On Jan 1, 2015 1:36 PM, "Mac McConnell-Wood via KRnet" <krnet at list.krnet.org>
wrote:
>
> Avro's should have read that before designing the Vulcan air
> brakes....fancy putting those solid slabs upwind of the flying controls..!
>
> See the pairs of yellow lines indicating position.
>

That main control surfaces on a Delta wing is way out of the turbulence of
the air brake...

The vert is humongous!

> Regards and a HNY to all our readers
> Mac
>
> On Wed, Dec 31, 2014 at 1:19 PM, Mike via KRnet <krnet at list.krnet.org>
> 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 <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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