G'day Anthony,

Thanks for your detailed reply, lots to think about & plan for. I'm going to 
wool tuft test the wing root of my Ventus, as I want to improve on the lamina 
flow & induced drag in that area, which ultimately will help with climbing & 
handling.

Once I discover the separation points, I plan to 'fix it'..

Guessing I'll need to view the tufts at thermalling speeds/bank, & at my usual 
cruise speeds.


Cheers,
WPP


> On 9 Mar 2015, at 18:38, Anthony Smith <[email protected]> wrote:
> 
> Adam
> 
> I have done it on the wing tip of a large military aircraft.
> 
> Wing loading is only a problem if you have a particular issue that is wing
> loading related.  In essence what are you looking for?  Is it Reynolds
> Number related or is it Angle of Attack related?  Or both?
> 
> Wool lengths need to be visible to the camera or observer.  For my project
> we had a PC-9 as a chase plane with a photographer and video camera in the
> back seat.  So we had really big tufts. For your purpose, quite fine wool
> may work depending on how you plan to record the results. 
> 
> You do not want the tufts to overlap.  Typical patterns have the end of each
> tuft, a small gap and then the start of the tape adhering the next tuft.
> Lateral spacing is the same.  
> 
> Wool thickness will depend on what speed you are operating at.  Also will
> depend on how visible you want it.  I used the thickest wool we could find
> in order to be visible to the camera.  Also we were operating at much higher
> speeds than your average glider.  You will not need to be that thick.  Some
> simple experimenting with a range of wool sizes stuck to the wing root may
> give you an answer.
> 
> How many tufts will depend on the length of the wool tuft.
> 
> For my project, we adopted a diamond pattern.  This aligned really well with
> some features on the wingtip that we wanted to study.  The size of the
> diamond was dictated by the length of the tuft and the features on the
> wingtip.    A square pattern may work better for your problem.
> 
> Installation:  You need to tie a knot in both ends of the wool tuft.  The
> knot under the tape helps to hold the tuft in place.  The knot in the free
> end stops the wool unravelling.  A simple knot will do.  Don't get carried
> away or the mass of the knot will affect the results.  A dob of super glue
> on the free end may also work just as well.  We used triangular pieces of
> fabric reinforced tape (instant airframe) to secure each tuft in place.  We
> had the point of the triangle faving forwards.  Wing gap tape with a good
> adhesive may suit you better.
> 
> Some experimentation may be required.  However if you start off with typical
> yaw string lengths you will not be far long.  You can also space them out a
> bit initially (say at twice the tuft length) and then increase the density
> as you need to and where you need it.
> 
> There appear to be plenty of photos if you google 'flow visualization tuft'.
> 
> Anthony
> 
> 
> -----Original Message-----
> From: [email protected]
> [mailto:[email protected]] On Behalf Of Adam
> Woolley
> Sent: Monday, 9 March 2015 6:32 PM
> To: Discussion of issues relating to Soaring in Australia.
> Subject: [Aus-soaring] Wool tuft testing
> 
> G'day all,
> 
> Has anyone got any experience or thoughts on wool tuft testing a wing root? 
> 
> Does wing loading matter?
> What wool lengths & thickness is best?
> How many?
> What pattern?
> 
> 
> Cheers,
> WPP
> 
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