Oh; yeah. I also tried VGs about 2 1/2 ft in front of the exit
fairing --
no noticeable effect. I had previously tried smaller VGs on top of the
exit
fairing for no joy.
Al
Hey Al,
I think there's likely separation as illustrated in the first picture.
I think Paul is right about the wedge diffuser, but I don't think you
have
to move the cooler to the cowl. Maybe have a look at the 2nd pic...
What do you think?
Matt-
A simple flap hanging down would be very inefficient. It would force
all the dynamic pressure to the rear of the coil, force the air to make
a sharp 90 degree turn, and keep all the boundary layer air at the front
of the core. The front half of the core would get little to no airflow.
Al, from your sketch, I'm guessing that is the problem you're having
now. The front half or your core is sitting idle. Ed mentioned that
you're ingesting boundary layer. Weak air. Doesn't have the energy to
make a turn. But that is the air that your trying to turn the hardest.
I agree with Matt that you will have very stale turbulent air in the
upper part of the intake duct, but I'll bet dollars to donuts that the
lower section will show very clean flow. The turns are slight, conform
to K&W and air is the most energetic in the duct.
I'd concentrate on trying to stir up that boundary layer and try to get
some energy into that portion of the duct. Try adding little reverse
winglets built on standoffs that you mount to the inside wall of the
scoop. If you can ignore my shaky freehand sketching, I've drawn what I
would try on top of your drawing.
Ernest Christley
You need to read my book Ernest.
You can get it from Aircraft Spruce
http://www.rotaryeng.net/how-to-cool12.html
http://www.aircraftspruce.com/catalog/bvpages/coolYourWankel.php
--
Paul Lamar ...No rotor no motor.
Here is a better way of dealing with the boundary layer Al.
This is from Hoerner Fluid Dynamic Drag.
--
Paul Lamar ...No rotor no motor.
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