Mailing List flyrotary@lancaironline.net Message #38623
From: H & J Johnson <hjjohnson@sasktel.net>
Subject: Re: [FlyRotary] Re: Oil cooler inlet
Date: Sat, 21 Jul 2007 11:28:06 -0600
To: Rotary motors in aircraft <flyrotary@lancaironline.net>

> Thanks, TJ.  Back to Black – below:
>
> In deciding where to put the VGs, I looked at things with the gear
> up (Photo
> 1).  The gear door has a bump, and there is some gap around the
> door.  Don't
> know what all this does to BL.  Ended up putting VG toward the
> left side
> about 26" in font of scoop, and toward the right side right on the
> gear door
> bump.
>
>
>
> Seeing your gear leg/wheel fairing I am afraid that your BL will
> be rather
> though to "repair".
>
> If the impression is not wrong, the wheelfairing alone shadows
> about 1/2 of
> the inlet....
>
>
>
> With the wheel fairing in the way (and as it is, it will produce
> some vortex
> at the edge where the tire is visible ....) I predict that you
> have some
> rather serious vortex causing trouble at least for half the
> intake...
>
>
>
>
>
>
>
> Recommend to to bend  like in rev-01. All the way closed you will
> give away.
> I would start to keep at least 1/4" off the core in the corner...
>
>
>
> Oh, the price of innovation :-).
>
> You are going to miss this once you dialed in!
>
> Not a chance!  The innovation was putting the cooler in the wing
> root – the
> price is having to do all this back-fitting.
>
>
>
> I think the photo exaggerates the effect of the gear door cover. 
> The bump
> only extends less than 1 ½” below the surface, and is nice and
> smooth and
> round.  The reflections on its surface make it look different, and
> the gear
> door is silver (matches the bottom when the gear is down, and the
> undersurface is white.  And it is about a 18” in front of the
> scoop. I expect the
> flow bends a bit going around and over, but likely stays attached.
> Don’t
> know what happens at the end where the wheel is exposed, but that
> fallsoutside the outer end of the scoop, though some turbulence
> may affect the
> outer end of the scoop.
>
>
>
> Al

 

Al, two more questions jump to mind when I looked at this picture and the sketch again.

1-The two scoop's seem to almost overlap in the inside corner, is it possible there is

some turbulant flow coming off the lower scoop to cause problems w/ the

wing scoop.

2- B was measured w/ Foam on the pipe while C was measured w/out.. is it

possible that the foam is your problem here, is it causing it to not read the

'proper' pressure?

Jarrett

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