Hi George, 

It?s not a ?Brit thing?. In geometry ?normal? is the expression used to
describe a line which perpendicular to a surface. In the case described in
the research paper, the flat plate was rigged in the wind tunnel so that it
was normal to airflow. On a KR fuselage, the bellyboard would only be normal
to the flow if it was deployed at 90 degrees.



Developing nations have no cause to feel inferior!



Have a good 2015.

Mike



  _____  

From: gluejam [mailto:gluejam at cox.net] 
Sent: 01 January 2015 19:05
To: Mike; KRnet
Subject: Re: KR> Bellyboard



Mike -  

Perhaps you can explain why in the report the term, "normal to the airflow"
rather 'than parallel with', or 'perpendicular to' the airflow is used.   Is
that a common reference in the UK?   It just seems a little nebulous to me
in understanding immediately upon reading the report, and it would seem
sensible to think that normal would be in line with airflow . . .  
but then ours (US) is a lower grade society, after all !!

George

  _____  



On 12/31/2014 6:19 AM, Mike via KRnet wrote:

A little science from English researchers in 1957
http://naca.central.cranfield.ac.uk/reports/arc/cp/0323.pdf but I'm sure
there must be more recent published findings from elsewhere.

This suggests that a solid airbrake produces a bubble of reduced airflow
behind the brake with airflow velocity fluctuations occurring around the
edge of the brake which may cause vibrations to the structure. Perforations
in the airbrake reduce this effect and were found to be more effective
towards the centre of the plate than around the periphery.

>From the Pprune forum, this explanation was offered: "Perforation reduces
buffeting downrange of the speed brake, and reduces its interference with
flying surfaces or the fuselage or wing or horizontal stab. Remember, the
speed brake is there to create drag, but not undesirable flight
characteristics. A perforated brake doesn't create nearly the airflow
disruption, pitch change, or load on the surrounding and supporting
structure that a solid brake might create. The number and placement of holes
are important considerations, and part of the design. Holes permit a lighter
structure that takes less of an airload, reducing not only the weight of the
brake assembly but the force required to actuate it and the structure around
it that must support the load. Remember that much of the time, that speed
brake isn't anything but dead weight." 

Mike Mold
Devon, UK. 

-----Original Message-----
From: KRnet [mailto:krnet-bounces at list.krnet.org] On Behalf Of Mac
McConnell-Wood via KRnet
Sent: 31 December 2014 10:35
To: Herbert F?rle; KRnet
Subject: Re: KR> Bellyboard

The RAF Vulcan bomber had solid airbrakes-no holes (which enabled this 90
ton delta to descend vertically-..been there..)
Mac

On Wed, Dec 31, 2014 at 9:51 AM, Herbert F?rle
<mailto:krnet at list.krnet.org> <krnet at list.krnet.org> wrote:



....any Test,however it is performed,gives a lot of informations! The
aerodynamic principles are always the same ,also in the case of the hot"
bellyboard -drag" discusion.For me it's important the location of the

board

and I think the place underneath the rearspar is very well chosen ( far
enough behind the CG ,to give the Kr a small amount of direction stability
like a dragchute and the waketurbulences does'nt hit the HS !) I 'm
convinced,a board without holes  are more effectiv ( one big

waketurbulence

produce more drag compared to many small ones).
I'm also think,a big advantage of the bellyboard is the fact ,that you can
lower the nose of the Kr on final for better sight( wether you have to

push

or pull the stik )!
Herbert
German Kr builder .


Von meinem iPad gesendet
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