Hi
Al,
If
a "full-strength" Streamline duct were tested under the conditions of
9.5"H20
at the entranced to the inlet then at the widest part of the duct
you
should theoretically measure 9.5*.84 = 7.98.
Ed;
Perhaps you could
enlighten me on this. Where does the .84 come from? Is this static pressure?
I thought that as the air was expanded and slowed, dynamic pressure was
converted to static pressure and the value increased. You’ve obviously
studied this more than I.
Regarding your second sketch, since you do have slower
moving boundary layer air moving next to the skin of the fuselage (and duct),
the vane would probably help it turn around the corner. However, you are
still ingesting slower moving air with less dynamic pressure to recover from
it. It is my opinion (no experience or hard data) that moving your
inlet fuselage side of your inlet opening approx 1 1/2 -
2"away from the fuselage would make an improvement.
You are very right about that. Actually in the location
that it is, even an inch or less away from the surface would make a big
difference. Keep in mind that the scoop is about 23” wide with about 1 ¼”
opening. How do you get BL diversion with that configuration? Of course this
configuration began the way it did because another Velocity builder
had put his standard aircraft oil cooler (for a Lyc) in the same
location, and said it worked great without a scoop – just the differential
pressure above and below the wing was enough. Go figure.
As I as looking over this diagram more carefully (Winginstallation.jpg),
it became apparent that it main point was to show one duct installation with
the inlet stand off (bottom one) and the other without inlet stand off using a
vane to assist the airflow. So, one could draw the conclusion that you
have a choice? either use inlet stand-off OR using a vane.
FWIW
Where did that diagram come from? Very interesting. I
think that my scoop opening is large enough, and the BL thin enough, that if I
can get effective diffusion in the duct it should work just fine.
Thanks for your input on this.
Al
Thanks,
Al