Mailing List flyrotary@lancaironline.net Message #40250
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: Total,duct, Ambient or Velocity????
Date: Fri, 9 Nov 2007 08:23:36 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Hi Al,
 
Not picky - some good points as always .  Yes, I agree, generalization does have its  pit falls, but on the other hand I think they can  help promote a conceptual understanding which can be refined (through study and experiments) to meet a particular situation.  As we know, cooling airflow is attempting to balance conflicting aerodynamic and thermodynamic  principles. 
 
I also agree that   much of this stuff addresses the "Perfect theoretical duct" out of necessity as there is only one perfect duct but many, many implementations  that fall short of perfect.  So its more of a conceptual goal to be aimed for  - it may never be achieved, but provides at least guidelines.   But,this is  just my opinion of course.
 
Actually, I disagree, you can not "suck" air though anything.  You may create a partial pressure difference with the fan, but it is the higher pressure air on the other end of the duct that pushes or "blows" air through the duct into the area of lower pressure  {:>)  .  
 
 But, semantics aside, yes, I agree, lower exit pressure is what you are after and that does not always equate to larger exit duct area.  In fact, if the air heated by the core flows through a nozzle it might even produce thrust and lower exit pressure using a smaller exit.  But, in general, I still believe that in most of our cases, we are short of the level of duct design that would reliably permit that.  What we need is someone to invest in one of those $$$$ Computer Fluid Flow software programs and see what they would reveal.
 
Ed
----- Original Message -----
From: Al Gietzen
Sent: Friday, November 09, 2007 1:09 AM
Subject: [FlyRotary] Re: Total,duct, Ambient or Velocity????

 

It  would seem "reasonable" that a low pressure area at the exit  will help flow through a duct - no argument on that point.  What the report appeared to say is that the after a certain point opening the exit area wider does not appear to have any additional benefit. (Exit “area” and exit “pressure” are not interchangeable terms) That if the duct is capable of "using up" all of the kinetic energy in your air flow by obstructions, pressure drops  and friction losses then enlarging the exit does not necessarily  add to the flow.

 

Remember you can not suck air through a duct, you can only blow it through. (Of course you can suck air through a duct – I do it after (and sometimes before) every flight with the fan I have on the back side of the radiator) So in effect if the straw is pinched you can "suck" on it all you want but it won't increase flow {:>).  

 

If I understood the report,  it appears that enlarging the exit area beyond the frontal area of your core provides little if any additional benefit.  That does not mean cowl flaps never work or provide benefit.  In fact it appears that the better your duct,  the more benefit the cowl flaps appear to have, the worst your duct, the lesser benefit - just the opposite of what you might think.

Ed;

 

Don’t mean to be picky, but some of these generalities are making me nervousJ.  These things are applicable only when the duct/diffuser is operating at max efficiency – which is rarely the case.

Lot’s of good info.  Thanks.  You’re right; it’s some kind of magic, and you don’t know for sure until you built it and try it.

Al

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