X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from exhub003-1.exch003intermedia.net ([207.5.74.28] verified) by logan.com (CommuniGate Pro SMTP 5.3.2) with ESMTPS id 4104122 for flyrotary@lancaironline.net; Fri, 29 Jan 2010 17:49:43 -0500 Received-SPF: none receiver=logan.com; client-ip=207.5.74.28; envelope-from=jwhaley@datacast.com Received: from EXVMBX003-5.exch003intermedia.net ([207.5.74.45]) by exhub003-1.exch003intermedia.net ([207.5.74.28]) with mapi; Fri, 29 Jan 2010 14:49:04 -0800 From: Jeff Whaley To: Rotary motors in aircraft Date: Fri, 29 Jan 2010 14:51:07 -0800 Subject: RE: [FlyRotary] Re: Tiff to CAD Software Thread-Topic: [FlyRotary] Re: Tiff to CAD Software Thread-Index: AcqhLPYEdgqAKV8PR9S9F/OhKThzgQACFb2A 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_C03ABB0A7362B84BB53D544B3C305E0E01669BB96996EXVMBX0035e_" MIME-Version: 1.0 --_000_C03ABB0A7362B84BB53D544B3C305E0E01669BB96996EXVMBX0035e_ Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable 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. --_000_C03ABB0A7362B84BB53D544B3C305E0E01669BB96996EXVMBX0035e_ Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

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 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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