X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from EXHUB003-2.exch003intermedia.net ([207.5.74.29] verified) by logan.com (CommuniGate Pro SMTP 5.3.2) with ESMTPS id 4104890 for flyrotary@lancaironline.net; Sat, 30 Jan 2010 12:12:41 -0500 Received-SPF: none receiver=logan.com; client-ip=207.5.74.29; envelope-from=jwhaley@datacast.com Received: from EXVMBX003-5.exch003intermedia.net ([207.5.74.45]) by EXHUB003-2.exch003intermedia.net ([207.5.74.29]) with mapi; Sat, 30 Jan 2010 09:12:05 -0800 From: Jeff Whaley To: Rotary motors in aircraft Date: Sat, 30 Jan 2010 09:14:09 -0800 Subject: RE: [FlyRotary] Re: Tiff to CAD Software Thread-Topic: [FlyRotary] Re: Tiff to CAD Software Thread-Index: AcqhW0WDnwcvekLbSz+nXVEol2EwTgAdDuiQ Message-ID: References: In-Reply-To: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-TNEF-Correlator: acceptlanguage: en-US Content-Type: multipart/alternative; boundary="_000_C03ABB0A7362B84BB53D544B3C305E0E0166B99402ECEXVMBX0035e_" MIME-Version: 1.0 --_000_C03ABB0A7362B84BB53D544B3C305E0E0166B99402ECEXVMBX0035e_ Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable Mike, I've got a 13B NA, flying a "Chubby Cubby" - 110 mph airplane. Jeff From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Beh= alf Of Mike Wills Sent: Friday, January 29, 2010 10:20 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Tiff to CAD Software Figures I'd make a statement like that and have somebody prove me wrong. I = cant remember Jeff, what airframe and what engine are you running? Mike Wills From: Jeff Whaley Sent: Friday, January 29, 2010 2:51 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Tiff to CAD Software FWIW, I my radiator core is 5.5" thick x 5.5" high x 20" wide ... it cools = ... JWW From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Beh= alf Of George Lendich Sent: Friday, January 29, 2010 4:49 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Tiff to CAD Software Thomas, I like your approach to the problem, I see nothing but positive outcomes in= proving the concept (one way or another). 3.5" is ( I believe) OK, the thi= ck verses thin debate is like comparing apples and oranges given the differ= ent applications of cars and aircraft. I don't know what speed your looking= at in cruise but 3.5" should be good for a higher cruise. I believe some h= ave used 3" cores successfully. However I'm no expert but I look forward to= the outcomes. George ( down under) Mike, The graphic is not a true representation of the final design. It merely dep= icts an unmodified P-51 scoop that has been rendered in CAD, scaled 61% and= rotated lightly in the clockwise direction. My actual radiator design has a frontal area of 203 sq in and a depth of 3.= 5 in. As stated earlier, the purpose of the post was to announce my willingness t= o share a software program that I had developed and found useful. T Mann This message, and the documents attached hereto, is intended only for the a= ddressee and may contain privileged or confidential information. Any unauth= orized disclosure is strictly prohibited. If you have received this message= in error, please notify us immediately so that we may correct our internal= records. Please then delete the original message. Thank you. This message, and the documents attached hereto, is intended only for the a= ddressee and may contain privileged or confidential information. Any unauth= orized disclosure is strictly prohibited. If you have received this message= in error, please notify us immediately so that we may correct our internal= records. Please then delete the original message. Thank you. --_000_C03ABB0A7362B84BB53D544B3C305E0E0166B99402ECEXVMBX0035e_ Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

Mike, I’ve got a 13B NA, flying a “Chubby Cubby&= #8221; – 110 mph airplane.

Jeff

 

From: Rotary m= otors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Mike Wills
Sent: Friday, January 29, 2010 10:20 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Tiff to CAD Software

 

Figures I'd make a statement like that and have somebody= prove me wrong. I cant remember Jeff, what airframe and what engine are yo= u running?

 

Mike Wills 

 

From:<= /b> Jeff= Whaley

Sent:<= /b> Friday, January 29, 2010 2:51 PM

Subject: [FlyRotary] Re: Tiff to CAD Software

 

FWIW, I my radiator core is 5.5” thick x 5.5” hi= gh x 20” wide … it cools …   JWW

 

From: Rotary m= otors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of George Lendich
Sent: Friday, January 29, 2010 4:49 PM
To: Rotary motors in aircraft
Subject: [FlyRotary] Re: Tiff to CAD Software

 

 

Thomas,

I like your approach to the problem, I se= e nothing but positive outcomes in proving the concept (one way or another)= . 3.5" is ( I believe) OK, the thick verses thin debate is like comparing apples and oranges given the different applications of c= ars and aircraft. I don't know what speed your looking at in cruise but 3.5= " should be good for a higher cruise. I believe some have used 3"= cores successfully. However I'm no expert but I look forward to the outcomes.

George ( down under)

Mike,

The graphic is not a true representation of the final design= . It merely depicts an unmodified P-51 scoop that has been rendered in CAD,= scaled 61% and rotated lightly in  the clockwise direction.

 

My actual radiator design has a frontal area of 203 sq in an= d a depth of 3.5 in.

 

As stated earlier, the purpose of the post was to announce m= y willingness to share a software program that I had developed and found us= eful.

 

T Mann


This message, and the documents attached hereto, is i= ntended only for the addressee and may contain privileged or confidential i= nformation. Any unauthorized disclosure is strictly prohibited. If you have received this message in error, please notify us immediately s= o that we may correct our internal records. Please then delete the original= message. Thank you.


This message, and the docum= ents attached hereto, is intended only for the addressee and may contain pr= ivileged or confidential information. Any unauthorized disclosure is strict= ly prohibited. If you have received this message in error, please notify us immediately so that we may correct our = internal records. Please then delete the original message. Thank you.
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