X-Virus-Scanned: clean according to Sophos on Logan.com X-PolluStop-Diagnostic: (direct reply)\eX-PolluStop-Score: 0.00\eX-PolluStop: Scanned with Niversoft PolluStop 2.1 RC1, http://www.niversoft.com/pollustop Return-Path: Received: from smtpauth09.mail.atl.earthlink.net ([209.86.89.69] verified) by logan.com (CommuniGate Pro SMTP 4.3c4) with ESMTP id 860272 for flyrotary@lancaironline.net; Thu, 07 Apr 2005 07:57:28 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.86.89.69; envelope-from=jerryhey@earthlink.net Received: from [65.176.136.213] (helo=earthlink.net) by smtpauth09.mail.atl.earthlink.net with asmtp (Exim 4.34) id 1DJVcm-00016B-VP for flyrotary@lancaironline.net; Thu, 07 Apr 2005 07:56:41 -0400 DomainKey-Signature: a=rsa-sha1; q=dns; c=simple; s=test1; d=earthlink.net; h=Date:Subject:Content-Type:Mime-Version:From:To:In-Reply-To:Message-Id:X-Mailer; b=OsUEfHAu3QJEO3Ler5wYXx9mrmv/MylMljKQS/hkdjAheEe+LJqIKp9bRkz/NvrP; Date: Thu, 7 Apr 2005 06:58:08 -0500 Subject: Re: [FlyRotary] Re: rule of thumb and RV-3 sizes- was Cooling Inlet Areas/Bernie's RV9 Content-Type: multipart/alternative; boundary=Apple-Mail-2--723581403 Mime-Version: 1.0 (Apple Message framework v552) From: Jerry Hey To: "Rotary motors in aircraft" In-Reply-To: Message-Id: <4EB6AAB8-A75C-11D9-A7A3-0003931B0C7A@earthlink.net> X-Mailer: Apple Mail (2.552) X-ELNK-Trace: 8104856d7830ec6b1aa676d7e74259b7b3291a7d08dfec79a2aa4c836dd650e06cda1f8a377c3ce5350badd9bab72f9c350badd9bab72f9c350badd9bab72f9c X-Originating-IP: 65.176.136.213 --Apple-Mail-2--723581403 Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset=ISO-8859-1; format=flowed Bill, would you agree that more air is more important than more=20 radiator? This would explain why smaller systems are functioning=20 better than predicted. Given the space available in most aircraft down=20= sizing the radiator is important. How small can we go? Jerry On Thursday, April 7, 2005, at 06:33 AM, William wrote: > The amount of heat rejected is very similiar, however the delta-T=20 > available to drive the heat into the air is less for the Rotary than=20= > for the air cooled engine because of the temperature limitations of=20 > the water cooling circuit. Therefore we cannot heat the air as hot,=20 > and therefore need more air than for a direct air-cooled engine. > Bill Schertz > KIS Cruiser # 4045 > > ----- Original Message ----- > From: rijakits > To: Rotary motors in aircraft > Sent: Wednesday, April 06, 2005 9:43 PM > Subject: [FlyRotary] Re: rule of thumb and RV-3 sizes- was Cooling=20 > Inlet Areas/Bernie's RV9 > > snip > > I mentioned that on the other list, but I was dismissed as " you can't=20= > compare aircooled engines with a rotary". > I don't think there is a great difference on the amout of cooling=20 > necessary, as the efficiency of both engines are fairly close. So some=20= > heat goes out the exhaust and the rest has to be cooled.=A0For sure = you=20 > need different ducting, but the amount of heat energy should be about=20= > the same and you want to get rid of it with the least drag, either > = way. > =A0 > =A0 > snip[ > =A0 > --Apple-Mail-2--723581403 Content-Transfer-Encoding: quoted-printable Content-Type: text/enriched; charset=ISO-8859-1 Bill, would you agree that more air is more important than more radiator? This would explain why smaller systems are functioning better than predicted. Given the space available in most aircraft down sizing the radiator is important. How small can we go? Jerry On Thursday, April 7, 2005, at 06:33 AM, William wrote: The amount of heat rejected is very similiar, however the delta-T available to drive the heat into the air is less for the Rotary than for the air cooled engine because of the temperature limitations of the water cooling circuit. Therefore we cannot heat the air as hot, and therefore need more air than for a direct air-cooled engine. Bill Schertz KIS Cruiser # 4045 ----- Original Message ----- From: = 1999,1999,FFFFrijakits To: 1999,1999,FFFFRotary motors in aircraft Sent: Wednesday, April 06, 2005 9:43 PM Subject: [FlyRotary] Re: rule of thumb and RV-3 sizes- was Cooling Inlet Areas/Bernie's RV9 snip I mentioned that on the other list, but I was dismissed as " you can't compare aircooled engines with a rotary". I don't think there is a great difference on the amout of cooling necessary, as the efficiency of both engines are fairly close. So some heat goes out the exhaust and the rest has to be cooled.=A0For sure you need different ducting, but the amount of heat energy should be about the same and you want to get rid of it with the least drag, either way. =A0 =A0 snip[ =A0 = --Apple-Mail-2--723581403--