Mailing List flyrotary@lancaironline.net Message #4894
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: K&W Cooling factors.
Date: Mon, 22 Dec 2003 19:22:43 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
----- Original Message -----
From: Al Gietzen
Sent: Monday, December 22, 2003 11:00 AM
Subject: [FlyRotary] Re: evap core versus radiator

Ed wrote:

 

Ok, Paul

 

    Using the K&W formulas, I calculate that the 14x10 core area would

handle 120HP at 120MPH TAS, you would need to get to 160 MPH to get the mass

flow to handle 160HP.  

 

Just scaling your power number on the basis of core area; it comes to about 225hp for my setup.  I designed for 200 hp at 120 mph; so I guess that is reasonable close correlation.  Either we’re both right, or both wrong J.

 

Al

 

Well, for both your and Paul's sake, I hope we are all correct {:>).

There are enough uncertainties just in the differences between different types of cooler core to make that much difference. 

 

 

Its fairly clear that air flow and core area are two of the most significant factors as together they determine the basic Mass flow possible through the cooler.  If that is not sufficient to carry away the heat you are trying to reject then all else is moot.

 

In K&W there are two coefficients they focus on, Kh the heat transfer coefficient which is dependent on the characteristics of the core, Kp the pressure drop coefficient - again based on core characteristics.  They end up with a combined coefficient that rates how well the core transfers heat based on the pressure drop this is Kv = Kh/Kp.  These coefficients are dependent on such things as the openness ratio, the hydraulic diameter of the individual passage in the core and the thickenss of the core.  Both Kh and Kp are also weakly dependent on the Reynolds number of the air flow throught the core.  I say weakly because they relate to the inverse fourth power of the Reynolds number or 1/(Re)^(1/4).

 

  Interestingly enough because it is an inverse relationship the heat transfer is better to the air with lower velocity through the core.  Not quite certain that I fully understand why, except it appears to do with the shear force and friction between the air flow in the core passage and the the passage walls.  However, while heat is apparently passed from the core walls to the air better at the lower Reynolds numbers, the downside is that low Reynold number also means lower air velocity throught the core which in turn means Low mass flow which is not good for cooling. 

 

So from the equations in K&W that there is an optimum balance between the heat transfer due to the lower Reynolds effect and the heat removed due to higher mass flow through the core. Too much of one and not enough of the other and your cooling is suboptimal.

 

FWIW

 

Ed Anderson

 

 

 

 

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