Return-Path: Received: from [24.25.9.101] (HELO ms-smtp-02-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.2b5) with ESMTP id 164537 for flyrotary@lancaironline.net; Wed, 16 Jun 2004 07:44:53 -0400 Received: from EDWARD (clt25-78-058.carolina.rr.com [24.25.78.58]) by ms-smtp-02-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id i5GBiJNs010578 for ; Wed, 16 Jun 2004 07:44:20 -0400 (EDT) Message-ID: <002101c45397$4961cd90$2402a8c0@EDWARD> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Cooling airflow Date: Wed, 16 Jun 2004 07:44:29 -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 6.00.2800.1409 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1409 X-Virus-Scanned: Symantec AntiVirus Scan Engine Mike, Not a dumb question - but, part of the answer may be as you suggested. There is a lot of work to installing a rotary power plant and cowl work is one more thing. Plus, the GM cores used behind the standard duct openings have proven inexpensive and that they work just fine. Also, I suspect some folks just want to retain the original cowl profile. Powersport had an arrangement similar to what you suggest - took them a long while to overcome cooling problems with it. Don't know what the problem was (Powersport has never been very forthcoming about any problems), but I think it was placing their rad too close to the firewall. Also there is a person who sells such a cowl for the RV ( I think he originally made them for PowerSport). There is no reason such an arrangement could not be made to work, one individual in Arizona also uses a similar arrangement (rad below the engine) and had cooling problems (he may have them sorted out by now) - but, then he is in Arizona which would stress the capability of any cooling system {:>). I do not know of anyone's example to follow, so perhaps you will be the first. Ed Ed Anderson RV-6A N494BW Rotary Powered Matthews, NC ----- Original Message ----- From: "Wynn, Mike" To: "Rotary motors in aircraft" Sent: Wednesday, June 16, 2004 1:43 AM Subject: [FlyRotary] Cooling airflow > Dear All, > > I have been reading with interest for a long time and wanted to ask what > maybe a dumb question... > > Everywhere I have looked people use the standard `Lyc.' type cowls with > cheek openings and place the A/C `radiators' either side of the PSRU behind > suitable ducts. I assume this is because it is easier to adapt the existing > rather than to build a new cowl. However, would it not allow a straighter > and less draggy cooling setup if one were to design a cowl with a single > opening under the prop (a bit like, but much smaller than, a P40) and then > use a single duct to expand the area into the rads (placed under the > engine), and then continue straight out under the cockpit - perhaps with > some augmented airflow from the exhaust??? Surely this would allow a more > efficient airflow and enable smaller intake area and avoid the air having to > fight its way round the engine bay to get out? > > Is it just the fiberglass work people are avoiding, is it the avoidance of > the unknown (surely Rusty will have a go here???) > What am I missing? > > Thanks > Mike > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html >