As of now the exit will be Completely open behind the radiator. Unlike the picture shown, my unit is angled much like the factory does with their a/c compressor.

Sent from my iPhone 4

On May 14, 2012, at 10:49 AM, "Bobby J. Hughes" <bhughes@qnsi.net> wrote:

> Chris,
>
> 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
>
>
>
> -----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" <bbradburry@bellsouth.net>
> wrote:
>
>> Chris,
>>
>> this is a cooling solution that seems to work.
>>
>> B2
>> <prop2.jpg>
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