Return-Path: Received: from fed1mtao04.cox.net ([68.6.19.241] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2901552 for flyrotary@lancaironline.net; Mon, 22 Dec 2003 20:43:18 -0500 Received: from BigAl ([68.107.116.221]) by fed1mtao04.cox.net (InterMail vM.5.01.06.05 201-253-122-130-105-20030824) with ESMTP id <20031223014314.GZXC3905.fed1mtao04.cox.net@BigAl> for ; Mon, 22 Dec 2003 20:43:14 -0500 From: "Al Gietzen" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] K&W Cooling factors. Date: Mon, 22 Dec 2003 17:43:24 -0800 Message-ID: <000001c3c8f6$27d84220$6400a8c0@BigAl> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0001_01C3C8B3.19B50220" X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.4024 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 This is a multi-part message in MIME format. ------=_NextPart_000_0001_01C3C8B3.19B50220 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable =20 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.=20 =20 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 =3D 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). =20 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. =20 =20 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. =20 FWIW =20 =20 The Reynolds number (a dimensionless parameter) includes = =93characteristic length=94 of the channel, so although the heat transfer coefficient is increasing with increased velocity, the =93residence time=94 of the air = is decreasing, meaning less time for the air to heat up. But the =BC power of the Re in the demoninator is only one piece of the equation (isn=92t it?). Somewhere in the numerator is the mass flow (velocity) which wins out every time. For a given core, higher velocity removes more heat. But of course, there are other limits on velocity. =20 Or am I missing something. It=92s been a long time since I worked on details of convective heat transfer. =20 Al ------=_NextPart_000_0001_01C3C8B3.19B50220 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
=

 

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 =3D = 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

 

 

The Reynolds = number (a dimensionless parameter) includes “characteristic length” of = the channel, so although the heat transfer coefficient is increasing with = increased velocity, the “residence time” of the air is decreasing, = meaning less time for the air to heat up. =A0But the =BC power of the Re in the = demoninator is only one piece of the equation (isn’t it?).=A0 Somewhere in the numerator is the mass flow (velocity) which wins out every time.=A0 For = a given core, higher velocity removes more heat.=A0 But of course, there are = other limits on velocity.

 

Or am I = missing something.=A0 It’s been a long time since I worked on details of = convective heat transfer.

 

Al

------=_NextPart_000_0001_01C3C8B3.19B50220--