X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from imr-db03.mx.aol.com ([205.188.91.97] verified) by logan.com (CommuniGate Pro SMTP 5.4.5) with ESMTP id 5541855 for flyrotary@lancaironline.net; Mon, 14 May 2012 12:32:43 -0400 Received-SPF: pass receiver=logan.com; client-ip=205.188.91.97; envelope-from=Lehanover@aol.com Received: from mtaomg-da05.r1000.mx.aol.com (mtaomg-da05.r1000.mx.aol.com [172.29.51.141]) by imr-db03.mx.aol.com (8.14.1/8.14.1) with ESMTP id q4EGVwh3005867 for ; Mon, 14 May 2012 12:31:58 -0400 Received: from core-moe001b.r1000.mail.aol.com (core-moe001.r1000.mail.aol.com [172.29.188.65]) by mtaomg-da05.r1000.mx.aol.com (OMAG/Core Interface) with ESMTP id 40457E000089 for ; Mon, 14 May 2012 12:31:58 -0400 (EDT) From: Lehanover@aol.com Message-ID: <12a99.28f34ac2.3ce28d7d@aol.com> Date: Mon, 14 May 2012 12:31:58 -0400 (EDT) Subject: Re: [FlyRotary] Re: Possible cooling solution? To: flyrotary@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="part1_12a99.28f34ac2.3ce28d7d_boundary" X-Mailer: AOL 9.6 sub 5004 X-Originating-IP: [173.88.30.23] x-aol-global-disposition: G DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=mx.aol.com; s=20110426; t=1337013118; bh=7MZiLLhqijcEE1E5NXGRPPA0mN5hpIuJtSr6R0C2qKg=; h=From:To:Subject:Message-ID:Date:MIME-Version:Content-Type; b=GUt+5vyxVYcFVhcxqAAUqlcsFuuhlNArtcFtsVVFOjgum54Idv/Wb8nY7CQ7h8QMd 7C4S0Mccl7vlHotHCtlqO/Hxaw3Od8idRe4dIRKjPRNLBOPcjPWXT4LGT1OUsMG9tO 4T60uWC6QUagS2qzC00L5YAwvtlL2F+IgynO4DfU= X-AOL-SCOLL-SCORE: 0:2:458376352:93952408 X-AOL-SCOLL-URL_COUNT: 0 x-aol-sid: 3039ac1d338d4fb1337e2bf3 --part1_12a99.28f34ac2.3ce28d7d_boundary Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit Since you are moving your inlet to the bottom have you considered a top exit? Is the top cowl area close to the prop in low pressure? I'm sure your turbo provides plenty of extra heat during ground operations. Bobby Plus you get faster cool-down from chimney effect. Air intakes in high pressure areas work great. In low pressure areas, not at all, or flow backwards. Surface mounted intakes require the flow be attached ahead of the intake to function. So, a few vortex generators often do the trick. The scoop style operating in undisturbed air will work perfectly. Lynn E. Hanover In a message dated 5/14/2012 11:58:33 A.M. Eastern Daylight Time, cbarber@texasattorney.net writes: > > > -----Original Message----- > From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On > Behalf Of Chris Barber > Sent: Monday, May 14, 2012 10:38 AM > To: Rotary motors in aircraft > Subject: [FlyRotary] Re: Possible cooling solution? > > Don't laugh, while I think mine should be a bit more elligant, that is > similar to my mods > > I can hopefully make it pretty later. :-) > > Chris. > > Sent from my iPhone 4 > > On May 14, 2012, at 9:37 AM, "Bill Bradburry" > wrote: > >> Chris, >> >> this is a cooling solution that seems to work. >> >> B2 >> >> -- >> Homepage: http://www.flyrotary.com/ >> Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html --part1_12a99.28f34ac2.3ce28d7d_boundary Content-Type: text/html; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable

Since you are moving your inlet to the bottom have you considered a=20 top exit? Is the top cowl area close to the prop in low pressure? I'm= =20 sure your turbo provides plenty of extra heat during ground=20 operations.
Bobby

Plus you get faster cool-down from chimney effect. Air intakes in high= =20 pressure areas work great. In low pressure areas, not at all, or flow backw= ards.=20 Surface mounted intakes require the flow be attached ahead of the intake to= =20 function. So, a few vortex generators often do the trick. The scoop style= =20 operating in undisturbed air will work perfectly.

Lynn E. Hanover

In a message dated 5/14/2012 11:58:33 A.M. Eastern Daylight Time,=20 cbarber@texasattorney.net writes:

= >=20
>
> -----Original Message-----
> From: Rotary motors = in=20 aircraft [mailto:flyrotary@lancaironline.net] On
> Behalf Of Chris= =20 Barber
> Sent: Monday, May 14, 2012 10:38 AM
> To: Rotary mot= ors=20 in aircraft
> Subject: [FlyRotary] Re: Possible cooling=20 solution?
>
> Don't laugh, while I think mine should be a bi= t=20 more elligant, that is
> similar to my mods
>
> I can= =20 hopefully make it pretty later. :-)
>
> Chris.
>
= >=20 Sent from my iPhone 4
>
> On May 14, 2012, at 9:37 AM, "Bill= =20 Bradburry" <bbradburry@bellsouth.net>
> wrote:
>=20
>> Chris,
>>
>> this is a cooling solution t= hat=20 seems to work.
>>
>> B2
>>=20 <prop2.jpg>
>> --
>> Homepage: =20 http://www.flyrotary.com/
>> Archive and UnSub:
>=20 http://mail.lancaironline.net:81/lists/flyrotary/List.html
>
&g= t;=20 --
> Homepage: http://www.flyrotary.com/
> Archive and= =20 UnSub:
>=20 http://mail.lancaironline.net:81/lists/flyrotary/List.html
>
&g= t;=20 --
> Homepage: http://www.flyrotary.com/
> Archive and= =20 UnSub: =20 http://mail.lancaironline.net:81/lists/flyrotary/List.html

--
H= omepage: =20 http://www.flyrotary.com/
Archive and UnSub: =20 http://mail.lancaironline.net:81/lists/flyrotary/List.html

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