Return-Path: Received: from 100m.mpr200-1.esr.lvcm.net ([24.234.0.78] verified) by logan.com (CommuniGate Pro SMTP 4.1.1) with ESMTP id 2520105 for flyrotary@lancaironline.net; Mon, 11 Aug 2003 23:04:36 -0400 Received: from self55b41d15e1 (ip68-108-88-49.lv.lv.cox.net [68.108.88.49]) by 100m.mpr200-1.esr.lvcm.net (Mirapoint Messaging Server MOS 2.9.3.5) with SMTP id BBY28320; Mon, 11 Aug 2003 20:04:32 -0700 (PDT) Message-ID: <000901c36147$e432e9a0$0a00a8c0@self55b41d15e1> From: "Kenneth R. Mintz" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Cooling / Pressure recovery Date: Tue, 12 Aug 2003 20:06:28 -0700 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 6.00.2800.1158 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Greetings Gentlemen, I've been following this thread from afar and thought that I'd inject my 2 cents on this cooling issue. One Jess Myers ( maker of the Belted Air Power PSRU ) and I have confronted this same cooling problem here in Las Vegas, NV, where summer ramp temps can reach 125 F. In the '80's Jess did a considerable amount of cut-and-try testing of various ways to cool a V8 engine using a Globe Swift as the test vehicle while developing his PSRU. To cut to the chase he found that if the system cooled well on the ground at some speed over 200 mph - memory fails here - it is as if a speed brake is deployed at this point and further acceleration becomes difficult. Cooling drops off as well and the engine heats up again. The number of fins per inch as well as their thickness contributed to the development of what was termed at the time as an "air dam" above this speed maximum. The more fins/inch and/or the greater the thickness of the radiator the better the ground cooling but the sooner the air dam formed at speed. Conversely, the fewer fins/inch the poorer the ground cooling and the better the cooling at speed. I encountered similar problems while looking for various ways to improve cooling on a liquid cooled engine mounted on a pusher aircraft - a Varieze. I reached a somewhat successful compromise in the form of an aluminium radiator boosted on the ground by an electric cooling fan. Jess was most helpful in this area saving me from reinventing the wheel so to speak more than once. Hope this info is of help. Let me know if more detail would help. Ken Mintz Varieze N86KM ----- Original Message ----- From: "Tracy Crook" To: "Rotary motors in aircraft" Sent: Monday, August 11, 2003 4:27 PM Subject: [FlyRotary] Re: Cooling / Pressure recovery > > Tracy Wrote: > > If you DO > > > manage to design > > > a cooling system that will cool at full throttle on the ground, it is > > > probably a disaster in terms of cooling drag while in-flight. > > > > > > > > > Uughhh... I really hope you're wrong about this. Mine cools great on the > > ground. Define "full throttle" in terms of length of time? I've gone to > full > > throttle for about 8 seconds with 6 psi boost, just to test it, however I > > normally limit it to 0psi boost or 30" MAP. At this I've done static > run-ups > > for up to a minute. I've taxied around for 45 minutes at various power > > settings and never seen more than 90C on the coolant and 85C on the oil. > > I hope it's not a wind bag in the air. > > S. Todd Bartrim > > Turbo 13B RV-9Endurance > > C-FSTB > > Hmmm...... You don't think 8 seconds counts as cooling do you? : ) > By cooling, I mean that the temperature has stabalized. > Lots of dragsters have no cooling system at all and "cool" OK for 5 - 10 > seconds. > > Tracy > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html >