Return-Path: Received: from [24.25.9.100] (HELO ms-smtp-01-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 485210 for flyrotary@lancaironline.net; Sun, 24 Oct 2004 20:33:35 -0400 Received-SPF: none receiver=logan.com; client-ip=24.25.9.100; envelope-from=eanderson@carolina.rr.com Received: from edward2 (cpe-069-132-109-019.carolina.rr.com [69.132.109.19]) by ms-smtp-01-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id i9P0X2Kk006087 for ; Sun, 24 Oct 2004 20:33:03 -0400 (EDT) Message-ID: <002f01c4ba29$edc913e0$2402a8c0@edward2> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: oil cooler duct suggestion Date: Sun, 24 Oct 2004 20:31:11 -0400 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1106 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 X-Virus-Scanned: Symantec AntiVirus Scan Engine So right you are, Bill. I made the assumption that the core was not the problem - but as you point out, the Mazda oil cooler does have the turbulators to promote turbulence on the oil side for better heat exchange. Could be the airflow is not the main culprit - but, since Rusty is somewhat committed? to the core {:>), I figure we'd help him work that side of the equation for a bit - then if we (he) can't get the improvement he would like, he may have to consider other alternatives (like a stock core). Ed ----- Original Message ----- From: "William" To: "Rotary motors in aircraft" Sent: Sunday, October 24, 2004 5:41 PM Subject: [FlyRotary] Re: oil cooler duct suggestion > Ed, > A third part of the equation is that the evaporator core may not function > very well as an 'oil' cooler, because it lacks the turbulence generators in > the oil flow passages. If the air temperature rise is low (20F you > speculated) I would look at the oil side of the equation. > > Bill Schertz > KIS Cruiser # 4045 > ----- Original Message ----- > From: "Ed Anderson" > To: "Rotary motors in aircraft" > Sent: Sunday, October 24, 2004 9:03 AM > Subject: [FlyRotary] Re: oil cooler duct suggestion > > > > All good points, Bernie > > > > My impression is that Rusty 1st objective is he would like for the oil > > temps to be lower. Assuming that the GM core, Rusty is using for an oil > > cooler provides adequate air/metal contact area, then it would appear to > me > > that the problem at this time is getting more cooling effectiveness from > the > > airflow. If you have adequate mass flow through the core, you will cool. > > However, if you have not adequately slowed the air down (diffusion) then > > your cooling drag could be higher than necessary. But, it would appear to > > me at this point that cooling is the crucial aspect rather than minimizing > > cooling drag. Tight 90 deg turns right before the core does not promote > > more flow through the core (in my opinion). > > > > According to K&W (if I understood the math), the more parallel the flow > is > > to the core surface at entry to the core the greater the pressure loss is > > and the less cooling effectiveness. They mention that in these cases the > > use of guide vans to direct the airflow more directly into the core > passages > > can result in cooling effectiveness approaching the straight-in duct. They > > also point out that staggering the core layers of the heat exchanger can > > also help (not feasible in this case). > > > > There appears to be two situations possible: > > > > 1. There is adequate air mass flow to cool - but the system is not > > transferring the heat to the air with the best efficiency. In this case, > > better diffusion offers improvement. > > > > 2. There is not have adequate air mass flow to cool - in this case, it > does > > not matter how effective you diffuser is, your system will not cool > > adequately. > > > > So either situation could apply in Rusty's case. > > > > If the delta T of the cooling air across the core is in the vicinity of > > 40-50F then I would estimate that he has adequate diffusion but perhaps > not > > adequate air mass flow to cool. In other words, the system is > transferring > > the coolant heat to the air with high efficiency - but, simply not enough > > air to carry away adequate heat. > > > > If the Delta T is closer to 20F then he may have sufficient air mass flow > > but inadequate diffusion (does not slow the air down enough for maximum > heat > > transfer) > > > > Even with the best diffuser a system will not adequately cool if there is > > inadequate mass flow through the core. So my focus would be 1st focused > on > > increasing the mass flow. Just my opinion, of course. > > > > Ed Anderson > > > > > > > > > > Rusty and Ed, > > > > > > Ed, maybe you know more about his configuration than what I can glean > from > > his schetches. I think we need to know whether he is trying to almost > > totally diffuse the air like mine (hopefully :>) ) to minimize the turning > > pressure loss and allow the flow to accelerate thru the cooler or whether > he > > is trying to do the Lamar type min height and volume flow path. > > > > > > Rusty, what is the x-cross maximum area perpendicular to the cooler > > compared to the inlet area? > > > > > > Boy the weather looks like it should be good on Wed for your flight down > > Ed. Rusty, really sorry you aren't going to make it next weekend, I really > > want to meet the guy behind all these emails. > > > > > > Bernie > > > > > > >> Homepage: http://www.flyrotary.com/ > > > >> Archive: http://lancaironline.net/lists/flyrotary/List.html > > > > > > > > > > > >> Homepage: http://www.flyrotary.com/ > > >> Archive: http://lancaironline.net/lists/flyrotary/List.html > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html