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EXAMPLES TO ILLUSTRATE
THE DIFFERENCES BETWEEN THE 1997 UBC AND THE
2002 MSJC CODE
PART II: IN-PLANE LOADS
ON MASONRY WALLS
INTRODUCTION
The previous issues of
"Masonry Chronicles" highlighted the differences
between the masonry design provisions of the
1997 Uniform Building Code (1997 UBC) and
Building Code Requirements for Masonry
Structures: ACI 530-02/ASCE 5-02/TMS 402-02
by the Masonry Standards Joint Committee (MSJC
Code.)
This issue will provide
examples for the design of masonry walls for
in-plane loads. The examples will be done using
both the method prescribed by the 1997 UBC and
the method prescribed by the MSJC Code with
major differences pointed out in the MSJC
Example. Since the 2003 International Building
Code (2003 IBC) references the MSJC Code,
modifications to the MSJC Code in the 2003 IBC
that effect design will be mentioned.
The examples used in this
issue are modified from examples used in Seismic
Design of Masonry Using the 1997 UBC, by
Ekwueme and Uzarski.
DESIGN OF WALL TO
RESIST IN-PLANE FORCES
In order to compare the
design of CMU walls to resist in-plane loads, a
typical 10" (nominal) CMU wall (f
'm=2500 psi) ) from a 6-story
residential building will be designed. The
average wall height is 10-feet. The loads on the
wall to be designed are given in Table 1.
TABLE 1 LOADS ACTING ON
EXAMPLE WALL FOR IN-PLANE SHEAR
|
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Dead
(kips)
|
Live(kips)
|
V(kips)
|
M(kip-ft)
|
|
Roof
|
38
|
2
|
87
|
870
|
|
5th
|
76
|
5
|
180
|
2670
|
|
4th
|
114
|
9
|
253
|
5200
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|
3rd
|
152
|
12
|
306
|
8260
|
|
2nd
|
190
|
15
|
339
|
11650
|
|
1st
|
228
|
17
|
354
|
15190
|
Comparison of
Working Stress Design of In-Plane Loads
Between the 1997 UBC and the MSJC
Code
The factored loads on the
wall for Working Stress Design are given as:
 
The design of in-plane loads between the 1997
UBC and the MSJC Code differs mainly in the
inclusion, in Section 2107.1.7 of the 1997 UBC,
of a 1.5 multiplier when calculating shear or
diagonal tension stresses in Seismic Zones 3 and
4. This multiplier is not included in the MSCJ
Code.
Thus, if we assume the
distribution of reinforcement in the sample wall
is as shown in Figure 1. Then,
 

FIGURE 1 REINFORCEMENT
FOR WORKING STRESS DESIGN
The shear stress on the
wall is given by:
 
Equation
(7-37)
At the first
story,
 
Thus, when shear
reinforcement is provided per Section 2107.2.17
of the 1997 UBC:
 
Equation
(7-22)
A one third increase is
allowed in Working Stress Design by the 1997 UBC
for short-term loads. Thus,
 
The shear stress on the
wall exceeds the allowable shear stress using
working stress design per the 1997 UBC. To
satisfy the shear requirement the wall thickness
should be increased or masonry with a higher
compressive strength should be used.
Since the MSJC Code does
not use a similar multiplier in the calculation
of shear stress in Working Stress Design, the
shear stress on the same wall is given
by:
 
Equation
(2-19)
At the first
story,
 
Thus, when shear
reinforcement is provided per Section 2.3.5.3 of
the MSJC Code:

Equation
(2-25)
When the wall is designed
according to the MSJC Code the wall has adequate
shear strength to resist the loads. Note,
however, that the 1.5 multiplier is required by
Section 2106.5.1of the 2003 IBC.
Strength Design for
In-Plane Loads Using the 1997
UBC
The factored loads on the
wall for Strength Design are given
as:

Combination 1

Combination 2
For both
combinations:
 
The area of distributed
steel required in the wall can be estimated
by:
 
If we use only jamb steel,
the required area of reinforcing steel can be
estimated by (assuming ):
 
Using a combination of
distributed steel and jamb steel, we can try
8-#9 at each end (
) and 2-#5 @ 16" o.c. for the rest of the wall (
),
as shown in Figure 2.

Figure 2 Vertical
Reinforcing Steel in Example Wall
To obtain the moment
capacity of the wall under various axial loads,
an axial load-moment interaction diagram of the
wall, with the selected reinforcement, has to be
created. For simplicity, three control points
will be located on the interaction diagram. This
is a conservative approximation; a more accurate
curve can be obtained by calculating more points
on the interaction diagram.
With no eccentricity of
axial load (Control Point 1) and masonry with a
compressive strength of 2500 psi (Section
2108.2.5.4 of the 1997 UBC):

...Equation (8-34)
 
The wall axial load is
limited by Equation (8-35):
 
For Control Point 2, which
has no axial load, we iterate to obtain the
neutral axis of the section so that the sum of
vertical forces equals zero. A rectangular
compressive stress block, with a maximum usable
compressive strain of 0.003 is used for the
masonry, as stipulated in Section 2108.2.1.2 of
the 1997 UBC. Using a spread-sheet for
calculating the in-plane moment in the wall with
no axial load, the neutral axis is located 38.45
inches from the extreme compressive fiber and
the moment on the cross-section is equal to
20708 kip-ft. A capacity reduction factor of
0.85 may be used for walls with symmetric
reinforcement and no axial load.
At the balanced strain
condition (Control Point 3), the strain in the
extreme compressive fiber is equal to 0.003 and
the reinforcing steel is just yielding as shown
in Figure 3. The neutral axis location is given
by:

Checking the equilibrium
of the wall cross-section with the given neutral
axis location, the balanced axial load is found
to be 3739 kips and the balanced moment is 41091
kip-ft. Figure 3 shows the interaction diagram
for the wall using the three control points
obtained.

FIGURE 3 INTERACTION
DIAGRAM FOR EXAMPLE WALL
When the wall failure mode
is in flexure, Section 2108.2.5.2 of the 1997
UBC stipulates that the flexural strength of the
wall should be at least 1.8 times the cracking
moment strength. This is to prevent a sudden
loss of strength in the section when the masonry
cracks during loading. For fully grouted hollow
unit masonry, the modulus of rupture is given
by:
 
Equation
(8-31)
The cracking moment
strength is equal to:
 
Equation
(8-30)
 
In-Plane Shear 1st
Story
Recall:
 
For a ductile flexural
failure mode, the shear capacity must exceed the
shear corresponding to development of the wall
nominal flexural strength. For load combination
(1), which has the larger axial load and thus
the larger nominal moment, the axial load is 337
kips. From the interaction diagram, the nominal
moment strength is estimated to be:
 
The shear corresponding to
this moment is equal to:
 
The required shear
reinforcement is obtained from Equation (8-39)
of the 1997 UBC:
 
If we try 2 layers of #4
bars spaced at 16 inches (
= 0.0026) the nominal shear in the region at the
base of the wall (where a plastic hinge may
form) is given by:
 
Thus, we do not expect
shear failure to occur, and the wall should
respond in a ductile flexural mode.
Since the nominal shear
capacity exceeds the shear corresponding to
development of the wall nominal flexural
strength, two shear regions exist as stipulated
in Section 2108.2.5.5 of the 1997 UBC. In the
region at the base of the wall:
 
For the region above half
the story height:

Table (21-K)
The shear strength is
given in Section 2108.2.5.5 of the 1997 UBC
as:
 
Boundary
Members
In Section 2108.2.5.6 of
the 1997 UBC Boundary elements are specified for
walls resisting in plane loads when the
compressive strains in the wall, determined
using factored forces and Rw
equal to 1.5, exceed 0.0015. Also the maximum
reinforcement ratio in the 1997 UBC is given as
0.5rb.
Note that in this section
the 1997 UBC refers to the obsolete Rw factor
that has been replaced by the
Rw factor in the 1997 UBC. As
discussed in Design of Reinforced Masonry
Structures by Brandow, Hart and Virdee,
published by the Concrete Masonry Association of
California and Nevada, a comparison of the old
Rw factor and the R factor (4.5 vs. 6 for
masonry bearing walls) results in using an
R of 1.1.
The design forces for the
bearing wall were calculated with an R
factor of 4.5. Since the check for boundary
members must be performed with an R of
1.1, the factored loads can be multiplied by
4.5/1.1 = 4.09. Then, boundary members are
required if the moment capacity of the wall at a
maximum compressive strain of 0.0015 is less
than 4.09Mu.
To calculate the moment
capacity at a maximum compressive strain of
0.0015, a linear masonry compressive
stress-strain curve should be assumed, with a
strain at peak stress of 0.002. Thus, a
triangular masonry compressive stress block can
be used to calculate the moment, and the stress
at the extreme fiber is then given
by:
 
Figure 4 shows the stress
and strain in the wall cross-section at a
factored axial load of 165 kips.
The moment about the
center of the cross-section is equal
to:
 
Thus, boundary members are
required. The minimum length of the boundary
members is three times the wall
thickness.
Strength Design for
In-Plane Loads Using the MSJC
Code
Recall that the factored
loads for Strength design are given as:

Combination 1

Combination 2
For both
combinations:
 
Similar to the 1997 UBC
example, we will try a combination of
distributed steel and jamb steel, 8-#9 at each
end (As = 8.0 in2) and
2-#5 @ 16" o.c. for the rest of the wall
(As = 9.92
in2).
The calculation for the
control points on the interaction diagram using
the MSJC Code is similar to the procedure used
for the 1997 UBC. However, the MSJC Code nominal
axial compressive strength calculation takes
into account slenderness of the wall by the
inclusion of slenderness dependent modification
factors. Also, the stress block for the MSJC
Code is equal to
(0.8)2f'mcb and the
maximum compressive strain in concrete masonry
is 0.0025 per Section 3.2.2 of the MSJC Code. In
addition, the strength reduction factor for
reinforced walls subjected to combinations of
flexure and axial load is taken as 0.9 per
Section 3.1.4.1 of the MSJC Code.

FIGURE 4 EQUILIBRIUM OF
CROSS SECTION
AT MAXIMUM COMPESSIVE STRAIN OF
0.0015
Control Point 1 occurs
where the wall experiences no eccentricity of
axial load. The axial capacity of the wall using
the MSJC Code is:
 
Equation
(3-16)
Where R is the
slenderness dependent modification factor.
Since, the slenderness ratio for the wall
is:
 
The slenderness
modification factor and nominal axial strength
are equal to:
 
And,
 
For Control Point 2, which
has no axial load, we iterate to obtain the
neutral axis of the section so that the sum of
vertical forces equals zero. A rectangular
compressive stress block, with a maximum usable
compressive strain of 0.0025 is used. The
neutral axis is located 43.1 inches from the
extreme compressive fiber, and the moment on the
cross-section is equal to 20575
kip-ft.
At the balanced strain
condition (Control Point 3), the strain in the
extreme compressive fiber is equal to 0.0025 and
the reinforcing steel is just yielding. The
neutral axis location is given by:
 
Checking the equilibrium
of the wall cross-section with the given neutral
axis location, the balanced axial load is found
to be 3023 kips and the balanced moment is 38960
kip-ft. Figure 5 shows the interaction diagram
for the wall using the three control points
obtained. Notice that the ultimate moment acting
on the wall is 86% of the reduced capacity per
the 1997 UBC and 82% of the reduced capacity per
the MSJC Code.

FIGURE 5 INTERACTION
DIAGRAM FOR EXAMPLE WALL
When the wall failure mode
is in flexure, Section 3.2.4.2.2.2 of the MSJC
Code stipulates that the flexural strength of
the wall should be at least 1.3 times the
cracking moment strength. This is to prevent a
sudden loss of strength in the section when the
masonry cracks during loading. For masonry
subjected to in-plane loads, the modulus of
rupture, fr, normal to the bed
joints shall be taken as 250 psi per Section
3.1.7.2.2 of the MSJC Code.
Thus, the cracking moment
strength is equal to:
 
Equation
(3-32)
 
OK
In-Plane Shear
1st Story
Recall,
 
Per Section 3.1.3 of the
MSJC Code, for a ductile flexural failure mode,
the shear design capacity must exceed 1.25 times
the shear corresponding to development of the
wall nominal flexural strength. For load
combination (1), which has the larger axial load
and thus the larger nominal moment, the axial
load is 337 kips. From the interaction diagram,
the nominal moment strength is estimated to
be:
 
The shear corresponding to
this moment is equal to:
 
The nominal shear
strength, as computed in accordance with Section
3.2.4.1.2 of the MSJC Code, includes both
masonry and steel shear strength for the entire
wall.

Equation (3-18)
Where Vn shall not
exceed the following:

Equation
(3-19)

Equation
(3-20)
The maximum value of
Vn for
between 0.25 and 1.00 may be
interpolated.
Since,
 
 
Per Section 3.2.4.1.2.1 of
the MSJC code, the nominal masonry shear
strength equals:
 
Equation
(3-21)
 
Try 2-layers of #4 bars
spaced at 16 inches. Per Section 3.2.4.1.2.2 of
the MSJC Code the nominal shear strength
provided by the reinforcement equals:

Equation
(3-22)
 
Given the strength
reduction factor for shear is 0.80 per Section
3.1.4.3 of the MSJC Code:

OK
Except that the nominal
shear strength, Vn, need not
exceed 2.5 times the required shear strength,
Vu.

OK
Thus, the wall should
respond in a ductile flexural mode. Note that
Section 2106.5.2 of the 2003 IBC specifies the
use of steel shear strength only in the base of
the wall for Seismic Design Category D when the
ductile flexural mode governs design.
Maximum Reinforcement
Percentages
Per section 3.2.3.5 of the
MSJC Code, masonry strain in shear walls is
limited to that which can be developed when
strain is limited to 5 times yield in the
extreme tension reinforcement. The calculation
of the equilibrium includes unfactored gravity
axial loads. In addition, the stress in the
tension reinforcement is assumed to be
1.25fy and the
strength of the masonry compression zone is 80%
f'm times 80% of the area of
the compression zone.
Using the limitations in
Section 3.2.3.5, the maximum masonry compressive
strain can be calculated using a trial and error
procedure.
Thus,
 
Since this value does not
exceed the allowable masonry strain of 0.0025
specified in Section 3.2.2 of the MSJC Code, the
reinforcement is adequate.
Conclusion
Working Stress Design for
in-plane loads using the MSJC Code allows for
larger shear capacities due to the exclusion of
the 1.5 multiplier for shear loads that is
included in the 1997 UBC. Strength Design for
in-plane loads includes several significant
differences between design using the 1997 UBC
and design using the MSJC Code. These
differences include the consideration of
slenderness in axial strength, the smaller
stress block, smaller maximum usable strain, and
larger strength reduction factors for axial load
and flexure. In addition, the shear strength
calculation using the MSJC Code for the entire
wall includes the contributions from both
masonry and steel. In the 1997 UBC, when the
ductile flexural mode governs design the shear
strength at the base of the wall includes only
the contribution of the steel. Finally, the MSJC
Code does not allow for the inclusion of
boundary elements to limit strain like the 1997
UBC. Instead the maximum reinforcement
percentage is limited to that which can develop
a strain of 5 times yield in the extreme tension
reinforcement and a maximum masonry strain of
0.0025.
This issue of "Masonry
Chronicles" was written by Melissa Kubischta of
Hart-Weidlinger.
Errata for "Summer
2003" issue:
In the calculation of
effective area, Ase, for the
MSJC Code designs, the modular ratio of
elasticity, n, should be:
not n = 25.8
This results in an
increase in the deflection and the ultimate
moment but does not affect the over-all design
of the section.
COMMING
SOON
2003
Design of Reinforced Masonry
Structures
Manual and CMD03 Computer Program
Look for announcements in late fall
regarding
details on our web site at www.
cmacn.org
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