The magnification of the sideslip angle effect is to do with the shape of
the fuselage / canopy and the airflow around it. It has nothing to do with
the boundary layer.  The effect will taper off as you get further from the
fuselage but will still be noticeable out to a fuselage diameter or so away
from the fuselage surface.

 

The same effect applies to the angle of attack probes on larger aircraft.
These are all calibrated for their position on the fuselage and the
calibration factor typically ranges from 1.6 up to 2.

 

Regards

 

Anthony

 

From: Mike Borgelt [mailto:[email protected]] 
Sent: Thursday, 17 January 2019 10:26 AM
To: Discussion of issues relating to Soaring in Australia.
<[email protected]>
Subject: Re: [Aus-soaring] slip in thermals?

 

Yes, I've seen that article, Erich.

A couple of months ago we ran a flight test of the theory that the string in
the boundary layer amplified the actual sideslip. Taped a bent paperclip
with a second string 25mm above the normal one.
The boundary layer a couple of feet from the nose is quite thin so this
should have got it outside the layer. 
Nope. Strings seemed to move together.

Need to do this again with several strings at different heights. The flow
disturbance may extend much further from the surface of the nose.

Mike


At 09:36 AM 1/17/2019, you wrote:



Hello Mike,
is this article useful?
http://www.wisoar.org/Documents/Holighaus%20-%20Thermalling%20Efficiency.pdf

ta
Erich


On Thu, 17 Jan 2019 at 07:16, Mike Borgelt < [email protected]
<mailto:[email protected]> > wrote:

When circling in a thermal, do you 

a) keep the string centered

b) fly with it pointing to the outside of the turn

c) why?



Your technique may not be doing what you think it is.

Mike







Borgelt Instruments - design & manufacture of quality soaring
instrumentation since 1978

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