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Structural Analysis: Example 1
Twelve-story Moment Resisting Steel Frame
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Analysis of a 12-Story Steel Building
In Stockton, California
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Building Description
12 Stories above grade, one level below grade
Significant Configuration Irregularities
Special Steel Moment Resisting Perimeter Frame
Intended Use is Office Building
Situated on Site Class C Soils
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Analysis Description
Equivalent Lateral Force Analysis (Section 12.8)
Modal Response Spectrum Analysis (Section12.9)
Linear and Nonlinear Response History Analysis(Chapter 16)
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Note: The majority of presentation is based on requirements provided by ASCE 7-05.
ASCE 7-10 and the 2009 NEHRP Provisions (FEMA P-750) will be referred to as applicable
Overview of Presentation
Describe Building
Describe/Perform steps common to all analysis typesOverview of Equivalent Lateral Force analysisOverview of Modal Response Spectrum AnalysisOverview of Modal Response History Analysis
Comparison of ResultsSummary and Conclusions
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Describe Building
Describe/Perform steps common to all analysistypes
Overview of Equivalent Lateral Force analysisOverview of Modal Response Spectrum AnalysisOverview of Modal Response History AnalysisComparison of ResultsSummary and Conclusions
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Overview of Presentation
Structural Analysis, Pa
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A A
B
B
Perimeter Moment
Frame
Gravity-Only Columns
Plan at First Level Above Grade
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Above Level 5 Above Level 9
Perimeter Moment
Frame
Perimeter Moment
Frame
Gravity-Only Columns
Plans Through Upper Levels
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Thickened Slabs
Section A-A
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Section B-B
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3-D Wire Frame View from SAP 2000
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Perspective Views of Structure (SAP 2000)
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Overview of Presentation
Describe Building
Describe/Perform steps common to all analysistypes
Overview of Equivalent Lateral Force analysisOverview of Modal Response Spectrum Analysis
Overview of Modal Response History AnalysisComparison of ResultsSummary and Conclusions
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Seismic Load Analysis: Basic Steps
1. Determine Occupancy Category (Table 1-1)
2. Determine Ground Motion Parameters:
SSand S1 USGS Utility or Maps from Ch. 22) Faand Fv(Tables 11.4-1 and 11.4-2) SDSand SD1(Eqns. 11.4-3 and 11.4-4)
3. Determine Importance Factor (Table 11.5-1)
4. Determine Seismic Design Category (Section 11.6)
5. Select Structural System (Table 12.2-1)
6. Establish Diaphragm Behavior (Section 11. 3.1)7. Evaluate Configuration Irregularities (Section 12.3.2)
8. Determine Method of Analysis (Table 12.6-1)
9. Determine Scope of Analysis [2D, 3D] (Section 12.7.2)
10. Establish Modeling Parameters
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Occupancy Category = II (Table 1-1)
Determine Occupancy Category
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SS=1.25g
S1=0.40g
Ground Motion Parameters for Stockton
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Fa=1.0
Fa=1.4
Determining Site Coefficients
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Determine Importance Factor,
Seismic Design Category
Seismic Design Category = D
I = 1.0
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Select Structural System (Table 12.2-1)Building height (above grade) = 18+11(12.5)=155.5 ft
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Establish Diaphragm Behavior
and Modeling Requirements
12.3.1 Diaphragm Flexibility.
The structural analysis shall consider the relative stiffness of diaphragmand the vertical elements of the seismic forceresisting system. Unless diaphragm can be idealized as either flexible or rigid in accordance withSections 12.3.1.1, 12.3.1.2, or 12.3.1.3, the structural analysis shallexplicitly include consideration of the stiffness of the diaphragm (i.e.,semi-rigid modeling assumption).
12.3.1.2 Rigid Diaphragm Condition.
Diaphragms of concrete slabs or concrete filled metal deck with span-to-depth ratios of 3 or less in structures that have no horizontalirregularitiesare permitted to be idealized as rigid.
Due to horizontal irregularities (e.g. reentrant corners) the diaphragmsmust be modeled as semi-rigid. This will be done by using Shellelements in the SAP 2000 Analysis.
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Selection of Method of Analysis (ASCE 7-10)
ELF is not permitted:
Must use Modal Response Spectrum or Response History Analysis
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Overview of Presentation
Describe Building
Describe/Perform steps common to all analysistypes
Overview of Equivalent Lateral Force analysisOverview of Modal Response Spectrum Analysis
Overview of Modal Response History AnalysisComparison of ResultsSummary and Conclusions
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Determine Scope of Analysis
(Continued)
Continuation of 12.7.3:
Structures that have horizontal structural irregularity Type 1a, 1b, 4, or
5 of Table 12.3-1 shall be analyzed using a 3-D representation.Where a 3-D model is used, a minimum of three dynamic degrees of
freedom consisting of translation in two orthogonal plan directions
and torsional rotation about the vertical axis shall be included at each
level of the structure.
Where the diaphragms have not been classified as rigid or flexible in
accordance with Section 12.3.1, the model shall include representation
of the diaphragms stiffness characteristics and such additional
dynamic degrees of freedom as are required to account for the
participation of the diaphragm in the structures dynamic response.
Analysis of structure must be in 3D, and diaphragms must be modeledas semi-rigid
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Modeling Parameters used in Analysis
1) The floor diaphragm was modeled with shell elements, providing
nearly rigid behavior in-plane.
2) Flexural, shear, axial, and torsional deformations were included in all
columns and beams.
3) Beam-column joints were modeled using centerline dimensions.
This approximately accounts for deformations in the panel zone.
4) Section properties for the girders were based on bare steel, ignoring
composite action. This is a reasonable assumption in light of the fact
that most of the girders are on the perimeter of the building and are
under reverse curvature.
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From Table 12.8.2:Ct=0.028
x=0.80
hn=18+11(12.5)=155.5 ft
Applies in Both Directions
Using Empirical Formulas to Determine Ta
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Applies in Both Directions
T = 1.4(1.59) = 2.23 sec
SD1=0.373Gives Cu=1.4
Adjusted Empirical Period T=CuTa
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Building has nLevels
Use of Rayleigh Analysis to Determine Tcomputed
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Fi i
Tcomputed = 2computed
computed =
g iFii=1
n
i2Wii=1
n
Wi
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K =M2
= Diagonal matrix containing circular frequencies
Periods Computed Using Eigenvalue Analysis
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Mode Shape Matrix
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Range of Periods Computed for This Example
Ta=1.59 sec
CuTa=2.23 sec
Tcomputed= 2.87 sec in X direction
2.60 sec in Y direction
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Periods of Vibration for Computing
Seismic Base Shear
(Eqns 12.8-1, 12.8-3, and 12.8-4)
if Tcomputed is not available use Ta
if Tcomputed is available, then:
if Tcomputed> CuTause CuTa
if Ta
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Area and Line Weight Designations
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CuTa=2.23 sec
Cs=0.044SDSI=0.037 (controls)
Cs=0.021 from Eqn. 12.8-3
Reffective= (0.021/0.037) x 8 = 4.54
Concept of Reffective
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Issues Related to Period of Vibration and Drift
12.8.6.1 Minimum Base Shear for ComputingDrift
The elastic analysis of the seismic force-resistingsystem for computing drift shall be made using theprescribed seismic design forces of Section 12.8.
EXCEPTION: Eq. 12.8-5 need not be considered forcomputing drift
12.8.6.2 Period for Computing DriftFor determining compliance with the story drift limitsof Section 12.12.1, it is permitted to determine theelastic drifts, (xe), using seismic design forces basedon the computed fundamental period of the structurewithout the upper limit (CuTa) specified in Section12.8.2.
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CuTa=2.23 secT=2.60 sec T=2.87 sec
Use DONT Use
Using Eqns. 12.8-3 or 12.8-5 for Computing ELF
Displacements
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Cs =0.5S1
(R /I)Eqn. 12.8-6, applicable only when S1>= 0.6g
What if Equation 12.8-6 had
Controlled Base Shear?
This equation represents the true response
spectrum shape for near-field ground motions.Thus, the lateral forces developed on the basis ofthis equation must be used for determiningcomponent design forces anddisplacements usedfor computing drift.
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CuTa Ccomputed
Cs
0.044SDSIe
Seismic Base Shear
Drift
CuTa Ccomputed
Cs
0.044SDSIe
CuTa Ccompu
Cs
0.044SDSIe
When Equation 12.8-5 May Control
Seismic Base Shear (S1< 0.6g)
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Calculation of ELF Forces (continued)
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Inherent and Accidental Torsion
(continued)
12.8.4.2 Accidental Torsion. Where diaphragms are not flexible, thedesign shall include the inherent torsional moment (Mt) (kip or kN)
resulting from the location of the structure masses plus the accidentaltorsional moments (Mta) (kip or kN) caused by assumed displacementof the center of mass each way from its actual location by a distanceequal to 5 percent of the dimension of the structure perpendicular tothe direction of the applied forces.
Where earthquake forces are applied concurrently in two orthogonaldirections, the required 5 percent displacement of the center of mass
need not be applied in both of the orthogonal directions at the sametime, but shall be applied in the direction that produces the greatereffect.
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Inherent and Accidental Torsion
(continued)
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Forces in Kips
Application of Equivalent Lateral Forces
(X Direction)
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Forces in Kips
Application of Torsional Forces
(Using X-Direction Lateral Forces)
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Stations for Monitoring Drift for
Torsion Irregularity Calculations
with ELF Forces Applied in X Direction
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Results of Torsional Irregularity Calculations
For ELF Forces Applied in X Direction
Result: There is not a Torsional Irregularity for Loading in the X Direction
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Results of Torsional Irregularity Calculations
For ELF Forces Applied in Y Direction
Result: There is a minor Torsional Irregularity for Loading in the Y Direction
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Results of Torsional Amplification Calculations
For ELF Forces Applied in Y Direction(X Direction Results are Similar)
Result: Amplification of Accidental Torsion Need not be Considered
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Drift and Deformation
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Not strictly
Followed in this
Example due to v
minor torsion
irregularity
Drift and Deformation (Continued)
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ASCE 7-05 (ASCE 7-10) Similar
ASCE 7-10
Drift and Deformation (Continued)
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CdAmplified drift based on forces
from Eq. 12.8-5Modified for forces based
on Eq. 12.8-3
Computed Drifts in X Direction
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CdAmplified drift based on forces
from Eq. 12.8-5
Modified for forces based
on Eq. 12.8-3
Computed Drifts in Y Direction
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= P
xI
VxhsxC
d
Eq. 12.8-16*
max = 0.5
Cd
Eq. 12.8-17
The drift in Eq. 12.8-16 is driftfrom ELF analysis, multiplied by Cdand divided by I.
The term in Eq. 12.8-17 is
essentially the inverse of theComputed story over-strength.
*The importance factor Iwas inadvertently left out of Eq. 12.8-16 in ASCE 7-05. It is properly included in ASCE 7-
P-Delta Effects
P-Delta Effects for modal response spectrum analysis and modal response
history analysis are checked using the ELF procedure indicated on this slide.
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Marginally exceeds limit of 0.091 using =1.0. would be
less than max if actual were computed and used.
P-Delta Effects
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Orthogonal Loading Requirements
12.5.4 Seismic Design Categories D through F. Structures
assigned to Seismic Design Category D, E, or F shall, as a
minimum, conform to the requirements of Section 12.5.3.
12.5.3 Seismic Design Category C. Loading applied to
structures assigned to Seismic Design Category C shall, as a
minimum, conform to the requirements of Section 12.5.2 for
Seismic Design Category B and the requirements of this section.
Structures that have horizontal structural irregularity Type 5 in
Table 12.3-1 shall the following procedure [for ELF Analysis]:
Continued on Next Slide
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Orthogonal Loading Requirements
(continued)
Orthogonal Combination Procedure. The structure shallbe analyzed using the equivalent lateral force analysis
procedure of Section 12.8 with the loading applied
independently in any two orthogonal directions and the
most critical load effect due to direction of application of
seismic forces on the structure is permitted to be assumed
to be satisfied if components and their foundations aredesigned for the following combination of prescribed loads:
100 percent of the forces for one direction plus 30
percent of the forces for the perpendicular direction;
the combination requiring the maximum component
strength shall be used.
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ASCE 7-05 Horizontal Irregularity Type 5
Nonparallel Systems-Irregularity is defined to exist where the
vertical lateral force-resisting elements are not parallel to orsymmetric about the major orthogonal axes of the seismic
forceresisting system.
The system in question clearly has nonsymmetrical lateral force
resisting elements so a Type 5 Irregularity exists, and orthogonal
combinations are required. Thus, 100%-30% procedure given
on the previous slide is used.
Note: The words or symmetric about have been removed from thedefinition of a Type 5 Horizontal Irregularity in ASCE 7-10. Thus, thesystem under consideration does not have a Type 5 irregularity inASCE 7-10.
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100% Eccentric
30% Centered
16 Basic Load Combinations used in ELF
Analysis (Including Torsion)
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1.2D+1.0E+ 0.5L + 0.2S
0.9D+1.0E+1.6H
E = Eh +Ev
Eh =QEEv = 0.2SDS
(
= 1.0)
(SDS=0.833g)
Combination of Load Effects
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Structure
is NOT regu
at all
Levels.
} See next slid
Redundancy Factor
12.3.4.2 Redundancy Factor,, for Seismic DesignCategories D through F. For structures assigned toSeismic Design Category D, E, or F, shall equal 1.3unless one of the following two conditions is met, whereby
is permitted to be taken as 1.0:
a) Each story resisting more than 35 percent of the baseshearin the direction of interest shall comply with Table 12.3-3.
b) Structures that are regular in plan at all levelsprovided that the seismic forceresisting systems
consist of at least two bays of seismic forceresistingperimeter framing on eachside of the structure in each orthogonal direction ateachstory resisting more than 35 percent of the base shear.Thenumber of bays for a shear wall shall be calculated asthelength of shear wall divided by the story height or two
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Redundancy, Continued
TABLE 12.3-3 REQUIREMENTS FOR EACH STORY
RESISTING MORE THAN 35% OF THE BASE SHEAR
Moment Frames Loss of moment resistance at the beam-to-
column connections at both ends of a single beam would not
result in more than a 33% reduction in story strength, nor does
the resulting system have an extreme torsional irregularity
(horizontal structural irregularity Type 1b).
It can be seen by inspection that removal of one beam in this structure willnot result in a result in a significant loss of strength or lead to an extremetorsional irregularity. Hence = 1 for this system. (This is applicable to ELF,MRS, and MRH analyses).
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Seismic Shears in Beams of Frame 1 from ELF
Analysis
Seismic Shears in Girders, kips, Excluding Accidental Torsion
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Seismic Shears in Beams of Frame 1 from ELF
Analysis
Seismic Shears in Girders, kips,Accidental Torsion Only
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Overview of Presentation
Describe Building
Describe/Perform steps common to all analysistypes
Overview of Equivalent Lateral Force analysisOverview of Modal Response Spectrum Analysis
Overview of Modal Response History AnalysisComparison of ResultsSummary and Conclusions
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Modal Response Spectrum Analysis
Part 1: Analysis
1. Develop Elasticresponse spectrum (Sec. 11.4.5)
2. Develop adequate finite element model (Sec. 12.7.3)
3. Compute modal frequencies, effective mass, and mode shapes4. Determine number of modes to use in analysis (Sec. 12.9.1)5. Perform modal analysis in each direction, combining each
directionsresults by use of CQC method (Sec. 12.9.3)
6. Compute Equivalent Lateral Forces (ELF) in each direction (Sec.12.8.1
through 12.8.3)7. Determine accidental torsions (Sec 12.8.4.2), amplified if necessary
(Sec. 12.8.4.3)
8. Perform static Torsion analysis
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Modal Response Spectrum Analysis
Part 3: Obtaining Member Design Forces
1. Multiply all dynamic force quantities by I/R (Sec. 12.9.2)
2. Determine dynamic base shears in each direction
3. Compute scale factors for each direction (Sec. 12.9.4) and apply torespective member force results in each direction
4. Combine results from two orthogonal directions, if necessary (Sec.12.5)
5. Add member forces from static torsion analysis (Sec. 12.9.5).Notethat static torsion forces may be scaled by factors obtained in Step
36. Determine redundancy factor (Sec. 12.3.4)
7. Combine seismic and gravity forces (Sec. 12.4)
8. Design and detail structural components
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Mode Shapes for First Four Modes
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Mode Shapes for Modes 5-8
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Number of Modes to Include
in Response Spectrum Analysis
12.9.1 Number of Modes
An analysis shall be conducted to determinethe natural modes of vibration for the structure.The analysis shall include a sufficient numberof modes to obtain a combined modal massparticipation of at least 90 percent of the actual
mass in each of the orthogonal horizontaldirections of response considered by themodel.
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TX
TY
+ +
Scaled Static Torsions
Apply Torsion as a Static Load. Torsions can be
Scaled to 0.85 times Amplified*EFL Torsions if theResponse Spectrum Results are Scaled.
* See Sec. 12.9.5. Torsions must be amplified because they are appliedstatically, not dynamically.
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A= ScaledCQCd Results in X Direction B= ScaledCQCd Results in Y Direction
A
B
Combination 1
A
0.3B
Combination 2
0.3A
B
A+ 0.3B+ |TX| 0.3A+ B+ |TY|
Method 1: Weighted Addition of
ScaledCQCd Results
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A= ScaledCQCd Results in X Direction B= Scaled CQCd Results in Y Direction
A
B
Combination
A
B
(A2+B2)0.5+ max(|TX| or |TY|)
Method 2: SRSS of ScaledCQCd Results
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Response Spectrum Drifts in Y Direction(No Scaling Required)
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Modal Response History Analysis Part 2: Drift and
P-Delta for Systems WithoutTorsion Irregularity
1. Multiply all dynamic displacements by Cd/R(omitted in ASCE 7-05).
2. Compute story drifts based on displacements at center of mass
at each level3. If 3 to 6 ground motions are used, compute envelope of story
drift at each level in each direction (Sec. 16.1.4)
4. If 7 or more ground motions are used, compute average story
drift at each level in each direction (Sec. 16.1.4)
5. Check drift limits in accordance with Sec. 12.12 and Table 12.2-1.
Note: drift limits for Special Moment Frames in SDC D and above
must be divided by the Redundancy Factor (Sec. 12.12.1.1)6. Perform P-Delta analysis using Equivalent Lateral Force procedure
7. Revise structure if necessary
Note: when centers of mass of adjacent levels are not vertically aligned the drifts should be based onthe difference between the displacement at the upper level and the displacement of the point on thelevel below which is the vertical projection of the center of mass of the upper level.(This procedure isincluded in ASCE 7-10.)
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Modal Response History Analysis Part 2: Drift and
P-Delta for Systems WithTorsion Irregularity
1. Multiply all dynamic displacements by Cd/R(omitted in ASCE 7-05).
2. Compute story drifts based on displacements at edge of building
at each level3. If 3 to 6 ground motions are used, compute envelope of story
drift at each level in each direction (Sec. 16.1.4)
4. If 7 or more ground motions are used, compute average storydrift at each level in each direction (Sec. 16.1.4)
5. Using results from the static torsion analysis, determine the driftsat the same location used in Steps 2-4 above. Torsional driftsmay be based on the computed period of vibration (without theCuTalimit). Torsional drifts should be based on computed displacementsmultiplied by C
d
and divided by I.
6. Add drifts from Steps (3 or 4) and 5 and check drift limits in Table 12.12-1.Note: Drift limits for special moment frames in SDC D and abovemust be divided by the Redundancy Factor (Sec. 12.12.1.1)
7. Perform P-Delta analysis using Equivalent Lateral Force procedure
8. Revise structure if necessary
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Average Scaled
SASA
Period Period0.2TAvg TAVG 1.5TAvg
Match Point
ASCE 7
Avg Sca
ASCE 7
TAvg
S2times Average Sca
Note: The same scale factor S2Applies to Each SRSSd Pair
Resolving Issues With Scaling ApproachThere are an infinite number of sets of scale factors that willsatisfy the criteria. Different engineers are likely to obtaindifferent sets of scale factors for the same ground motions.
Use Two-Step Scaling:1] Scale each SRSSd Pair to the Average Period
2] Obtain Suite Scale Factor S2
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Average S1 Scaled Spectra
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Ratio of Target Spectrum to Scaled SRSS
Average
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Match Point
Target Spectrum and SS Scaled Average
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Individual Scaled Components (90)
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Computed Scale Factors
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Number of Modes for
Modal Response History Analysis
ASCE 7-05 and 7-10 are silent on the number of modes to use in ModalResponse History Analysis. It is recommended that the same procedures
set forth in Section 12.9.1 for MODAL Response Spectrum Analysis be used forResponse History Analysis:
12.9.1 Number of Modes
An analysis shall be conducted to determine the natural
modes of vibration for the structure. The analysis shall
include a suffi cient number of modes to obtain acombined modal mass part icipation of at least 90
percent of the actual mass in each of the orthogonal
horizontal directions of response considered by the
model.
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Scaling of Results for
Modal Response History Analysis (Part 1)
The structural analysis is executed using the GM scaled earthquakerecords in each direction. Thus, the results represent the expected
elastic response of the structure. The results must be scaled torepresent the expected inelastic behavior and to provide improvedperformance for important structures. ASCE 7-05 scaling is as follows:
1) Scale all component design forces by the factor (I/R). This isstipulated in Sec. 16.1.4 of ASCE 7-05 and ASCE 7-10.
2) Scale all displacement quantities by the factor (Cd
/R). Thisrequirementwas inadvertently omitted in ASCE 7-05, but is included in Section16.1.4 of ASCE 7-10.
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TcomputedCuTa
VMin
V
ELF
MRH (unscaled)
Inelastic GM
Inelastic ELF
No Scaling Required
Period
Base Shear
Response Scaling Requirements when
MRH Shear is Greater Than Minimum Base Shea
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Low >
High >
Result Maxima from Response History Analysis
Using SS Scaled Ground Motions
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Response History Drifts for
all X-Direction Responses
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Load Combinations for Response History
Analysis
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Envelope of Scaled Frame 1 Beam Shears
from Response History Analysis
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Overview of Presentation
Describe Building
Describe/Perform steps common to all analysistypes
Overview of Equivalent Lateral Force analysisOverview of Modal Response Spectrum Analysis
Overview of Modal Response History AnalysisComparison of ResultsSummary and Conclusions
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Comparison of Maximum X-Direction
Design Story Drift from All Analysis
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Overview of Presentation
Describe Building
Describe/Perform steps common to all analysistypes
Overview of Equivalent Lateral Force analysisOverview of Modal Response Spectrum Analysis
Overview of Modal Response History AnalysisComparison of ResultsSummary and Conclusions
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Required Effort
The Equivalent Lateral Force method and the
Modal Response Spectrum methods requiresimilar levels of effort.
The Modal Response History Method requiresconsiderably more effort than ELF or MRS.
This is primarily due to the need to select andscale the ground motions, and to run so manyresponse history analyses.
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Recommendations for Future Considerations
1. Three dimensional analysis should be required for allResponse Spectrum and
Response History analysis.
2. Linear Response History Analysis should be moved from Chapter 16 into Chapter
12 and be made as consistent as possible with the Modal Response Spectrum Method.For example, requirements for the number of modes and for scaling of results should
be the same for the two methods.
3. A rational procedure needs to be developed for directly including Accidental Torsion in
Response Spectrum and Response History Analysis.
4. A rational method needs to be developed for directly including P-Delta effects in
Response Spectrum and Response History Analysis.
5. The current methods of selecting and scaling ground motions for linear response
history analysis can be and should be much simpler than required for nonlinear
response history analysis. The use of standardized motion sets or the use of
spectrum matched ground motions should be considered.
6. Drift should always be computed and checked at the corners of the building.
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Questions
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Titleslide
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ThesearethethreelinearanalysismethodsprovidedinASCE7.
TheEquivalentLateralForcemethod(ELF)isessentiallyaonemoderesponsespectrum
analysiswithcorrectionsforhighermodeeffects. ThismethodisallowedforallSDCBand
Cbuildings,andforthevastmajorityofSDCD,EandFbuildings. Notethatsomeformof
ELFwill
be
required
during
the
analysis/design
process
for
all
buildings.
TheModalResponseSpectrum(MRS) methodissomewhatmorecomplicatedthanELF
becausemodeshapesandfrequenciesneedtobecomputed,responsesigns(positiveor
negative)arelost,andresultsmustbescaled. However,therearegenerallyfewerload
combinationsthanrequiredbyELF. MRScanbeusedforanybuilding,andisrequiredfor
SDCD,E,andFbuildingswithcertainirregularities,andforSDCD,E,andFbuildingswith
longperiodsofvibration.
ThelinearModalResponseHistory(MRH)methodismorecomplexthatMRS,mainlydue
tothe
need
to
select
and
scale
at
least
three
and
preferably
seven
sets
of
motions.
MRS
canbeusedforanybuilding,butgiventhecurrentcodelanguage,itisprobablytootime
consumingforthevastmajorityofsystems.
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Thevastmajorityofthewritten exampleandthisslidesetisbasedontherequirementsof
ASCE705. TherequirementsofASCE710arementionedwhennecessary. WhenASCE7
10ismentioned,itisgenerallydonesotopointoutthedifferencesinASCE705andASCE
710.
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Thestructureanalyzedisa3DimensionalSpecialSteelMomentresistingSpaceFrame.
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Inthisbuildingalloftheexteriormomentresistingframesarelateralloadresistant. Those
portionsofFramesCandFthatareinterioratthelowerlevelsaregravityonlyframes.
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Thegravityonlycolumnsandgirders belowthesetbacksingridsCandFextendintothe
basement.
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Thisviewshowtheprincipalsetbacksforthebuilding. Theshadedlinesatlevels5and9
representthickeneddiaphragmslabs.
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Notethatthestructurehas onebasementlevel. Thisbasementisfullymodeledinthe
analysis(thebasementwallsaremodeledwithshellelements),andwillleadto
complicationsintheanalysespresentedlater.
Alloftheperimetercolumnsextendintothebasement,andareembeddedinthewall.
(Thewall
is
thickened
around
the
columns
to
form
monolithic
pilasters).
Thus,
for
analysis
purposes,thecolumnsmaybeassumedtobefixedatthetopofthewall.
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AllanalysisforthisexamplewasperformedonSAP2000. TheprogramETABS mayhave
beenamorerealisticchoice,butthiswasnotavailable.
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Theseviewsshowthatthebasementwallsandthe floordiaphragmswereexplicitly
modeledinthreedimensions. Itistheauthorsopinionthatalldynamicanalysisshouldbe
carriedoutinthreedimensions. Whendoingsoitissimpletomodeltheslabsandwalls
usingshellelements. Notethataverycoarsemeshisusedbecausethedesireistoinclude
thestiffness(flexibility)oftheseelementsonly. Nostressrecoverywasattempted. If
stressrecovery
is
important,
amuch
finer
mesh
is
needed.
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ThegoalofthisexampleistopresenttheASCE7analysismethodologiesbyexample.
Thus,thisslidesetissomewhatlonger thanitwouldneedtobeifonlythemainpointsof
theanalysisweretobepresented.
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Thestepspresentedonthisslidearecommontoallanalysismethods. Themainstructural
analysiswouldbeginafterstep10. Note,however,thataverydetailed sideanalysis
mightberequiredtoestablish diaphragmflexibilityandtodetermineifcertainstructural
irregularitiesexist. Onepointthatshouldbestressedisthatregardlessofthemethodof
analysisselectedinstep8(ELF,MRS,orMRH),anELFanalysisisrequiredforallstructures.
Thisis
true
because
ASCE
705
and
ASCE
710
use
an
ELF
analysis
to
satisfy
accidental
torsionrequirementsandPDeltarequirements. Additionally,anELFanalysiswouldalmost
alwaysbeneededinpreliminarydesign.
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This structureisusedforanofficebuilding,sotheOccupancyCategoryisII. Notethat
analystsusuallyneedtorefertotheIBCoccupancycategorytablewhichissomewhat
differentthanshownonthisslide. ItisforthisreasonthatTable11asshownabovehas
beensimplifiedinASCE710. ItshouldalsobenotedthatassigninganOccupancyCategory
canbesubjective,andwhenindoubt,thelocalbuildingofficialshouldbeconsulted.
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These coefficientsarenotparticularlyrealisticbecausetheywereselectedtoprovide
compatibilitywithanearlierversionofthisexample. ItisforthisreasonthatLatitude
Longitude coordinatesarenotgiven. StudentsshouldbeadvisedthatLatitudeLongitude
ispreferabletozipcodebecausesomezipcodescoverlargegeographicareaswhichcan
haveabroadrangeofgroundmotionparameters.
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Notethatthesitecoefficientsarelargerinareasoflowseismicity. Thisisbecausethesoil
remainselasticundersmallerearthquakes. Forlargerearthquakesthesoilisinelastic,and
thesiteamplificationeffectisreduced. NotethatforsiteclassesDandEthefactorFvcan
goashighas3.5forsmallerearthquakes. Thus,forsuchsitesinthecentralandeastern
U.S.,thegroundmotionscanbequitelarge,andmanystructures(particularlycritical
facilities)
maybe
assigned
to
Seismic
Design
Category
D.
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InthisslidetheintermediatecoefficientsSMSandSM1arenot separatelycomputed. Note
thatthesubscriptMstandsforMaximumConsideredEarthquake(MCE),andthesubscript
DinSDSandSD1standsforDesignBasisEarthquake(DBE). TheMCEistheearthquakewith
a2%probabilityofbeingexceededin50years. InCalifornia,theDBEisroughlya10%in50
yeargroundmotion. IntheEasternandcentralU.S.theDBEissomewherebetweena2%
and10%
in
50
year
event.
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NotethattheSDCisafactorofBOTHtheseismicityandintendeduse. For important
buildingsonsoftsitesinthecentralandEasternU.S. itispossibletohaveanassignmentof
SDCD,whichrequiresthehighestlevelofattentiontodetailing. Afewcodecyclesagothe
samebuildingwouldhavehadonlymarginalseismicdetailing(ifany).
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Weenteredthisexampleknowingitwouldbea specialmomentframe,sosystemselection
wasmoot. However,thistablecanbeusedtoillustrateheightlimits(whichdonotapplyto
theSpecialSteelMomentFrame). Therequireddesignparametersarealsoprovidedby
thetable.
Thevalues
of
R=
8and
0arethelargestamongallsystems. TheratioofCdtoRis
oneofthesmallestforallsystems.
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Thediaphragmismodeled usingshellelementsinSAP2000. Onlyoneelementisrequired
ineachbayasallthatisneededintheanalysisisareasonableestimateofinplane
diaphragmstiffness. Ifdiaphragmstressesaretoberecoveredamuchfinermeshwould
berequired.
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Torsional irregularitiesmustbedeterminedbyanalysis,andthisisdiscussedlaterinthe
example. Thestructureclearlyhasareentrantcornerirregularity,andthediaphragm
discontinuityirregularityisalsolikely. Note,however,thattheconsequencesofthetwo
irregularities(2and3)arethesame,sotheseareeffectivelythesameirregularity.
Thestructure
has
anonparallel
system
irregularity
because
of
the
nonsymmetrical
layout
of
thesystem. NotethatinASCE710thewordsorsymmetricaboutinthedescription of
thenonparallelsystemirregularityhavebeenremoved,sothisstructurewouldnothavea
nonsymmetricalirregularityinASCE710. Thisisaconsequentialchangebecause
requirementsforthreedimensionalanalysisand orthogonalloadingaretiedtothe
presenceofatype5irregularity.
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Thestructureinquestionclearlyhasthetwoirregularitiesnoted.
Onethingthatshouldbeillustratedonthisslide(andthepreviousslide)isthatthethere
arenoconsequencesifcertainirregularitiesoccurinSDCBandCsystems. Forexample,
VerticalIrregularities1,2,and3haveconsequencesonlyforSDCD,E,andF,thusthe
possibleoccurrence
of
the
irregularities
need
not
be
checked
in
SDC
B
and
C.
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TheELFmethodisallowedforthevastmajorityofsystems. ThemainreasonthatELFis
notallowedforthissystemisthat(1)itisinSDCD,and(2)ithasReentrant Cornerand
DiaphragmDiscontinuityIrregularities. ItisinterestingtonotethatELFisallowedinhigher
SDCevenwhentherearestiffness,weight,andweakstoryirregularities. Itseemsthatthis
wouldbemoreofadetrimenttotheaccuracyofELFthanthanwouldareenrtant corner.
NotethatTable12.61asshownintheslideisfromASCE705. Thetablehasbeen
simplifiedsomewhatforASCE710(seethenextslide),butthebasicconfigurationswhere
ELFareallowed/disallowedareessentiallythesame.
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ThisisTable12.61fromASCE710. ThemaindifferencewithrespecttoASCE705isthat
building heightisthetriggerformakingdecisions,ratherthantheuseofT
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Titleslide.
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ItisimportanttonotethatALLseismicanalysisrequiresELFanalysisinoneformor
another. ThestatementthatELFmaynotbeallowedasaDesignBasisanalysis means
thatthedesigndriftsandelementforcesmayneed tobebasedonmoreadvanced
analysis,suchasModalResponseSpectrumorResponseHistoryanalysis.
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ThereisasignificantinconsistencyintherequirementthatPDeltaeffectsberepresented
inthemathematicalmodel. Infact,sucheffectsshouldNOTbeincludedinthemodel
becausetheyareevaluatedseparatelyinSection12.8.7. Additionally, directmodelingof
thestrengthoftheelementsisnotrequiredinlinearanalysis,butofcourse,wouldbe
neededinanyformofnonlinearanalysis.
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Threedimensionalanalysisisrequiredforthissystem,andthediaphragmsmustbe
modeledassemirigidbecausethereentrant cornersprohibitclassificationofthe
diaphragmsasrigid.Regardlessofthisrequirement,itwouldbevirtuallyimpossibleto
modeltheexamplestructurein2dimensions.
Inmost
cases
is
is
easier
to
model
astructure
in
three
dimensions
than
in
two.
This
is
due
tothefactthatmostmodernsoftwaremakesiteasytogeneratethemodel,and
assumptionsdonotneedtobemadeastothebestwaytoseparateoutthevarious
elementsforanalysis. Additionally,theuseofrigiddiaphragmsasawaytoreducethe
numberofDOFisnotneededbecausetheprogramscananalyzequitecomplex3Dsystems
inonlyafewseconds. Semirigiddiaphragmsareeasytomodelusingshellelements,and
verycoarsemeshesmaybeusedifitisnotdesiredtorecoverdiaphragmstresses.
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No commentrequired. Seethenotesonthefollowingslide.
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Mostofthesepointsareselfexplanatory. Itshouldbenotedthattheuseofcenterline
analysisinsteelmomentframesis usedbecauseithasbeenshownthatoffsettingerrors
leadtoreasonableresults. Theerrorsincenterlineanalysisarethat(a)sheardeformations
inthepanelzonesareunderestimated,and(b)flexuraldeformationsinthepanelzonesare
overestimated. Manyprogramshavemodelsthatcandirectlyincludepanelzonebeam
columnjoint
deformations.
Several
programs
allow
the
use
of
rigid
end
zones,
but
this
shouldneverbedonebecauseitdrasticallyoverestimatesthelateralstiffnessofthe
structure.
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Thebasementwasmodeledbecauseitwasdesiredtoruntheinteriorcolumnsdownto
thebasementslab.
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Thesearethebasicstepsrequiredforequivalentlateralforceanalysis. Eachofthesepoints
arediscussedinthefollowingseveralslides.
ItshouldbenotedthatthereisalotofdetailintheELFanalysis,andthusthisisnotatrivial
task. TherearenumerousrequirementsscatteredthroughoutASCE7,andsometimes
theserequirements
are
somewhat
ambiguous.
Anyone
attempting
an
ELF
analysis
(or
any
otherASCE7analysisforthatmater)shouldreadtheentirerelevantchapters(11and12in
thiscase)beforebeginningtheanalysis.
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Heretheheightforperiodcalculationsistakenastheheightabovegrade. Thisis
reasonablebecausethebasementwallsareverystiff,andbecausetheperimeter columns
areembeddedinpilastersthatarecastwiththewalls.
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If acomputermodelisavailableitiseasytoestimatetheperiodusingthisapproach. The
lateralloadpatternshouldbeofthesameapproximateshapeasthefirstmodeshape. An
uppertriangularpatternortheELFloadpatternwillusuallysuffice.
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Both oftherationallycomputedperiodsexceedCuTa,soCuTawillbeusedintheELF
analysis.
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TheperiodsfromtheEigenvalue analysisarethemostmathematicallyprecise. Asseen,
theseareveryclosethatthoseproducedbytheRayleighmethod(seepreviousslide).
PeriodscomputedusingtheRayleighmethodshouldgenerallybecloseto,butslightlyless
thanthosecomputedfromEigenvalue analysis.
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Thisslideprovidesa simplesummaryforchoosingtheperiodtouseforELFanalysis.
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Thisslideissimplyakeyforuseindescribingmassescomputation(seefollowingslide).
Bothlinemassesandareamasseswereconsidered.
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Thecalculationsfordeterminingtotalseismicweightareshown. Theequivalentlateral
forceswillbebasedontheweightofthestructureabovegrade(30,394kips)eventhough
thefullstructure,includingthebasement,ismodeled.
Thelocation oftheCMisneededbecausetheequivalentlateralforcesareappliedtothe
CMat
each
level.
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This slideshowntheequationsthatareneededforcomputingthedesignbaseshear.
Equation12.84isnotneededbecausethestructuresperiodislessthanTL. Equation12.6
6isnotneededbecauseS1
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AlthoughbaseshearmaybecontrolledbyEquation12.85, thedriftscanbebasedonthe
baseshearcomputedfromEqn.12.83,andfurthermore,thecomputedperiodofvibration
maybeusedinlieuofCuTafordriftcalculations. Thismeansthataseparatesetoflateral
forcesmaybecomputedforthepurposesofcalculatingdeflectionsinthestructure.
Theexception
shown
for
ASCE
710
did
not
exist
in
ASCE
705,
although
many
analysts
used
thisexceptionanyway. Thereasonisshownonthefollowingslide,wherethedeflections
basedonEqn.12.83and12.55arecompared.
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Thereisnotorsional irregularityforloadingintheXdirection.
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Thereisaveryminortorsional irregularityalevel9forloadsappliedintheYdirection. It
wouldprobablybebesttoredesignthestructuretoeliminatetheirregularity. However,
theconsequencesoftheirregularityarenotsevere.
Notethatthedoubleentriesfordisplacementsinsomelocations(Levels5and9)isdueto
thesetbacks. Thiswasdiscussedonapreviousslidethatshowedthedeflection monitoring
stationsfor
this
loading.
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Thisissuewasdiscussedinearlierslides. Inthepresentanalysisdriftiscomputedonthe
basisoflateralforcescomputedusingEqn.12.83withT=CuTa. Hasthedriftsfromthis
analysisexceededtheallowabledrift,areanalysiswouldhavebeenpermittedusingthe
periodsforRayleighorEigenvalue analysis.
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ThedriftshavebeendeterminedonthebasisoflateralloadsfromEqn.12.85,andhave
beenmodified tobeconsistentwithEqn 12.83,whichusesCuTaastheperiodofvibration.
NotethatthecomputedperiodsfromEigenvalue analysiscouldhavebeenusedinstead,
andtheresultingdriftswouldbeevenlower.
Ifthe
drifts
had
been
based
on
lateral
forces
consistent
with
Eqn.
12.8
5,
the
drifts
would
havebeenexcessive. However,thecomputeddriftsaresignificantlylessthanthelimits
whentheadjustmentismade.
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Thecommentsonthepreviousslideapplytothisslideaswell.
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The100/30percentloadingisusedforthisstructure.
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Thisslideshowsthe16basicseismicloadings thatarerequiredwhenaccidentaltorsion
andorthogonalloadingrequirementsaremet. Whenthetwobasicgravityloadingsare
included,itisseenthat32seismicloadcasesarerequired.
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Thestructureisnotregular,soonlysubparagraph(a)applies.
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Thisslideprovidesthemaximum beamshearsinFrame1ofthestructure. Theseinclude
lateralloadsonly,withoutgravityandwithoutaccidential torsion. Accidentaltorsional
forcesareincludedseparately(seenextslide). Separationofthetorsional forcesfacilitates
thecomparisonoftheresultsfromthethreemethodsofanalysis.Additionally,the
torsional forcesdeterminedintheELFanalysiswouldbeused(withpossiblysome
reduction)in
the
response
spectrum
and
response
history
calculations.
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Thesearethebasicstepsinamodalresponsespectrumanalysis. Manyofthestepsare
requiredforELFanalysis,sotheamountofadditionalworkisnotsubstantial,andthe
additionalworkthatisrequired(steps6,7,and8) isgenerallydonebythecomputer.
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Thisprocedurewouldbeusedforasystemwithsignificanttorsional displacements. Itwas
notrequiredforthebuildingunderconsideration.
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Thenextfourmodeshapesareshownhere. Thereissignificantlateraltorsional interaction
becauseofthesetbacks.
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ThisisoneoftwoapproachestohandleorthogonalloadinginMRSanalysis. Theapproach
shownonthenextslideispreferred.
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ThisslideshowsthemodalshearsforeachlevelascomputedusingtheMRSapproach.
TheXdirectionbaseshearis438.1kips,andtheYdirectionshearis492.8kips. Thus,allof
thestoryshearsandrelatedmemberforcesneedtobescaleupto0.85timestheELFbase
shearof1124kips. Thescalefactorsare2.18and1.94intheXandYdirections,
respectively.
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Seepreviousslidefordiscussion
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Thebeamshearsarefoundineachmode,andthencombinedbySRSS. Theshearsshown
onthisslidehavebeenscaledsuchthattheyareconsistentwith(85%scaled)scaledbase
shears.
TheseshearswillbecomparedtotheELFandMRHshearsattheendofthisslideset.
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Titleslide.
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ThisslideshowsthebasicstepsintheModalResponseHistorymethod. Manyofthesteps
arethesameasrequiredforELForMRSanalysis. Thelargestnewitemistheselection
andscalingofthegroundmotions,andtherunningofthedynamicanalysis.
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Theonlydifferencebetweenthisslideandthepreviousslideisthatwhenthereare
significanttorsional deflections,thedriftshouldbecomputedatthecornerofthebuilding.
Thiswasnotdonehereasthestructuredidnothaveasignificanttorsional response.
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Thisistheprocedurefordeterminingdesignseismicmemberforces. Thesignificantpoint
inthisslideisthatthescalingto85percentofthedesignbaseshearwillberequiredifthe
dynamicbaseshearsarelessthanthe85percentoftheELFshears.
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The ASCE710requirementsforselectinggroundmotionareshownhere. Selectingan
appropriatenumberofrecordsthatsatisfythecriteriacanbechallengingbecausethere
arefewavailablerecordingsofdesignlevelgroundmotions.
Thereisageneralconsensusthatmoreisbetterwhenrunningresponsehistoryanalysis.
Iffact,
ASCE
7rewards
the
engineer
when
seven
or
more
motions
are
used
as
the
average
responseamongthesevenmaybeusedwhendeterminingdesignvalues. Thepeak
responsemustbeusediflessthansevenmotionsareincludedintheanalysis. Onemust
notusefewerthanthreerecordsunderanycircumstances.
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ThescalingrequirementsforthegroundmotionsarebasedonASCE710. Thisresultsin
somewhatlowerscalefactorsthanusedinASCE705.
Hereitisimportanttonotethatthatthereareseveralsetsofscalefactorsappliedinthe
analysis:
(1) ScalingbyratioofI/R
(2) Groundmotionscalingasindicatedabove
(3) Scalingto85%ofELFbaseshear
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Thesepointsareinadditiontotheproblemdiscussedinthecommentaryinthelastslide.
Regardingthefirstpoint,theauthorschosetoscaletotheaverageofthetwofirstmode
fundamentalperiods. Anotherchoicewouldbetoscaleovertherangeof0.2timesthe
smallerperiodto1.5timesthelargerperiod.
Tosomethesecondpointisnotimportantbecauseitisunlikelythatdifferentengineers
wouldusethesamesetofgroundmotions. However,thecurrentmethodallowsthe
designertoapplyscalefactorsinaarbitrarymanner,andthisallowsthedesignertoscale
downoffendinggroundmotions.
Innonlinearanalysistheperiodselongate,soitmakessensetoconsiderthiswhenscaling.
Forlinearanalysis,theperiodsdonotchange,andthereisnoreasontoscaleatperiods
aboveT(unlessoneistryingtomanageuncertaintiesrelatedtocomputingT).
Thefinal
point
is
related
to
the
problem
illustrated
in
the
previous
slide.
The
higher
modes
dominatethescaling,eventhoughtheymaycontributeverylittletothedynamicresponse.
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Asalreadymentioned,thethirdapproachwasusedinthisexample.
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Inthisexampleatwostepscalingapproachisused. First,theSRSSofeachcomponentpair
arescaledtomatchthetargetspectrumattheperiodTavg. Thisfactorwillbedifferentfor
eachofSRSSspectra.
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Thefinalscalefactorforeachmotionistheproductofthetwoscalefactors. Byuseofthis
approachallengineerswillarriveatthesamescalefactorsforthesamesetofmotions.
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Theactualrecordsusedformtheanalysisareshowninthisslide. Theserecordscamefrom
thePEERNGAdatabase. TheyarereferredtoassetsA,B,andCherein.
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Thisslideshowstheunscaled SRSSspectraforeachmotionpair,togetherwiththetarget
spectrum.
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ThisslideshowstheaverageoftheS1scaledspectraforthethree earthquakes. Notethe
perfectmatchatthetargetperiod.
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ThisslideshowstheratioofthetargetspectrumtotheS1 Scaledspectraoverthetarget
periodrange.
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Thespectrum finalscaledspectrumiscomparedtothetargetspectrumhere. Thereisa
prettygoodmatchatperiodsbetween0.5secondsand5.0seconds,butthematchisnot
sogoodinthehighermodes.
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Thisplotshowstheindividualscaledcomponentsinthe00direction. Notethatthe
component spectrafallbelowthetargetspectrabecausethecomponentsarenot
amplifiedbytheSRSSprocedure. TheSRSSofthecomponentpairswouldbecloserto
thetargetspectrum.
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Seethecommentonthepreviousslide.
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This slideshowsthefinalcomputedscalefactors. Notethateachcomponentpairreceives
itsownS1factor,andallrecordsusethesameS2factor.
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Chapter16ofASCE7does notprovideguidanceonthenumberofmodestouseinmodal
responsehistoryanalysis. Itseemslogicaltofollowthesameproceduresasgivenin
Chapter12formodalresponsespectrumanalysis,andthiswasdonefortheexample
building.
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Chapter 16ofASCE7doesnotprovideguidanceondampinginresponsehistoryanalysis.
Itseemslogicaltouse5%dampingineachmodeasthiswasusedinthedevelopmentof
theresponsespectra. Thus,5%wasusedintheexample. Note,howeverthethatuseof
5%dampinginnonlinearresponsehistoryanalysisisprobablyunconservative. Theuseof
alowervalue,say2%critical,isgenerallyrecommendedfornonlinearanalysis.
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Thesepointsareexplainedinthefollowingslides.
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Theresponsehistoryshearsshouldbescaledupto85%oftheminimumbaseshear.
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NoscalingisrequiredwhentheMRHshearisgreaterthantheMinimumBaseShear.
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Thisslidecomparesresponsespectrumscalingwithresponsehistoryscaling.
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Thesearetheindividually scaledGMusedintheanalyses.
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ThisslideshowsthemaximumresponsequantitiesfromtheSSscaledgroundmotions.
Thereisahugevariation(considering thefactthatallrecordswerescaledinasimilar
mannertothesametargetspectrum),withbaseshearsrangingfromalowof1392kipsto
ahighof5075kips. Thevariationin otherresponsequantitiesaresimilar. Itisdifficultto
determinethesourceofthesevariations,whichincludethescalingmethod,thedifference
betweencomponents,
and
higher
mode
effects.
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Heretheindividualscalefactorsareprovided. Thesefactorsnormalizetheresponsesto
havethesamebaseshearasgivenby85percentoftheELFbaseshear. Itisnotablethatall
ofthegroundmotionshadtobescaledup.
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Thecomputeddriftenvelopesareshownhere. Thedriftsshave beenscaledbyCd/R,but
no85%scalingisrequired.Aswiththeothermethods,thedriftsappeartobewellbelow
thelimits,indicatingthatthestructureisprobablytoostiff.
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This slideshowsthevariousloadcombinations. Notethat100percentofthe85%scaled
motionswereappliedineachdirection.
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Thisslideshowstheenvelopesofallofthe85%scaledbeamshearsonFrame1. These
willbecomparedtotheresultsfromtheothermethods attheendofthepresentation.
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Titleslide.
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Thestoryshearsare comparableduetothescalingoftheMRSandMRHresults. However,
itseemsthatheshearsintheupperlevelsarerelativelygreaterintheMRHanalysis. This
isprobablyduetothehigherspectralaccelerationinthehighermodes(whencomparedto
thetargetspectrum).
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TheELFmethodproducesthelargestdrifts. However,thesedriftswerebasedona period
ofCuTa,andnotonthecomputedsystemperiod. Theresponsehistorydriftsarelargerat
theupperlevels,reflectingtheinfluenceofthehighermodes.
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Again,thebeamshearsarelargerintheupperlevelswhencomputedusingresponse
history. Aswithdrift andstoryshear,thisisattributedtohighermodeeffectsaccentuated
byhighspectralaccelerationsatlowerperiods(whencomparedtothetargetspectrum).
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Titleslide.
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Slidecomparingrelativeeffortofvariousmethodsofanalysis.
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Slidedescribesaccuracyinanalysis.
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ThesearetheauthorsopinionanddonotnecessarilyreflecttheviewsofASCEorBSSC.
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Thisslide isintendedtoinitiatequestionsfortheparticipants.
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Instructional Material Complementing FEMA P-751, Design Examples
StructuralAnalysis:Example1
TwelvestoryMoment ResistingSteelFrame
InstructionalMaterial ComplementingFEMAP751,DesignExamples
4
Structural Analysis
Finley Charney, Adrian Tola Tola, and Ozgur Atlayan
StructuralAnalysis,Part11
Analysisofa12StorySteelBuilding
InStockton,California
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part12
BuildingDescription
12Storiesabovegrade,onelevelbelowgrade
Significant ConfigurationIrregularities
SpecialSteelMomentResistingPerimeterFrame
IntendedUseisOfficeBuilding
SituatedonSiteClassCSoils
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part13
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Instructional Material Complementing FEMA P-751, Design Examples
AnalysisDescription
EquivalentLateralForceAnalysis(Section12.8)
ModalResponseSpectrumAnalysis(Section12.9)
LinearandNonlinearResponseHistoryAnalysis(Chapter16)
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part14
Note:Themajorityofpresentation isbasedonrequirements providedbyASCE705.
ASCE710andthe2009NEHRPProvisions(FEMAP750)willbereferred toasapplicable.
OverviewofPresentation
DescribeBuildingDescribe/PerformstepscommontoallanalysistypesOverviewofEquivalentLateralForceanalysisOverviewofModalResponseSpectrumAnalysisOverviewofModalResponseHistoryAnalysisComparisonofResultsSummaryandConclusions
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part15
DescribeBuildingDescribe/Performstepscommontoallanalysis
typesOverviewofEquivalentLateralForceanalysisOverviewofModalResponseSpectrumAnalysisOverviewofModalResponseHistoryAnalysisComparisonofResultsSummaryandConclusions
InstructionalMaterialComplementingFEMAP751,DesignExamples
OverviewofPresentation
StructuralAnalysis,Part16
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Instructional Material Complementing FEMA P-751, Design Examples
A A
B
B
PerimeterMoment
Frame
GravityOnlyColumns
PlanatFirstLevelAboveGrade
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part17
AboveLevel
5 AboveLevel9
PerimeterMoment
Frame
PerimeterMoment
Frame
GravityOnlyColumns
PlansThroughUpperLevels
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part18
ThickenedSlabs
SectionAA
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part19
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Instructional Material Complementing FEMA P-751, Design Examples
SectionBB
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part110
3DWireFrameViewfromSAP2000
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part111
PerspectiveViewsofStructure(SAP2000)
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part112
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Instructional Material Complementing FEMA P-751, Design Examples
OverviewofPresentation
DescribeBuildingDescribe/Perform stepscommontoallanalysis
typesOverviewofEquivalentLateralForceanalysisOverviewofModalResponseSpectrumAnalysisOverviewofModalResponseHistoryAnalysisComparisonofResultsSummaryandConclusions
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part113
SeismicLoadAnalysis:BasicSteps
1. DetermineOccupancyCategory(Table11)
2. DetermineGroundMotionParameters:
SSandS1 USGSUtilityorMapsfromCh.22)
FaandFv(Tables11.41and11.42)
SDSandSD1 (Eqns.11.43and11.44)
3. DetermineImportanceFactor(Table11.51)
4. DetermineSeismicDesignCategory(Section11.6)
5. SelectStructuralSystem(Table12.21)
6. EstablishDiaphragmBehavior(Section11.3.1)
7. EvaluateConfigurationIrregularities(Section12.3.2)
8. DetermineMethodofAnalysis(Table12.61)
9. DetermineScopeofAnalysis[2D,3D] (Section12.7.2)
10. EstablishModeling
Parameters
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part114
OccupancyCategory=II(Table11)
DetermineOccupancyCategory
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part115
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Instructional Material Complementing FEMA P-751, Design Examples
SS=1.25g
S1=0.40g
GroundMotionParametersforStockton
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part116
Fa=1.0
Fa=1.4
DeterminingSiteCoefficients
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part117
DeterminingDesignSpectralAccelerations
SDS=(2/3)FaSS=(2/3)x1.0x1.25=0.833
SD1=(2/3)FvS1=(2/3)x1.4x0.40=0.373
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part118
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Instructional Material Complementing FEMA P-751, Design Examples
DetermineImportanceFactor,
SeismicDesignCategory
SeismicDesignCategory=D
I=1.0
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part119
SelectStructuralSystem(Table12.21)Buildingheight(abovegrade)=18+11(12.5)=155.5ft
SelectSpecialSteelMomentFrame: R=8, Cd=5.5, 0=3InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part120
EstablishDiaphragmBehavior
andModelingRequirements
12.3.1DiaphragmFlexibility.
Thestructuralanalysisshallconsidertherelativestiffnessofdiaphragmsandtheverticalelementsoftheseismicforceresistingsystem.Unlessadiaphragmcanbeidealizedaseitherflexibleorrigidinaccordancewith
Sections12.3.1.1,
12.3.1.2,
or
12.3.1.3,
the
structural
analysis
shall
explicitlyincludeconsiderationofthestiffnessofthediaphragm(i.e.,semirigidmodelingassumption).
12.3.1.2RigidDiaphragmCondition.
Diaphragmsofconcreteslabsorconcretefilledmetaldeckwithspantodepthratiosof3orlessinstructuresthathavenohorizontalirregularitiesarepermittedtobeidealizedasrigid.
Duetohorizontalirregularities(e.g.reentrantcorners)thediaphragmsmustbemodeledassemirigid. ThiswillbedonebyusingShellelementsintheSAP2000Analysis.
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Instructional Material Complementing FEMA P-751, Design Examples
X
?
?
DetermineConfigurationIrregularities
HorizontalIrregularities
Irregularity2occursonlowerlevels. Irregularity3ispossiblebutneednotbeevaluatedbecauseithassameconsequencesasirregularity3.TorsionalIrregularitieswillbeassessedlater.
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part122
X
X
X
X
DetermineConfigurationIrregularities
VerticalIrregularities
Irregularities2and3occurduetosetbacks. Softstoryandweakstoryirregularities
arehighlyunlikelyforthissystemandarenotevaluated.
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part123
Systemisnotregular
Verticalirregularities
2and3exist
Notapplicable
SelectionofMethodofAnalysis(ASCE705)
ELFisnotpermitted:
MustuseModalResponseSpectrumorResponseHistoryAnalysis
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part124
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7/26/2019 G+12 Steel Building
295/504 StructuralAnalysis1
Instructional Material Complementing FEMA P-751, Design Examples
SelectionofMethodofAnalysis(ASCE710)
ELFisnotpermitted:
MustuseModalResponseSpectrumorResponseHistoryAnalysis
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part125
OverviewofPresentation
DescribeBuildingDescribe/Performstepscommontoallanalysis
types
OverviewofEquivalentLateralForceanalysisOverviewofModalResponseSpectrumAnalysisOverviewofModalResponseHistoryAnalysisComparisonofResultsSummaryandConclusions
InstructionalMaterialComplementingFEMAP751,DesignExamples StructuralAnalysis,Part126
CommentsonuseofELFforThis
System
ELFisNOTallowedastheDesignBasisAnalysis.
However,ELF(oraspectsofELF)mustbeusedfor:
PreliminaryanalysisanddesignEvaluationoftorsionirregularitiesand
amplification
EvaluationofsystemredundancyfactorsComputingPDeltaEffectsScalingResponseSpectrumandResponseHistory
results