tuft testing

On 29 Oct 2004 05:17:03 -0700, (sidk) wrote:

No, there are no other cooling air inlets. The cooling air flows down
thru the pressure cowling, down thru the cylinders, and exits out the
back around the prop spinner.
This photo shows a rear, in-flight view. The small, dark object on
the bottom cowling is the left exhaust

http://img96.exs.cx/img96/5820/Velocityinflight.jpg

This Velocity was one of the earlier versions (early '90s). The
builder/previous owner told me that this was the third attempt...
The first (IRRC) was pitot type scoops on the bottom cowling. Then
pitot type scoops on the bottom of the strakes a few inches outboard
of the bottom cowling with internal ductwork (about 2 1/2 id) piping
the air into the engine compartment. Finally, apparently the Velocity
people came up with this current design and the plane was retrofitted
shortly before I bought it.

Sid

Sid, I guess I'm stating the obvious then, the cooling system as
designed does not appear to flow enough air through the ductwork to
cool the engine properly.

You can probably improve the inflow by attaching scoops on top of the
Naca inlets. I'd recommend the scoops be standoffs, like the P-51
belly scoop so that you do not have turbulent boundary air flowing in
and disrupting the flow. You can even shape them to emulate the shape
of the Naca inlet where they attach to the opening. This should be an
easy thing to fabricate and attach for a test. Just tape them over
the inlets and fly. If you see the cooling improve, you're on the
right track.

Corky Scott