Abstract
The orientation of the seismic action is known to have a non-negligible effect on the seismic behaviour of buildings. However, modern earthquake-related standards only partially cover the effect of this factor and results of practical utility on this topic are still limited. To address this issue, a methodology enabling the determination of the critical angle of seismic incidence in the context of Lateral Force Analysis is proposed. The analytical methodology determines the critical angle of seismic incidence for the storey displacements and the interstorey drifts of buildings that conform with standard-based provisions for linear static analysis. The applicability of the methodology is illustrated for three buildings comprising different typologies in plan and in elevation. The accuracy of the analytical results obtained is validated by performing a parametric lateral force analysis of the buildings for different orientations of the bidirectional seismic action.
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Abbreviations
- α, ASI:
-
Angle of seismic incidence
- α01 :
-
Angle between the structural axis X and the optimum principal axis I opt
- α02 :
-
α01 + 90°
- αcrit, ASIcrit :
-
Critical angle of seismic incidence
- β :
-
Percentile used for the percentage combination rule, 30 or 40%
- θi,F :
-
Rotation about axis i due to F
- λ:
-
Modal mass correction factor
- ω:
-
Angle between the structural axis X and the principal axis I
- ω :
-
Angle between the structural axis X and the fictitious principal axis I
- A:
-
Arbitrary point on a diaphragm
- ag :
-
Design ground acceleration on type A soil
- CS :
-
Elastic centre
- C S :
-
Fictitious elastic centre
- dof/s:
-
Degree/s of freedom
- F:
-
Module of force vector F
- F “1” :
-
Unit force vector
- f i :
-
Flexibility coefficient along axis i
- \({\text{F}}_{\text{i,F}}^{\text{A}}\) :
-
Component of F along axis i applied on A
- \(\underline{\text{f}}_{\text{i}} ,\underline{\text{m}}_{\text{i}}\) :
-
N-dimensional vector of forces and moments, respectively, along and about axis i
- [F m F s]T :
-
Force vector acting on the master and on the slave dofs
- \(\underline{\text{F}}_{\text{R}}\) :
-
Equivalent force vector acting on the master dofs
- F R“1” :
-
Equivalent force vector of a unit force acting on the master dofs
- I, II, III:
-
Principal axes
- I, II, III :
-
Fictitious principal axes
- I opt , II opt , III opt :
-
Optimum principal axes
- ISDA :
-
Interstorey drift of point A
- KI, KII, KIII :
-
Principal stiffness coefficients
- K I , K II , K III :
-
Fictitious Principal stiffness coefficients
- kI, kII, kIII :
-
Numerical coefficients associated with the principal directions of the torsionally coupled single storey system
- Kij :
-
Stiffness matrix coefficients with i = X, Y, Z and j = X, Y, Z defined on (X, Y, Z)
- kij :
-
Coefficients functions of kn with i = x, y, z and j = x, y, z defined on (X, Y, Z)
- \(\underset{\raise0.3em\hbox{$\smash{\scriptscriptstyle-}$}}{\text{K}}_{\text{ij}}\) :
-
N × N stiffness matrix with i = x, y, z and j = x, y, z defined on (X, Y, Z)
- \(\left[ {\begin{array}{*{20}c} {\underset{\raise0.3em\hbox{$\smash{\scriptscriptstyle-}$}}{K}_{mm} } & {\underset{\raise0.3em\hbox{$\smash{\scriptscriptstyle-}$}}{K}_{ms} } \\ {\underset{\raise0.3em\hbox{$\smash{\scriptscriptstyle-}$}}{K}_{sm} } & {\underset{\raise0.3em\hbox{$\smash{\scriptscriptstyle-}$}}{K}_{ss} } \\ \end{array} } \right]\) :
-
Stiffness matrix of a structure rearranged so that K mm is a matrix of the master dofs and K ss the matrix of the slave dofs
- \({\text{k}}_{\text{n}}\) :
-
Numerical coefficient of isotropic buildings
- \(\underset{\raise0.3em\hbox{$\smash{\scriptscriptstyle-}$}}{\text{K}}_{ 0}\) :
-
Stiffness matrix of order N of the N-storey plane frame
- \(\underset{\raise0.3em\hbox{$\smash{\scriptscriptstyle-}$}}{\text{K}}_{\text{R}}\) :
-
Condensed stiffness matrix that corresponds to the master dofs
- Kunc :
-
Uncoupled stiffness of the building
- m:
-
Total mass of a building
- Mi,F :
-
Moment about axis i due to F
- N:
-
Number of storeys
- O(X, Y, Z):
-
Coordinate system of three orthogonal axes X, Y, Z that intersect the diaphragm at point O
- S:
-
Soil factor of the EC8 response spectrum
- Se(T):
-
Elastic spectral acceleration at period T
- TB, TC, TD :
-
Corner periods of the EC8 response spectrum
- TI, TII :
-
Principal periods
- T Iopt , T IIopt :
-
Optimum principal periods
- Tunc :
-
Uncoupled fundamental period of vibration
- T unc.opt :
-
Optimum uncoupled fundamental period of vibration
- \({\text{u}}^{\text{A}}\) :
-
Resultant displacement of A
- \({\text{u}}_{\text{i,F}}^{\text{A}}\) :
-
Displacement of A on axis i due to F
- \(\underline{\text{u}}_{\text{i}} ,\underline{\uptheta}_{\text{i}}\) :
-
N-dimensional vector of displacements and rotations, respectively, along and about axis i
- \(\left[ {\underline{\text{u}}_{\text{m}} \,\,\underline{\text{u}}_{\text{s}} } \right]^{\text{T}}\) :
-
Displacement vector of the master and the slave dofs
- xA, yA :
-
Coordinates of A on the structural reference system
- \({{\text{x}}_{\text{A}}}^{\prime}\), \({{\text{y}}_{\text{A}}}^{\prime }\) :
-
Coordinates of A on the principal reference system
- \({{x}_{A}}^{\prime }\), \({{y}_{A}}^{\prime }\) :
-
Coordinates of A on the fictitious principal reference system
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Acknowledgements
Financial support of the Portuguese Foundation for Science and Technology, through the Ph.D. Grant of the first author (PD/BD/113681/2015), is gratefully acknowledged.
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Appendix: Derivation of the piecewise expression for the final demand
Appendix: Derivation of the piecewise expression for the final demand
The terms F(α) and F(α + 90°) included in the expression of the final demand, which is expressed by Eq. (15) (for buildings with a real elastic axis), Eq. (28) (for buildings without a real elastic axis) and Eq. (30) (for the ISD), depend on the corner periods TB and TC of the response spectrum and on the principal periods of the structure TI and TII. As a result, the referred equations may have different forms according to the following scenarios:
-
TB ≤ TII and TI ≤ TC—In this case all Tunc(α) fall on the horizontal branch of the spectrum and the spectral acceleration Se is constant for all angles α. Therefore, F(α) and F(α + 90°) obtained from Eq. (11) are also constant and equal to Fconst for all angles α. Equations (15), (28) and (30) have one branch in which the base shear can be omitted in the maximization procedure since it is not a function of the angle α. For example, Eq. (15) has the following form:
$${\text{u}}^{\text{A}} ( {{\upalpha )}} = {\text{F}}^{ 2}_{\text{const}} \cdot \sqrt {\left( {{\text{u}}_{\text{I},\text{``}1\text{''}}^{\text{A}} ( {{\upalpha )}} \pm \beta \cdot {\text{u}}_{\text{I},\text{``}1\text{''}}^{\text{A}} ( {{\upalpha \,+\, 90}}^{\text{o}} )} \right)^{ 2} { + }\left( {{\text{u}}_{\text{II},\text{``}1\text{''}}^{\text{A}} ( {{\upalpha )}} \pm \beta \cdot {\text{u}}_{\text{II},\text{``}1\text{''}}^{\text{A}} ( {{\upalpha + 90}}^{\text{o}} )} \right)^{ 2} }$$(38) -
0 < (TII, TI) ≤ TB or TC ≤ (TII, TI) ≤ TD—In this case all Tunc(α) fall on the first or the third branch of the spectrum and Se is a function of the angle α. Since both Se (α) and Se (α + 90°) belong to the same branch of the spectrum, F(α) and F(α + 90°) are expressed by the same equation. Hence, Eqs. (15), (28) and (30) have one branch in which F(α) and F(α + 90°) are expressed as functions of the angle α. For example, the terms F(α) and F(α + 90°) of Eq. (13) which lead to the final displacement in Eq. (15) are given by Eq. (39) assuming ω = 0.
$${\text{F}}(\upalpha ) = \frac{{{\text{T}}_{\text{C}} \cdot {\text{a}}_{\text{g}} \cdot {\text{S}} \cdot {{\upeta }} \cdot 2. 5}}{{\frac{{{\text{T}}_{\text{I}} \cdot {\text{T}}_{\text{II}} }}{{\sqrt {{ \cos }\left( {{\upalpha }} \right)^{ 2} \cdot {\text{T}}_{\text{II}}^{ 2} + { \sin }\left( {{\upalpha }} \right)^{ 2} \cdot {\text{T}}_{\text{I}}^{ 2} } }}}} ,\quad {\text{F}}(\upalpha + 9 0^{\text{o}} ) { = }\frac{{{\text{T}}_{\text{C}} \cdot {\text{a}}_{\text{g}} \cdot {\text{S}} \cdot {{\upeta }} \cdot 2. 5}}{{\frac{{{\text{T}}_{\text{I}} \cdot {\text{T}}_{\text{II}} }}{{\sqrt {{ \cos }\left( {{{\upalpha \,+\, 90}}^{\text{o}} } \right)^{ 2} \cdot {\text{T}}_{\text{II}}^{ 2} + { \sin }\left( {{{\upalpha \,+\, 90}}^{\text{o}} } \right)^{ 2} \cdot {\text{T}}_{\text{I}}^{ 2} } }}}}$$(39) -
All other combinations of TII and TI—To illustrate this scenario, the case in which TC ≤ TI ≤ TD and TB ≤ TII ≤ TC (see Fig. 10a) is presented herein and the same rationale can be followed for any other combination.
In this case, Tunc(α) falls on different branches of the spectrum depending on the angle α. As a result, Se is expressed by different equations as a function of α and F(α) has multiple branches, where at least one of these branches is a function of α. The base shear of the perpendicular direction F(α + 90°) is expressed following the same rules. The relative position of Tunc(α) and Tunc(α + 90°) for a given angle α, shown in Fig. 10b, affects the development of Eqs. (15), (28) and (30). It can be seen in Fig. 10b that the angle θTc corresponding to the corner period TC determines the angle range of the branches of the final expression. To illustrate the formulation of Eqs. (15), (28) and (30), the relative position of Tunc(α) and Tunc(α + 90°) is presented in Fig. 11 for all ASIs and for all three cases with respect to the angle θTc. The solid hatched areas represent the position of Tunc(α), while the dashed hatched areas represent the respective position of Tunc(α + 90°). As a result, Eqs. (15), (28) and (30) comprise eight branches with specific angle range limits. The terms F(α) and F(α + 90°) of Eq. (15) that are used to form the piecewise equation are presented in Eq. (40) for the first case of Fig. 11, i.e. θTc < 45° and ω = 0.
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Skoulidou, D., Romão, X. Critical orientation of earthquake loading for building performance assessment using lateral force analysis. Bull Earthquake Eng 15, 5217–5246 (2017). https://doi.org/10.1007/s10518-017-0176-9
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DOI: https://doi.org/10.1007/s10518-017-0176-9