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Abstract
Several
issues regarding multi-components seismic response analysis
of structures are addressed in this paper. The first issue
is related to the accuracy of the commonly used rules to
estimate the combined effect of the individual components of
earthquakes. The rules are studied for normal and principal
components, for local and global response parameters,
elastic and inelastic behavior and two and three components.
The critical orientation of the components is identified.
The second issue threats with the relative magnitude of the
effect of the vertical component with respect to those of
the horizontal components. Finally, the accuracy of
estimating the effect of the weaker horizontal component (RY)
as 85% of that of the stronger horizontal component (RX)
is studied. Results indicate that the total base shear is
reasonable estimated by the rules. However, they can
underestimate the combined response in terms of axial loads
for inelastic behavior. For the horizontal components the
SRSS rule is, in general, less conservative than the
30% rule. For the three components the 30% rule
is less conservative. It is concluded that if the
percentile rule is used to estimate the combined response a
value of 40% should be used instead of 30%. It is also
observed that the principal components give the maximum
response and that the ratio of the effect of the vertical
component to those of the horizontal components can be
significant and consequently should explicitly be used in
design. Values larger than unity are observed in some
cases. Results also indicate that the ratio of the effect
of the minor horizontal component to that of the major
horizontal component is much smaller that the typical
assumed value of 0.85. The value obtained in this study is
about 0.40.
Introduction
After
catastrophic damages during some recent earthquakes around
the world, seismic analysis and design procedures have been
significantly modified. Several methods with different
degrees of sophistication have been suggested in many codes
(IBC 2003, RCDF 2004) including the equivalent lateral force
procedure and several types of dynamic analysis procedures
(modal response spectra analysis, linear time-history
analysis, and nonlinear time-history analysis).
Our
understanding of the earthquake phenomenon has improved
significantly during the last years; however, there are many
issues that require our attention regarding its effects on
the response of structures. Energy released during an
earthquake travels in the form of waves. They are measured
in the form of two horizontal and one vertical translational
acceleration time histories. Although, earthquakes can
cause rotational excitations, they are not measured and are
completely ignored in the analysis. In addition, for
far-source ground motions, the effect of the vertical
component is usually smaller than those of the horizontal
components and is consequently neglected. Additional bases
to neglect the vertical component effect are that building
designs allow for gravity loads, which provides for a high
factor of safety in the vertical direction. Thus,
when we analyze a structure, we generally apply either one
assumed or recorded horizontal component in a specific way
or two components along the two major axes of the structure,
sometimes ignoring the orientation of maximum response.
Article
1620.2.10 of the IBC code (2003) states “The direction of
application of seismic forces used in design shall be, that
which will produce the most critical load effect in each
component. The requirement will be deemed satisfied if the
design seismic forces are applied separately and
independently in each of the two orthogonal directions.”
Later, in Article 1620.3.2 for the design of common
structures with various plan irregularities belonging to
Seismic Design Category C and D, IBC states “The critical
direction requirement of Section 1620.2.10 will be deemed
satisfied if one hundred percent of the forces in one
direction are added to the 30 percent of the forces in the
perpendicular direction. Alternatively, the effects of the
two orthogonal directions are permitted to be combined on a
square root of the sum of the squares (SRSS) basis. When the
SRSS method of combining directional effects is used, each
term computed shall be assigned the sign that will result in
the most conservative result.” The two combination
procedures discussed above will be denoted hereafter as the
30% and the SRSS combination rules,
respectively. The relative magnitude of the effects of the
components will be important in the relative accuracy of the
rules. Usually, the ratio of the effect of the minor
horizontal component is estimated as 85% of that of the
major horizontal component. The RCDF (2004) code states
similar requirements for the evaluation of the combined
responses of the seismic components. The codes however, do
not specify the type of effect or the type of structures to
be considered.
The above
discussions clearly identify several issues that need our
attention: (1) how to combine the separated responses in
different directions to obtain the overall response?, (2)
what is the critical orientation of the components?, (3)
what is the relative importance of the vertical component?,
and (4) what is the relative importance of the weak
horizontal component compared to that of the strong
horizontal component? These issues are studied in this
paper. To study them comprehensively, one possible
attractive option would be to estimate the response of
structures as accurately as possible, preferably by using
sophisticated three-dimensional nonlinear time history
analysis, and compare the results obtained by the simplified
practices. The comparison may increase our understanding
and may identify the limitations of the simplified
approaches.
Literature Review
The
critical orientation of the components as well as the ways
of combining their individual effects have been of interest
to the civil engineering profession.
Penzien and Watabe (1975) stated that the three components of an
earthquake are uncorrelated along a set of axes generally
denoted as principal axes.
The major principal axis is horizontal and directed toward
the epicenter, the intermediate axis is horizontal and
perpendicular to the orientation of the major component, and
the minor principal axis is vertical. The critical
response could be obtained when these components are
applied. López and Torres (1996) proposed a method to
estimate the critical angle of incidence. Smeby and Der
Kiureghian (1985) observed that, for response spectra
analysis of linear structures, when the two horizontal
principal components are not along the structural principal
axes, the effect of correlation is small and that if the two
horizontal components have identical or nearly identical
intensities, then the effect of correlation disappears. Newmark (1975) and Rosenblueth and Contreras (1977) proposed the
Percentage Rule to approximate the combined response as
the sum of the 100% of the response resulting from one
component and some percentage (λ) of the responses
resulting from the other two components. To combine the two
horizontal components, Newmark (1975) suggested λ to
be 40% and Rosenblueth and Contreras (1977) suggested
λ to be 30%. Wilson et. al. (1995) concluded
that the Percentage Rule could underestimate the design
forces in certain members. More recently, many other
studies attempted to combine the seismic responses due to
two or three components (Correnza and Hutchinson 1994,
Wilson et. al. 1981). These studies are limited in scope.
They used simple one-story or two degree-of-freedom concrete
structures.
Der Kiureghian (1981) and Wilson et. al. (1995) proposed the
Complete Quadratic Combination (CQC) rule to
combine modal responses due to a single seismic component.
Smeby and Der Kiureghian (1985) proposed an extension of the
CQC rule, known as the CQC3 rule to combine
modal responses due to the three seismic components. Smeby
and Der Kiureghian (1985) and Lopez and Torres (1996)
verified the application of the CQC3 rule by
considering building-type structures with rectangular
geometry. Menun and Der Kiureghian (1981) extended these
studies by considering more complex three-dimensional curved
bridge structures subjected to two horizontal components.
They compared the results of the CQC3 rule with those
of the SRSS, the 30% (λ = 0.3), and the
40% (λ = 0.4) rules and examined the
shortcomings of these three rules.
López et. al.
(2001) conducted a similar study to combine the two
horizontal components with a range of one-story systems with
symmetrical and unsymmetrical plan, and two multi-story
buildings. Hernández and López (2003) extended the work of
López et. al. (2001) by considering the effect of the
vertical component. They observed that if a principal
component does not coincide with the vertical direction, the
critical response could be underestimated.
Most of the previous studies on combination rules were
limited to elastic analysis applied to simplified plane
concrete frames connected by rigid diaphragms and/or only
few stories high. They did not consider the inelastic
behavior of the structural elements or the appropriate
energy dissipation mechanisms. In a typical strong-column
weak-beam (SCWB) moment resisting steel frame (MRSF),
plastic hinges are
expected to be formed in the weak elements.
Reyes-Salazar et. al.
(2000) found that SCWB steel frames are very efficient in
dissipating earthquake-induced energy. If a SCWB is modeled
as a frame with rigid diaphragms, one of the most important
sources of energy dissipation, i.e. dissipation of energy at
plastic hinges will be lost and the structural behavior will
be different. Numerical studies by Wang and Wen (2000)
showed that the response of SCWB steel buildings would be
significantly underestimated if they were modeled by
shear-beams assuming rigid diaphragms. Recently,
Reyes-Salazar et al. (2004) observed that both the 30%
and the SRSS rules could underestimate the combined
response and the energy dissipation mechanism should be
considered as accurately as possible. Thus, it is essential
that the SCWB steel frames should be analyzed as complex
multi-degree of freedom (MDOF) systems.
In this study, the four questions raised earlier, i.e., the
issues related to the combination of the individual effects
of the components, the critical orientation, the ratio of
the effect of the vertical component to those of the
horizontal components and the ratio of the effect of the
minor horizontal component to that of the major horizontal
component, are comprehensively addressed. The responses of
MRSF are specifically studied. To study the directionality
issue, the normal and principal components of an earthquake
are considered. Recorded horizontal time histories will be
denoted as normal components. When they are transformed to
uncorrelated components following the procedure suggested by
Penzien and Watabe (1975), they will be denoted as principal
components.
Combination Rules
The
combination rules are formally defined in this section. For
the ease of discussion, RX will represent
hereafter the maximum absolute load effect at a particular
location when the structure is excited by the horizontal
X component of a given earthquake. Similarly, RY
and RZ will denote the corresponding
maximum absolute load effect at the same location when the
structure is excited by the horizontal Y and the
vertical component of the earthquake, respectively. The
load effects produced by each component can be calculated
using many simplified methods including the equivalent
lateral load procedure, modal analysis, and time history
analysis. Then, the combined effect can be calculated as
the most unfavorable of:

The above
Eqs. represent the Percentage Rule. If λ =
0.3 is used, it represents the 30% rule for three
components. According to the SRSS rule the combined
response is given by

Despite
these rules seem to be simple to apply; there is no
indication in the codes on how to select the critical
directions for the seismic components nor the types of
effects to be considered. As stated earlier, Penzien
and Watabe (1975) observed that during the strong motion
phase of an earthquake the ground components are
uncorrelated along a well-defined orthogonal system of axes
defined as the principal axes of the motion. It could
represent the critical condition. The basic assumption of
the SRSS rule is that there is no correlation between
the orthogonal components.
Mathematical Formulation
The authors and their associates (Gao and Haldar 1995,
Reyes-Salazar 1997) developed an efficient finite
element-based time-domain nonlinear analysis algorithm,
which is used to estimate the effect of the seismic
components on the overall structural response. The
procedure estimates nonlinear seismic responses of steel
frames considering all major sources of energy dissipation.
Material nonlinearity and geometric nonlinearity are
considered. Considering its efficiency, particularly for
steel frame structures, the assumed stress-based finite
element method (Kondo and Atluri 1987) is used. Using this
approach, an explicit form of the tangent stiffness matrix
is derived without any numerical integration. Fewer
elements can be used in describing a large deformation
configuration without sacrificing any accuracy.
Furthermore, information on material nonlinearity can be
incorporated in the algorithm without losing its basic
simplicity. It gives very accurate results and is very
efficient compared to the displacement-based approach. The
procedure has been studied and verified with existing
theoretical and experimental results.
The
geometric and material nonlinearities are considered in the
tangent stiffness matrix. The mathematical details of the
derivation are not shown here, but can be found in the
literature (Kondo and Atluri 1987). The material is
considered to be linear elastic except at plastic hinges.
Concentrated plasticity behavior is assumed at plastic hinge
locations. In the past, several analytical procedures were
proposed to predict the deformation of elasto-plastic frames
under increasing seismic and static loads. However, most of
these formulations were based on small deformation theory.
In this study, each elasto-plastic beam-column element can
experience arbitrary large rigid deformations and small
relative deformations. Thus, in addition to the elastic
stress-strain relationships, the plastic stress-strain
relationships need to be incorporated into the constitutive
equations if a given yield condition is satisfied. Several
yield criteria have been proposed in the literature in terms
of stress components or nodal forces. Since the nodal
forces can be obtained directly from the proposed method,
the yield criteria used here is expressed in terms of nodal
forces. When the combined action of the resultant stresses
satisfies a prescribed yield function at a given end of an
element, a plastic hinge is assumed to occur instantaneously
at that location. Plastic hinges are considered to form at
the ends of the beam-columns elements. The yield function
depends on both, the type of section and loading acting on
the beam-column element (Mahadevan and Haldar 1991).

The
yield
function for three-dimensional beam-column elements has the
following general form:
where P is the axial force, Mx and My
are the bending moments with respect to the mayor and
minor axis, respectively, Mz is the
torsional moment,
sy
is the yield stress, and lp is the
location of the plastic hinge. For the W-type sections of
the models used in this study, this equation has the
following particular form:

where
Pn is the axial strength, Mnx
and Mny are the flexural strength with
respect to the major and minor axis, respectively and Mnz
is the torsional strength.
The
additional axial deformations and relative rotations
produced by the presence of plastic hinges are taken into
account in the stiffness matrix and the internal force
vector of the plastic stage. Explicit expressions for the
elasto-plastic tangent stiffness matrix and the elasto-plastic
internal force vector are also developed. The mathematical
derivations can be found in the literature (Kondo and Atluri
1987). Depending on the level of earthquake excitation, in a
typical structure, all the elements may remain elastic, or
some of the elements may remain elastic and the rest yield.
The structural stiffness matrix and the internal force
vector can be explicitly developed from the individual
elements and the particular state (elastic or plastic) they
are in. Based on an extensive literature review, it is
observed that viscous Rayleigh-type damping is commonly used
in the profession and is used in this study (Clough and
Penzien 1993). The
consideration of both the tangent stiffness and the mass
matrices is a rational approach to estimate the energy
dissipated by viscous damping in a nonlinear seismic
analysis. The mass matrix is assumed to be
concentrated-type. The step-by-step direct integration
numerical analysis procedure and the Newmark β method
(Bathe 1982) are
used to solve the nonlinear seismic governing equation of
the problem.
A computer program has been developed to implement the
solution procedure. The program was extensively verified
using information available in the literature. The
structural response behavior in terms of members' forces
(axial load, shear force and bending moment), total base
shear and interstory displacements, can be estimated using
this computer program.
Structural Models
To study the issues raised earlier, four three-dimensional
MRSF structures as shown in Fig. 1a, with different dynamic
characteristics, are considered. They are one, three, eight,
and fifteen story structures and will be denoted hereafter
as Models 1, 2, 3 and 4, respectively. The locations of the
columns are shown in Fig. 1b. For each model, four plane
frames are used as shown in Fig. 1a: two interior (Mxi
and Myi) and two exterior (Mxe and Mye).
The plane frames in both directions were designed according
to the UBC standards and then modified following the strong
column-weak beam (SCWB) concept. The seismic design load
was computed for seismic zone 4. The dead and live loads
were 5.8 and 2.9 kN/m2 (≈ 120 and 60 psf),
respectively. The member sizes are summarized in Table 1.
The story height for all the models is a constant of 3.66 m
and their bay width is 7.32 m in both directions. The
fundamental periods of the models in the major direction (X
direction) are 0.20, 0.47, 1.06 and 1.55 sec., respectively.
The corresponding values for the minor direction are 0.33,
0.73, 1.64 and 2.28 sec., respectively. In all these
frames, the columns are assumed to be made of Grade-50 steel
and the girders are of A36 steel. The columns are assumed
to be fixed at the base and the connections fully restrained
(FR).
The frames are modeled as MDOF systems.
Each column is represented by one element and each girder is
represented by two elements, having a node at the mid-span.
Each node is considered to have six degrees of freedom.
Thus, the total number of degrees of freedom for Models 1,
2, 3 and 4 are 240, 720, 1920 and 3660, respectively.
The four models are excited by twenty recorded earthquake
motions, as listed in Table 2, in time domain. They are
denoted hereafter as Earthquakes 1 to 20. Epicentral
distance (ED), Magnitude (M), peak ground acceleration (PGA)
and predominant period (T) are given in the table. The
damping is considered to be 5% of the critical damping; the
same damping is used in the codified approaches. As will be
discussed later in detail, the real earthquakes are applied
first and later they
are
scaled up in such way that produce approximately 1.5%
interstory displacement in all frames to study the inelastic
response.
Accuracy
of the Rules for the Horizontal Components
For the
ease of discussion, the following notations will be used in
the remainder of the paper. Numerically, an earthquake
excitation will be represented by three acceleration time
histories: two in the horizontal directions and one in the
vertical direction. The first component will be
denoted as X. The second and third
components will be denoted as Y and Z,
respectively. They will be denoted as Xn,
Yn and Zn when normal
components are used to excite structures, and as Xp,
Yp and Zp, if
principal components are used instead. Hence, the notations
(Xn, Yn, Zn)
indicate that the first, second and third
normal components are simultaneously applied to the major
horizontal, minor horizontal, and vertical directions of the
structure, respectively. The notations (Yp,
0, 0) indicate the structure is excited by only the
second principal component acting along the major structural
axis. In order to fulfill the objectives of the study, the
following cases of analysis are considered for each
structure, earthquake and elastic and inelastic behavior:


Table
1. Member sizes
|
MODEL |
FRAME |
STORY |
EXT COL |
INT COL |
GIRDERS |
|
1 |
Mxe |
1 |
W14x61 |
W14x90 |
W21x44 |
|
Mxi |
1 |
W14x99 |
W14x145 |
W21x68 |
|
Mye |
1 |
W14x61 |
W14x99 |
W16x31 |
|
Myi |
1 |
W14x90 |
W14x145 |
W16x45 |
|
2 |
Mxe
|
1-2 |
W14x74 |
W14x109 |
W21x83 |
|
3 |
W14x61 |
W14x90 |
W21x68 |
|
Mxi |
1-2 |
W14x120 |
W14x176 |
W21x122 |
|
3 |
W14x99 |
W14x145 |
W21x93 |
|
Mye
|
1-2 |
W14x74 |
W14x120 |
W21x50 |
|
3 |
W14x61 |
W14x99 |
W18x40 |
|
Myi |
1-2 |
W14x109 |
W14x176 |
W21x68 |
|
3 |
W14x90 |
W14x145 |
W21x57 |
|
3 |
Mxe
|
1-2 |
W14x109 |
W14x159 |
W21x122 |
|
3-4 |
W14x90 |
W14x132 |
W21x93 |
|
5-6 |
W14x74 |
W14x109 |
W21x73 |
|
7-8 |
W14x61 |
W14x90 |
W21x62 |
|
Mxi
|
1-2 |
W14x176 |
W14x257 |
W21x201 |
|
3-4 |
W14x145 |
W14x211 |
W21x147 |
|
5-6 |
W14x109 |
W14x159 |
W21x111 |
|
7-8 |
W14x82 |
W14x120 |
W21x83 |
|
Mye |
1-2 |
W14x109 |
W14x176 |
W21x73 |
|
3-4 |
W14x90 |
W14x145 |
W21x62 |
|
5-6 |
W14x74 |
W14x109 |
W18x46 |
|
7-8 |
W14x61 |
W14x82 |
W16x26 |
|
Myi |
1-2 |
W14x159 |
W14x257 |
W21x101 |
|
3-4 |
W14x132 |
W14x211 |
W21x83 |
|
5-6 |
W14x109 |
W14x159 |
W21x68 |
|
7-8 |
W14x90 |
W14x120 |
W21x50 |
|
4 |
Mxe
|
1-2 |
W14x233 |
W14x311 |
W21x248 |
|
3-4 |
W14x176 |
W14x257 |
W21x201 |
|
5-6 |
W14x145 |
W14x211 |
W21x166 |
|
7-8 |
W14x120 |
W14x176 |
W21x132 |
|
9-10 |
W14x99 |
W14x145 |
W21x111 |
|
11-12 |
W14x82 |
W14x120 |
W21x93 |
|
13-14 |
W14x68 |
W14x99 |
W21x83 |
|
15 |
W14x53 |
W14x82 |
W21x62 |
|
Mxi
|
1-2 |
W14x370 |
W14x500 |
W24x370 |
|
3-4 |
W14x311 |
W14x426 |
W24x306 |
|
5-6 |
W14x233 |
W14x342 |
W24x250 |
|
7-8 |
W14x193 |
W14x283 |
W24x207 |
|
9-10 |
W14x159 |
W14x233 |
W24x146 |
|
11-12 |
W14x132 |
W14x193 |
W24x117 |
|
13-14 |
W14x109 |
W14x159 |
W21x122 |
|
15 |
W14x82 |
W14x120 |
W21x93 |
|
Mye
|
1-2 |
W14x233 |
W14x370 |
W21x166 |
|
3-4 |
W14x176 |
W14x311 |
W21x132 |
|
5-6 |
W14x145 |
W14x233 |
W21x101 |
|
7-8 |
W14x120 |
W14x193 |
W21x83 |
|
9-10 |
W14x99 |
W14x159 |
W21x68 |
|
11-12 |
W14x82 |
W14x132 |
W21x57 |
|
13-14 |
W14x68 |
W14x109 |
W21x44 |
|
15 |
W14x53 |
W14x82 |
W16x26 |
|
Myi |
1-2 |
W14x311 |
W14x500 |
W21x223 |
|
3-4 |
W14x257 |
W14x426 |
W21x182 |
|
5-6 |
W14x211 |
W14x342 |
W21x147 |
|
7-8 |
W14x176 |
W14x283 |
W21x122 |
|
9-10 |
W14x145 |
W14x233 |
W21x101 |
|
11-12 |
W14x120 |
W14x193 |
W21x83 |
|
13-14 |
W14x99 |
W14x159 |
W21x68 |
|
15 |
W14x82 |
W14x120 |
W21x50 |
Table
2. Earthquake models

Case 1,
the structures are simultaneously excited by the three
normal components; the first component is acting along the
strong horizontal structural direction, the second one along
the weak horizontal structural direction and the third along
the vertical direction (Xn, Yn,
Zn).
Case 2,
same as Case 1, but the horizontal components are
interchanged (Yn, Xn, Zn).
This is another possibility of applying the normal
components.
Case 3,
the structures are simultaneously excited by the two
horizontal normal components; the first component is acting
along the strong horizontal structural direction and the
second one along the weak horizontal structural direction (Xn,
Yn, 0).
Case 4,
same as Case 3, but the horizontal components are
interchanged (Yn, Xn, 0).
Case 5,
the structures are excited only by the first normal
horizontal component applied to the strong horizontal
structural direction (Xn, 0, 0)
Case 6,
the structures are excited only by the second normal
horizontal component applied to the weak horizontal
structural direction (0, Yn, 0)
Case 7,
the structures are excited only by the third normal
horizontal component in the vertical direction (0, 0, Zn)
Case 8,
same as Case 5, but the second component is applied
along the strong direction (Yn, 0, 0).
Case 9,
same as Case 6, but the first component is applied
along the weak direction (0, Xn, 0).
Similarly, another nine cases of analysis are considered
when the principal components are applied. They are: Case
10 (Xp, Yp, Zp);
Case 11 (Yp, Xp, Zp);
Case 12 (Xp, Yp, 0);
Case 13 (Yp, Xp, 0);
Case 14 (Xp, 0, 0); Case 15
(0, Yp, 0); Case 16 (0, 0,
Zp), Case 17 (Yp,
0, 0) and Case 18 (0, Xp,
0). Cases 1 and 2 will give the actual
response for normal components since the three
components are simultaneously applied. Cases 10 and 11 will
give the actual response for principal components.
Thus, for four structures, twenty earthquakes, eighteen
cases, and considering the responses to be elastic and
inelastic, a total of 2880 analyses were required.
The
accuracy of the combination rules for the normal horizontal
components are specifically addressed in this section of the
paper. The structural responses obtained according to the
SRSS and the 30% rules are estimated and
compared to that given by the actual solution. For
the normal horizontal components the actual response
will be given by Cases 3 and 4 while the
combined response according to the rules will be obtained by
combining Cases 5, 6, 8 and 9. In
addition, the combined effect is calculated by using λ
= 40% instead 30%This additional combination rule will be
referred hereafter as the 40% rule. For comparison
purposes, the following error terms are defined:

where the
terms, 30% value, actual value, SRSS value,
and 40% value represent the combined effect according
to
l
= 30%, actual response, SRSS rule and
l
= 40%, respectively. A negative error in the above
equations implies that the combination rule under
consideration underestimates the combined effect of both
components. The errors are calculated for the axial loads
at ground level columns and for the total base shear for all
the models. Both, elastic and inelastic behavior are
considered. Results for elastic analysis are discussed
first. The errors for the axial load on columns of Model 1
are shown in Figs 2a through 2d. It is observed that both
the 30% and the SRSS rules reasonable
overestimate the response for most of the earthquakes. The
combined response is underestimated only in a few cases. In
general, the curve for the 30% rule is over the
corresponding curve for the SRSS rule. In other
words, the 30% rule is more conservative than the
SRSS rule. The errors for the axial load on columns of
Models 2, 3 and 4, are similarly estimated but are not
shown. The major observations made for Model 1, also apply
to these models.
The errors in terms of the total base shear for elastic
behavior are shown in Figure 3. As for the case of axial
loads in columns, both the 30% and the SRSS
combination rules accurately estimate the combined effect
for the total base shear. However, the errors are in
general smaller for the total base shear. The maximum
underestimation error is about –5% for a few cases. It is
observed that the scatter in the error values tends to
increase with the fundamental period of the frames. As for
the case of axial loads, the underestimation is more for the
SRSS rule than for the 30% rule.


Fig. 2.
Errors for axial load, Model 1, elastic behavior, normal
horizontal components
Fig. 4
shows the errors for the inelastic axial loads on columns of
Model 1. As for the case of elastic axial loads, both the
30% and SRSS rules may underestimate the
combined response. However, the number of cases and the
magnitude of the underestimation are larger for the
inelastic case. The underestimation error is larger than
–15% in many cases. This indicates that the results for
elastic analysis may be quite different from those of
inelastic analysis. The implication of this is that the
results obtained from elastic analysis of steel frame
structures subjected to strong motions may be a very crude
approximation. The errors in terms of axial load on columns
of Models 2, 3 and 4 are also estimated. The results are
similar to those of Model 1.


Fig. 3.
Errors for total base shear, elastic behavior, normal
horizontal components
The
errors for the total inelastic base shear are shown in Figs
5 for all the models. It is observed that, as for the case
of elastic base shear, the 30% and SRSS rules,
in general estimate the combined effect very well. The
errors are positive or relatively small in most of the
cases. The underestimation is always more for the SRSS
than for the 30% rule. In summary, whether elastic
or inelastic analysis is used the combined total base shear
is reasonably overestimated by the rules. However, the
combined response in terms of axial loads can be
underestimated for inelastic behavior. The errors when the
frames are excited for the normal components have been
considered so far. Similar plots to those of Figs 2
through 5 were also developed for the principal components.
But are not shown. The major conclusion made for normal
component also apply to principal components. Only the
average errors are presented as discussed below.


The
averaged of the errors are presented in Table 3 for normal
and principal components. Elastic behavior is first
discussed. It is observed that, for low-rise frames (Models
1 an 2), the 30% rule is conservative practically in
all the cases. The SRSS rule is conservative in most
of the cases. For taller frames (Models 3 and 4) these two
rules are either conservative or slightly underestimate the
response. The level of overestimation or underestimation
varies from one column to another. The 40% rule on
the average practically overestimates the response for all
models and columns. Results also indicate that for
inelastic behavior, the SRSS and 30% rules
underestimate the response in many cases. The corresponding
errors can be up to -11% for the SRSS rule. The
results are quite similar for normal and principal
components.
Accuracy
of the rules for the three components
In this
section of the paper the accuracy of the combination rules
for the effects of the three components or earthquakes is
studied. The structural responses obtained according to the
SRSS and the 30% rules are estimated and
compared to that given by the actual response.

For the
three components of the earthquakes, Cases 1 and 2
will give the actual response for normal
components while the combined response according to the
rules is obtained by combining Cases 5, 6, 7,
8 and 9, which were defined in Section 6.
Similar plots to those of Section 6 for two components are
developed for the three components but are not shown; only
the mean values of the errors are presented. The results
for all models and columns are presented in Table 4. It is
observed that, for low-rise frames (Models 1 an 2) and
elastic behavior, the 30% and SRSS rules are
conservative practically in all the cases. For taller
frames (Models 3 and 4) these two rules are either
conservative or slightly underestimate the response. The
level of overestimation is similar for all the columns. The
40% rule on the average practically overestimates the
response for all models and columns. Results also indicate
that for inelastic behavior the SRSS and 30%
rules underestimate the response in many cases. The
corresponding errors can be up to -11% for the SRSS
rule. By comparison of Tables 3 (two components) and Table
4 (three components) it is observed that, in general, the
30% rule is more conservative than the SRSS rule
when only the horizontal components are considered. For the
three components however, the SRSS is more
conservative. If the criteria to say that a rule is
acceptable is that, on the average, it should give
values of the error close to but greater than zero, these
two commonly used rules (30% and SRSS) would
be acceptable for elastic behavior but they would not be for
inelastic behavior. Results clearly indicate that the
40% rule gives error values, which, in general, are
larger than and close to zero. Consequently, if the
percentile rule is used to estimate the combined response,
in general, a value of 40% should be used for
l.

Table 4.
Average errors (%) for axial loads three components

Critical components
In order to identify the type of components that produce the
maximum response, the ratio (P) of the actual
response for principal components (Cases 10 and
11) and the actual response for normal
components (Cases 1 and 2), is introduced.
The values of P for the axial loads acting at the
base of the four column locations are estimated for the
twenty earthquake time histories. Only the statistics are
presented.

The mean
value and standard deviation of P (μP,
σP) for different cases are summarized in
Table 5 for elastic (actual earthquakes) and inelastic
(scaled earthquakes) behavior. Results indicate that la
mean values of P vary from one column to another and
from one model to another. In general, the larger values of
μP occur for interior columns and elastic
behavior while the larger values of σP are
in general for interior columns and inelastic behavior. The
most important observation that can be made is that μP
is larger than unity practically for all the cases
indicating that the principal components produce greater
axial loads than the normal components, although the
difference may be significant only in a few cases (up to
21%).
Effect
of the vertical component
In order to evaluate the relative importance of the effect
of the vertical component, the structural responses produced
by this component acting alone is estimated and compared to
those of the horizontal components. Typical results are
shown in Fig. 6 for Model 2, elastic behavior and normal
components.
It is
observed that, for lateral columns, the maximum of the two
effects produced by each horizontal component [(Xn,
0, 0) or (0,Yn, 0)] will correspond to
the case where the orientation of the component is the same
than that of the maximum eccentricity of the column with
respect to the structural center of mass (see Fig. 1b). It
is illustrated in Fig. 6 where for lateral columns located
on X direction, the load case (0, Yn,,
0) produces the maximum response while for lateral
column on Y direction the maximum effect is for (Xn,0,
0). The most important observation that can be made is
that the relative effect of the vertical component with
respect to those of the horizontal components, represented
by the Z ratio, is significant. In some cases this
parameter is larger than unity.
Results
for the other models, type of components and inelastic
behavior were also estimated but are not shown. The major
observation made before also apply to these models: the
effect of the vertical component may be significant. In
total 64 plots (four models, four columns, two type of
components and two levels of deformation) similar to those
of Figure 6 were developed. Only the statistics of Z
are presented below.
The mean
values of Z are presented in Table 6 for all the
models, type of components and levels of deformation. Since
the interior columns are close to the center of mass, the
axial load produced by the horizontal components is small
and consequently the Z ratio for these columns is not
considered. Results in the table indicate that the μZ
values significantly vary from one model to another and from
one column to another without showing any trend. Mean
values of up to 0.80 are observed indicating the relative
importance of the effect of the vertical component. These
members are expected to be designed as beam columns.
According to the AISC LRFD code the following equations
should be satisfied:

where
Pu is the required axial strength, Mux
and Muy are the required flexural strength
with respect to the major and minor axis, respectively;
fc
is the resistance factor for compression and
fb
the resistance factor for bending. Other symbols were
defined before. The implication of this is that if the
total axial load is not properly considered it will produce
a detrimental effect on the behavior of the columns. Thus,
the effect of the vertical component not only should not be
overlooked in design but also it should be explicitly
considered no matter how complicated the analysis process
becomes.


Accuracy of Estimating Ry as 0.85 of Rx.
As stated
earlier, the ratio of the effect of the minor horizontal
component to that of the major horizontal component is
usually assumed to be 0.85. As discussed below, the value
of this ratio is important in the relative accuracy of the
rules in the evaluation of the combined response.
Let us assume that RX is the larger of the
two effects and consequently RY will be
the smaller one. If Q denotes the ratio of the
smaller to the larger effect, that is Q = RY
/RX, then for the horizontal components
the SRSS rule can be expressed as:

The values of R are plotted in Fig. 7 for several
values of Q and λ. It is observed from this
figure that for λ= 0.3, RC2 and
RC1 are close each other. From Q = 0
to ≈ 0.3, the 30% rule gives larger response that the
SRSS rule (R< 1). From Q
»
0.3 to 0.65 the R ratio is still smaller than unity
however, the SRSS combined value increases with
respect to the 30% combined value. For Q
»
0.65 to 1.0 the R parameter is larger than unity and
consequently the SRSS rule give values larger than
the 30% rule.
If the SRSS combination rule were the exact solution,
the minimum introduced error by using λ= 0.3 would be
zero for Q
»0.65,
the maximum underestimation error would be about 4% for Q
»
0.3 and the maximum overestimation error would be about 8%
for Q = 1.0. Thus, depending on the Q ratio
the SRSS rule can give greater or smaller combined
response than the 30% value.

The
actual values of the Q parameter are estimated for
the earthquakes and models considered in this study. Only
the columns (corner and interior) where the individual
effects may be comparable are studied. The mean values and
standard deviation of Q are presented in Table 7.
It is observed that
mQ
values
vary from one model to another and from one column to
another. The values range from 0.21 to 0.69. In general
the values are smaller for corner columns than for interior
columns. This difference, however, tend to decrease as the
fundamental period of the models increases. For a given
column, the results in general are similar for both types of
component. Also, for a given column and type of components
the results are similar for both levels of deformation
(elastic and inelastic). The most important observation
that can be made from the table is the mean values of Q
(which range from 0.31 to 0.46 when averaged over all models
and columns) obtained in this study are significantly
smaller than the usually assumed value of 0.85. For this
reason the SRSS rule, when used for the horizontal
components, is less conservative than the 30% rule in
the estimation of the combined response, as shown in Section
6 of the paper.
Conclusions
Several
issues regarding multi-components seismic response analysis
of structures are addressed in this paper. The first issue
is related to the accuracy of the rules to estimate the
combined effect of the individual components of earthquakes.
The rules are studied for normal and principal components,
for local (axial loads) and global (total base shear)
response parameters, elastic and inelastic behaviour and two
and three components. The critical orientation of the
components is identified. Several models of Moment Resisting
Steel Frames (MRSF) are used in the study. The second issue
threats with the relative magnitude of the effect of the
vertical component (RZ) con respect to
those of the horizontal components (RX and
RY). Finally, the accuracy of estimating
the intensity of the weaker component (RY)
as 85% of that of the stronger component (RX)
is studied.

Results
indicate that whether elastic or inelastic behavior occurs
the combined total base shear is reasonably overestimated by
all the rules. The 30% and the SRSS rules,
however, can underestimate the combined response in terms of
axial loads for inelastic behavior. This indicates that the
results for elastic analysis may be quite different from
those of inelastic analysis. The implication of this is that
the results obtained from elastic analysis of steel frame
structures subjected to strong motions may be a very crude
approximation. For the horizontal components the SRSS
rule is less conservative than the 30% rule. For the
three components, the 30% rule is less conservative.
If the criteria to say that a rule is acceptable is
that, on the average, it should give values of the error
close to but greater than zero, these two commonly used
rules would be acceptable for elastic behavior but they
would not be for inelastic behavior. Results clearly
indicate that the 40% rule gives error values, which,
in general, are larger than and close to zero practically in
all cases. Consequently, if the percentile rule is used to
estimate the combined response, in general, a value of 40%
should be used for
l.
It is also observed that the principal components give the
critical response and that the ratio of the effect of the
vertical component to those of the horizontal components can
be significant and consequently should explicitly be used in
design. Mean values of up to 0.80 are observed. Results
also indicate that the ratio of the effect of the minor
horizontal component to that of the major horizontal
component is much smaller than the typical assumed value of
0.85. The value obtained in this study is about 0.40.
Acknowledgements
This
paper is based on work supported by El Consejo Nacional de
Ciencia y Tecnología (CONACyT) under grant 50298-J and by La
Universidad Autónoma de Sinaloa (UAS) under grant
PI-PROFAPI-06-06. Any opinions, findings, conclusions, or
recommendations expressed in this publication are those of
the authors and do not necessarily reflect the views of the
sponsors.
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