----- Original Message -----

From: Jeff Whaley

To: Rotary motors in aircraft

Sent: Sunday, January 31, 2010 3:14 AM

Subject: [FlyRotary] Re: Tiff to CAD Software

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 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 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 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 see 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 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 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 and a depth of 3.5 in.

 

As stated earlier, the purpose of the post was to announce my willingness to share a software program that I had developed and found useful.

 

T Mann

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This message, and the documents attached hereto, is intended only for the addressee and may contain privileged or confidential information. Any unauthorized 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.