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Metal Roofing from A(luminum) to Z(inc) Part VI: Attachment of Metal Panels

February 13, 2009

Editor’s Note: This is the sixth article in a
multipart series about metal roofing in
today’s market. The series provides an indepth
look at materials and their uses,
coatings, system designs, and installation
techniques. It is reprinted with permission
of metalmag.
In previous A to Z articles, we have
looked into history, materials, finishes, fabrication
equipment, panel profiles, and
standing seam types. In this article, we look
at panel attachment and how it provides the
necessary wind resistance while still allowing
panels to respond to thermal loads. We
also look at “panel pinning”—where and
how it is done.
Wind Effects and Testing
Metal panels that
comprise the finished
surface of a roof constitute
an airfoil of sorts. As
wind buffets the walls of
the building, it is redirected
up and over the roof.
As this happens, negative
pressure (suction) is created
over certain zones of
the roof surface, producing
“lift” or “uplift.” This is
the same dynamic that
makes airplanes fly, and
the effect can be quite
exaggerated, threatening
to tear the roof from its
mounting. The frequency
and strength of the metal
panels’ attachment, consequently,
can be vital to
roof survival during a windstorm.
Wind is measured by its speed in miles
per hour, but those units of measurement
are not useful to design structures and
roofs. The forces that are exerted on the roof
surface are determined by taking the highest
historical wind speed and translating it
into pounds of pressure per square foot of
roof surface. This involves a number of
tables, equations, and variables that
include the height of the building and other
size factors as well as the exposure factor
from the effects of the surrounding terrain
or nearby buildings.
The ASCE-7.05 design standard is the
most widely accepted engineering standard
to determine the relative effects of these
variables. The standard divides the roof into
“zones,” each of which will experience different
uplift forces resulting from the same
wind speed (Figure 1). Corner zones are
where the wind effects are the greatest.
Perimeters are next, along with ridges on
steeply sloped roofs. The “field” of the roof is
where wind suction effects are the least.
The resistance of panels and attachments
to the uplift forces to which they will
be exposed is either calculated or tested.
More design parameters and specifications
require testing rather than structural engineering
calculation. Recognized test methods
include Underwriters Laboratories UL
580, Factory Mutual 4471, and ASTM E
1592.
These tests use various methods of
inducing static pressure on the roof assemblies
in an attempt to quantify their performance.
Most of them are designed and
intended for structural
panels (panels installed
over open support framing).
In my opinion, they
generally produce conservative
results compared
to the real-world effects of
wind on a roof surface.
This has to do with conservatism
within the
design standard and test
methods as well as the
inability of any test to
replicate the unusual
“microbursts” that wind
produces on the surface
as opposed to prolonged
sustained pressures.
Some ongoing tests at
Mississippi State Uni –
versity (Figure 2) using
Figure 1 – Zones 1, 2, and 3 each have pressure coefficients that vary with
other aspects of the structure. Zone 3 experiences the greatest pressure; Zone
1, the least. Zones near the ridge are nonexistent when the slope is below 7
degrees.
F E B R U A RY 2009 I N T E R FA C E • 1 1
electromagnetic fields rather than air pressure
are getting closer to the real effects of
wind on structural metal panels; however,
testing of this type is too costly to be adopted
as an industrywide procedure. The
effects of wind on a roof surface that is
installed over a deck are known to be mitigated
to some degree, but the industry tests
noted here cannot reflect this, and indeed
some of them do not enable testing of these
“nonstructural” panels over solid decks.
(See Figure 3.)
Because each test is very specific in
terms of the material and assembly particulars,
a manufacturer testing a new roof
product may have to go through a battery of
tests for each gauge, panel width, and
material that he wishes to market. This can
mean dozens of tests costing thousands of
dollars each. Such repetition is necessary,
however, as there are many variables in
actual assemblies. Those variables include
the gauge and mechanical properties of the
material, geometric shape of the seam and
profile, dimensions of the seam, strength of
the clip or other attachment, and width of
the panel. The metal roof assembly is a
chain, in essence, with the weakest link
representing the point of failure. Changing
one of the variables means increasing or
decreasing the strength of one of the links.
But doubling the strength of one link does
not necessarily double the strength of the
chain—the failure point just moves to a different
link.
Panel Attachment
Panels are attached with either exposed
or concealed fastenings. Exposed fasteners
are used for certain panel types, including
ribbed and corrugated profiles. This “direct”
method of attachment can provide in –
creased wind resistance but it does not provide
for thermal movement of panels and
has the obvious disadvantage of penetrating
the weathering surface.
Such methods and systems must be utilized
with some precaution for these reasons.
When the structure to which they are
attached consists of wood or steel purlins,
thermal cycling is relieved to some extent by
flexure or rotation of the purlins. When
these systems are used over solid wood
decks or bridged bar joists, however, fastening
fatigue can result from repeated thermal
cycling. It may, therefore, be a good idea to
limit roof lengths for such applications, as
thermal movement is directly related to
length. Hundreds of years ago, brakeformed
shapes were all fix-cleated to the
structure, but their end-to-end joining was
done with loose locks; and pan lengths were
short, so thermal movement was never
accumulated. Now, with roll-forming methods,
panels have gotten considerably longer.
Most (not all) “concealed fastening” provides
for differential thermal movement of
panels to structure by the interface of the
clip with the panel (Figure 4). A simple clip
design would have this interface be a frictional
engagement wherein the clip is rigidly
attached to the building structure but
slip-connected to the male seam component
of the panel. This one-piece clip method is
quite popular with most steep-slope roof
Figure 2 – Research funded by the Metal Building
Manufacturers Association (MBA) and the Amer i –
can Iron and Steel Institute (AISI) is ongoing at
Mississippi State University. It utilizes electro –
magnetic fields to more accurately replicate the
effects of wind on a roof surface.
Figure 3 – Design begins with the fastest three-second gust as measured “on the
ground” (33 ft above and lower). Because of ground friction, as building heights increase,
wind speeds also increase; hence, a roof on a 100-ft-tall building will experience more
severe wind effects than a one-story construction. For related reasons, surrounding
construction and topography also play a role, resulting in different “exposures.”
Figure 4 – Concealed fastened panels
eliminate most fasteners from the
weathering surface by using hold-down
clips inside the side-seam joint. The clips
permit thermal movement, but because the
“flat” of the panel is unrestrained, wind
resistance is diminished. Under load, the
panel flat arcs upward, rotating the seam
and disjointing.
12 • I N T E R FA C E F E B R U A RY 2009
products, especially those that have “snaptogether”
seam types. The clip is stationary
but allows for differential movement
between panel and clip (Figure 5).
When sealants are used within a panel
seam, often the clip design shown in Figure
5 cannot work. This is because the differential
movement between the panel and clip
would abrade the sealant, jeopardizing
weather integrity of the seam. In such
cases, a different clip design must be
employed. The most popular designs for
such a seam involve dual component clips.
The clip base is attached rigidly to the
structure, and the
clip top folds into
the panel seam.
Differential movement
then takes
place within the
clip itself, be tween
its two com po –
nents—base and
top. It bears mentioning
that the
clip is an integral
part of the assembly and unique in most
cases to the panel with which it is used.
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Figure 5 – One-piece clip designs provide for thermal cycling
by a sliding engagement of the panel seam. The differential
movement takes place between panel and clip.
Figure 6 – Most two-piece clip designs provide for
differential movement within the clip itself. The base
is fixed to the structure, and the top folds into the
panel seam. The top does not move relative to the
seam, preserving the integrity of seam sealants.
F E B R U A RY 2009 I N T E R FA C E • 1 3
Panel Fixity
Clip fastenings that allow the panel to
cycle freely in response to thermal loads
also make it necessary to deliberately “pin”
or “fix” the panel at some point along its
length to prevent it from migrating out of
position. Gravity or “drag loads,” as they are
sometimes called, will act in a direction parallel
to the roof’s surface, trying to pull the
panel down the slope of the roof (Figure 7).
These primarily comprise vertical loads
(mostly snow) on the roof’s surface. The
only resistance to them (other than the panels’
designed point of fixity) is the frictional
resistance of the clip attachment and the
friction between panel and structure. (See
sidebar on page 17 on calculating drag
loads.)
Panel fixity can be accomplished by
using one or more “fixed clips” or by some
method of direct
panel fastening at
that location. Use of
fixed-clip methods
depends upon the
nature of the interface
of clip to panel
seam; with some
designs, it is not possible.
The location of
choice for fixity of
steeply sloped architectural
systems is at
the ridge, where
exposed fasteners can
be hidden beneath a
ridge cover. These
systems will then
accumulate movement
at their eave end.
Conversely, the popular point of fixity
for low-slope systems is at the eave. The primary
reason for this preference is that such
systems are often hydrostatic
by design, and it is much easier
to waterproof a joint that is
stationary than one that
moves. Such a system will
then accumulate thermal
movement to the ridge where a
“bellows”-style ridge flashing
can accommodate differential
movement of the two opposing
roof planes while maintaining
a hydrostatic seal.
These statements are not
meant to be exclusive, as there
are exceptions in both cases. It
is also possible to see a panel
fixed at its midpoint, dividing thermal
movement in half by sending it in both
directions rather than one.
Having chosen a point of fixity for the
metal panel system, it then becomes critical
to ensure that such a point is singular
(Figure 8). In other words, the panel should
not be pinned inadvertently at any other
point along its length. To do so would likely
produce a failure of some sort. On occasion,
the thermal movement integrity of a roof
system is violated because some construction
detail or roof accessory mounting did
not preserve this characteristic (Figures 9
and 10). Design and as-built construction
should be scrutinized in this regard. A fascia
break detail, for example, fixes the panel
at the point of the break; to fix it again at its
opposite end would constitute dual pinning.
How Does Thermal Movement Occur?
As metal panels get hot, they expand,
increasing their length. When they get cold,
they contract, reducing that dimension.
Figure 7 – If a panel is not “fixed” at some location, gravity or “drag loads” can pull it down
the slope of the roof.
Figure 8 – The point of fixity may be at the ridge, the
eave, or some midpoint. It is crucial that this point is
singular, e.g. that “dual pinning” does not occur. Figure 10 – Detail avoiding panel pinning.
14 • I N T E R FA C E F E B R U A RY 2009
Figure 9 – Often, when a pipe is flashed through a steep
roof product over a deck, it results in panel fixity. To
avoid this, the deck should be overcut as shown.
This cyclical changing of dimension is called thermal
movement. This is a linear effect. In other words, it will
accumulate in direct proportion to the panels’ “unbroken”
length. If panels are joined end to end with
mechanical fasteners through the lap, then the unbroken
length is the total length of two or more panels, not
just one.
Thermal movement does not accumulate
across the width of the panels because
the unbroken length in that axis is so small.
The geometry of panels and their joining
method at side joints allow flexure at each
joint so that the thermal effects never accumulate.
Small, unitized metal covering
products, such as shingles, minimize
unbroken length dimensions; hence, thermal
movement is rarely a consideration for
such systems (Figures 11 and 12).
Total (or worst-case) thermal movement
is calculated by extending the material’s
coefficient of expansion over its length and
anticipated in-service temperature range
throughout its service life. It is the surface
temperature of the material and not ambient
air that affects these extremes.
The maximum high-end temperature
will be conditioned by the color of the panel
and its solar absorption characteristics
(lighter colors and high-gloss finishes will
be cooler than dark colors and low-gloss
finishes). A dark-colored panel with low
gloss at right angles to the summer sun can
approach temperatures of 200˚F.
In cold winter nighttime scenarios, the
low extremes of surface temperature can
actually dip 25˚ or 30˚ below ambient air.
This is due to the principles of radiant ener-
Figures 11 and 12 – In the early days of metal roofing,
pan lengths were short, so thermal movement never
accumulated. As the “unbroken length” of panels
increases, so does the dimensional gain or loss due to
differences in surface temperature.
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F E B R U A RY 2009 I N T E R FA C E • 1 5
gy. Skyward-facing objects
radiate heat energy
to the night sky. As this
energy transfer occurs,
the material loses BTUs,
reducing its temperature.
It is this same effect that
results with dew or frost
on the ground, roof, or
windshield of your car. It
is a combination of these
factors that can result
with delta figures of close
to 250˚F in cold northern
climates (Figure 13).
Because building
struc tures are not directly
exposed to direct solar
gain or nighttime radiation,
they do not expand
and contract at the same
rate as roof panels.
Additionally, the structure
is often a different
material with a different
coefficient of expansion.
Hence, differential movement
of the roof panels to
the structure or deck to
which they are mounted
must be accommodated. If the roof moves
an inch and a half but the structure only
one-half inch, then differential movement of
one inch must be provided by the clip
attachment. Often, the structure is a conditioned
element inside the insulated building
envelope. When this is the case, it experiences
no change in temperature and, therefore,
no change in length. This means that
the differential movement between roof and
structure is equal to the total movement of
the roof, with no offsetting or mitigating
thermal cycling of the structure.
It bears mentioning that it is not unusual
to see about 80% of this theoretical calculated
thermal movement actually used in
design. Panels distort a bit; structural
mountings or members may be deflected
and strained, but roofs don’t seem to fail.
On the other hand, if thermal movement
calculations are based upon ambient air,
they will often be only 50% of the correct
extremes, and I have seen these fail—
repeatedly. A single metal panel exerts
forces measured in tons when it tries to
move thermally; hence, a restriction of this
anticipated movement could precipitate
attachment fatigue and failure.
I have also seen engineers who try to
prove that the panel will undergo a “buck –
Figure 13 – Different metals have different expansion coefficients. Note that aluminum will gain or lose about
double the dimension of steel when subjected to the same temperature differences.
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16 • I N T E R FA C E F E B R U A RY 2009
ling” failure before
the attachment will
fail. In other words,
it will hump up, oilcan,
or otherwise
move out of plane to
relieve the thermal
forces. The trouble
with this theory is
that a member only
buckles in compression
(during an
expansion cycle).
Most attachment
fatigue and failure
occurs in tension
(during cold-cycle
contraction).
Manufactured
clips usually include
some mechanism to
ensure that they are
centered at the time
of installation. In
theory, the roof panels
are installed
somewhere in the
mid-range of their
in-service extremes.
Although it may not
be exactly at the
halfway mark, common
practice does
not compensate for
exact temperatures
at installation. It is absurd to suppose that
installers will move clips to some predetermined
location contingent upon installation
temperature. Even if they did, the temperature
is likely to be different when the
mechanical seaming is done. Most clips find
their own “centering” within the range of
thermal cycling of the roof within the first
few months of service.
Example of “drag load”
calculation. Drag loads should
be calculated in order to verify
adequacy of the panels’ method
and frequency of fixity. In this
example, the fixity point should
resist 1,069 pounds for each
panel (plus safety factors).
www.rci-online.org
F E B R U A RY 2009 I N T E R FA C E • 1 7
Rob Haddock is president of the Metal Roof Advisory Group,
Ltd., and a well-recognized authority on metal roofing. He is
a consultant, technical writer, training curriculum author,
inventor, and educator. Haddock is a member of NRCA,
ASTM, ASCE, ASHRAE, MBCEA, and MCA. He has been a
course author and instructor of RCI classes and a course
instructor for the University of Wisconsin School of
Engineering. He is also a recipient of RCI’s Horowitz Award.
Rob Haddock