increased skin friction was a far lesser evil than flow separation as indicated by the NACA study.
 
  As to whether the boundary layer penetrates further due to increased velocity is probably dependent on the influence of the  rate of pressure rise vs the rate of boundary layer deceleration.  Is that relationship linear or non-linear?   Given the number of variables, I suspect non-linear but don't know.
 
The rapid expansion of the streamline duct configuration would tend to indicate (to me at least) delaying separation, by keeping the airstream energy high, until just before the core pays dividends.  Now whether my ratio of inlet, pinched and core area successfully accomplish that is simply unknown at this point. 
 
Using this approach, I have been able to reduce my inlet area and make use of a very constrained space for a duct.  Again, I make no pretense that it could possibly be as effective as a full up streamline duct for instance, but on the other hand I believe it creates less cooling drag than a streamline duct truncated sufficiently to meet my space constraints.  It might well be that its success is largely due to external diffusion as you suggest , but I would have expected that effect on all my ducts.
 
The pinched duct does cools my installation better than my previous approaches to a duct and has enabled me to reduce my radiator inlet area by 33% less area than previous duct attempts.   But, your may be correct, I may have just gotten lucky on this duct shape and it is simply "less-bad" than my  previous attempts. 
 
 I do agree that all of this is conjecture from both view points and only instrumentation, data collection and analysis might clarify what is actually happening. 
 
As always, appreciate your viewpoint.  Thanks again, Al
 
Ed
    
----- Original Message -----
From: Al Gietzen
Sent: Monday, May 07, 2007 1:30 AM
Subject: [FlyRotary] Re: Pinched Duct

Ed;

 

Well, ED, the more I look at this idea, the more trouble it gives me; so I will express a dissenting opinion.  I never argue against what works; but my conclusion here is that - assuming it does work better in your case than a nice entrance and a continuously expanding duct of some reasonable shape - is due to the fact that you have external diffusion (buildup of pressure in front on the cowl entrance) and turbulent flow at the entrance behind the prop.  So without doing some flow testing, I’d suggest caution in using this approach for inlet scoops in front of radiators in other locations.

 

Accelerating the air costs you dynamic pressure and increases friction losses, and (depending on entrance and frictional losses) ‘pinching’ the area by more than about 30% would cause serious choking of the flow, resulting in most of the air spilling around the entrance.  The more rapidly expanding area after the pinch and more rapid pressure increase is at least as likely to result in flow separation as a less rapidly expanding area, and a slower pressure increase.  And since you are now expanding from a smaller high velocity area, I’m gonna guess that the fractional area of turbulent flow would be larger.

 

The concepts you put together make sense in themselves, but it seems to me a little like adding apples and oranges to get more apples.  So, more proof of concept is required; well, at least to convince me.

 

Have you made any measurements of the flow distribution at the core exit?

 

Just my opinion, and, of course nothing personal.

 

Best,

 

Al (off to Baja for a few days of relaxation)

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