10
make it turbulent, which may be heard as wind
noise, particularly because it can excite the
organ-pipe resonances of the tube.
Far more serious problems occur when laminar
airflow tries to leave the tube at high velocities.
If the curvature of the diffuser (flare) is too
sharp, the minimal momentum of the air at the
base of the laminar boundary layer is insufficient
to pass the resulting sharp, adverse pressure
gradient without stopping or stagnation. Slightly
downstream, the pressure gradient (higher
velocity with lower pressure to lower velocity
with higher pressure) causes the flow at the
base of the boundary to reverse and a turbulent
eddy is created in the form of a rotating torus
(this is how smoke rings can be blown). The
boundary layer now becomes the region that is
between the eddy and the main flow, but it has
now separated from the surface of the diffuser.
It tries to follow the pressure gradient formed by
the turbulence, but may form more eddies trying
to do so, and so on.
The turbulent wake thus created is responsible
for the ‘chuffing’ noises that even gently flared
ports can produce under some conditions.
The separation can sometimes be so extreme
that a turbulent jet can hit a listener at some
distance from a speaker. The aerodynamics
of reflex ports is actually rather complex and
somewhat unusual in that it involves alternating
flow in two different pressure regimes (at and
below port resonance), three octaves of the
frequency spectrum (different systems have
different tunings), completely indeterminate
starting conditions and well over 100dB of
level difference.
Aerodynamics research into reflex ports at B&W
is still in its infancy. Classical wind tunnel work
is very difficult because the alternating flow
makes a mockery of smoke trails. Recent work
with Computational Fluid Dynamics has shown
that ports are very difficult to model accurately.
This is partly because of the large number of
variables, and also because the flow regime is
influenced so heavily by small-scale turbulence
creation, which is less well understood than
large-scale fully-developed turbulence (more
is known about how aircraft stay in the air than
how midge flies do). Therefore, work has been
largely empirical, using comparative rather than
11
The movement of air in and out of tuning ports,
which may represent quite a considerable
physical displacement, often causes ‘chuffing’
noises as the air interacts with the discontinuities
found at the internal and external ends of the
port tube. These noises occur as turbulence is
formed at the discontinuities. Even when the
inside and outside ends of the tube are given
smoothly rounded profiles, the problem is not
totally cured, though it is mollified.
The reflex port is a well-established device to
improve the bass response of a transducer in
an otherwise sealed box of finite dimensions.
As the power handling, excursion and linearity
of bass drivers have steadily improved over the
years, the limitations of a simple tuned port
have become apparent. At low levels the
behaviour of the air in the tube can be correctly
approximated to a solid piston bouncing on
a known air volume and at a specific tuning
frequency; a readily predictable and essentially
acoustic problem. At higher levels, aerodynamic
effects become increasingly important and the
associated loss means that a given rise in bass
driver input level will yield a smaller rise in clean
port output level. This also means that the port
is not reducing the excursion of the bass driver
as effectively and the system will thus behave
increasingly like a lossy sealed box design; the
combined effect is known as ‘port compression’
and can often create an ultimate ceiling to
achievable bass levels.
Well before any ceiling is reached, the energy
losses associated with port compression cause
problems and it is the way energy is lost rather
than the amount lost that causes serious
acoustic problems. At very low velocities, and
with a perfect entry, air travelling through a real
port tube will pass smoothly along streamlines,
which do not interfere with one another. Close
to the walls of the tube is a thin boundary layer
caused by skin friction, with a relatively high
velocity gradient. It provides the transition
between the stationary walls and the moving air.
Laminae of air rub against each other causing
pressure drag through noiseless viscous losses.
These are minimal at low levels but increase at
a geometric rate in proportion to velocity. At
high enough velocities, if the tube is excessively
long and rough (or just very rough), the high
shearing energies in the boundary layer can
Flowport
7 Representation of streamlines exiting port flare.
a Laminar airflow following curvature of flare
b Higher velocity turbulent airflow separates from surface
of flare causing large scale eddy formation
c Small scale turbulence due to dimples encourages
laminar streamlines to remain attached to boundary
a
b
c
absolute benchmarks, because it is difficult to
make reliable measurements of turbulent noise.
Theoretical predictions of air velocities down
the port were checked with a new Doppler
measurement system, to establish the kind of
flow regime operating around chuffing levels in
terms of the Reynolds number (a dimensionless
indicator of turbulence levels). This showed that,
with care, it was possible to maintain laminar
flow down the port tube, but that air could
detach from the flares at fairly modest levels.
Simply making the flares more gentle would
not guarantee silence.
Anyone studying aerodynamics will soon learn
that turbulence is not always a problem. In fact,
many aerodynamicists engineer turbulence to
their advantage (indeed, some aircraft would
not stay in the air without it). If a boundary layer
is turbulent prior to the stagnation point it will
be less inclined to separate because the base
layer has increased kinetic energy. This means
that the surface flow can be swept further
downstream before pressure conditions
stagnate it and the lower pressure in the layer
that results from the higher velocities within the
eddies adheres the main flow to the surface
profile better. Thus, small-scale turbulence can
be used to delay the large-scale turbulence
caused by separation.
Artificially creating turbulence in the air moving
down the tube can delay the onset of chuffing
to higher bass unit input levels, but problem
wind noise happens far earlier, especially when
turbulent air is sucked back in to the port as the
flow alternates. In addition, the thickened boundary layer effectively constricts the flow, causing
pressure drag and thus airflow compression.
This constriction also alters the effective area
of the port, which in turn affects the Helmholtz
tuning. Thus it is otherwise desirable to delay
the onset of turbulent flow down the tube to as
high a level as possible. A more optimal solution
would thus be to use a smooth tube and limit
artificial turbulence creation to the problematic
stagnation area. (figure 7)
It is quite easy to produce turbulence where
it is needed; aircraft use vortex generators,
(vertical strakes) ahead of separation points.
These strakes project into the main flow and
are very effective, but when the same technique
is applied to port flares it creates too much
wind noise at lower levels.
Enter the golf ball. It can travel twice as far
as an equivalent smooth ball because of its
distinctive dimpled surface. The dimples are
very carefully shaped to produce tiny separation
points and favourable conditions for the creation
of vortices within them. The ball is thus covered
by a thin turbulent boundary layer that moves
the separation point further round the ball. This
decreases the ball’s wake and hence its drag,
and it was this technology that was used to
improve the performance of the port flares.
Because a round port flare is axisymmetric,
it was first thought that a series of rings with
the cross section of a dimple might work (and
be easier to prototype). However, the regular
vortices formed simply became the new separation points and at lower levels there was audible
wind noise because they were so abrupt. So
real, pseudo random dimples were tried on
the surface of the flare. These immediately
improved the chuffing phenomenon as
predicted, but there was still wind noise caused
by deep dimples at the edge of the tube where
flow velocities were highest. These were filled
but at the expense of earlier separation levels.
A process of experimentation refined the size,
shape and distribution of the dimples to
maximise headroom and minimise wind noise.
Small, smooth dimples are thus used where
velocities are highest and larger, more abrupt
dimples are used where velocities are lower.
This greatly refines the exit flow regime and also
ensures that a minimum of turbulence is carried
back down the tube when the flow is reversed.
It was found unnecessary to make the dimples
totally random over the whole flare, but as long
as they are locally irregular, perceptible wind
noise is incoherent and unobtrusive.
In the case of the 800D, the port is down firing,
so more wind noise is acceptable and the
dimples are optimised for maximum high level
flow. In use, the dimpled ports delay the
nuisance chuffing noise to significantly higher
levels. However, and perhaps of even greater
importance, when large-scale separation does
occur the resulting turbulence is far more
incoherent and thus less apparent. A reduction
of 6dB in certain regions of the noise spectrum
was measured, particularly around the problem
organ pipe frequencies. Port compression is
also decreased and the tuning frequency is
more stable at higher levels.
Having achieved excellent cabinets for each of
the drive units independently, it is important that
vibrations and radiation from each driver do not
leak into the enclosures of others. Decoupling
has been used extensively in the 800D to isolate
drive units, apart from bass units, from their
enclosures and the individual enclosures from
one another. A discussion of the technique can
be found in Appendix VIII.
Decoupling was not used for bass or bass/
midrange units in the Series. While it has the
potential for reducing vibration in cabinet walls,
listening tests have always confirmed that
this is more than offset by a reduction in the
speaker’s ability to portray ‘slam’. A similar
effect is noticed if the bass cabinet is not firmly
anchored to the floor, for example using spikes.
It should be noted that it is only bass drive units
that are required to operate in the stiffness
region, below their fundamental resonance
frequency. All others operate entirely in the
mass controlled region.
Decoupling
8 Gel gasket used for vibration isolation between tweeter and
midrange enclosures