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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

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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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    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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    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