Thanks Bryan
That's it, 1948 wow. This is all the info, ramp angles, divergent walls,
width to depth ratio. Two of their possible recommendations involve
carburetor air and cooling air.
JB
----- Original Message -----
From: "Bryan Savage" <basavage@earthlink.net>
To: "Thomas E. Bryant" <saltracer@awwwsome.com>
Cc: "John Beckett" <saltracer@servusa.com>; <Flowbench@aol.com>;
<piggy@accessatc.net>; <land-speed@autox.team.net>
Sent: Tuesday, February 17, 2004 12:31 AM
Subject: Re: NACA duct
>
> For those who are interested,
> The NACA report is at:
> http://naca.larc.nasa.gov/reports/1948/naca-rm-a7i30/
> this URL has a brief abstract and a link to the PDF file which is 16.8
Meg.
>
> This may explain Tom's experience:
> " The boundary-layer thickness of the surface into which the inlet
> is placed was
> found to have a large effect on the pressure recovery"
>
> Cheers,
> Bryan
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