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GTSTRUDL Version 28 and Future Enhancements

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Title: GTSTRUDL Version 28 and Future Enhancements


1
GTSTRUDL Version 28 andFuture Enhancements
  • Kenneth M.(Mac) Will
  • CASE Center
  • GTSUG 2004
  • June 2004

2
Presentation Outline
  • Versions 27.1 and 27.2
  • New features in Version 28
  • Longer term future enhancements

3
Version 28 Release Status
  • Documentation being prepared
  • Release Guides Volumes 1 2
  • Installation Guide
  • Getting Started
  • Analysis Guide
  • Design Guide
  • Revision R of Reference Manuals
  • Release is scheduled for September

4
Versions 27.1 and 27.2
  • Error correction releases for non-QA customers
    who encountered problems
  • If you would like to request 27.2, please let us
    know. This is not a full release only a
    replacement for the gtst27.exe. A new password
    is required.

5
Version 27.2
  • Corrections and Enhancements for Version 27.2 of
    GTSTRUDL
  • GTMenu
  • The number of member property groups that can be
    used by Redraw Solid has been increased from 1000
    to 10000. Models such as those for offshore
    jacket structures which contain variable member
    properties in a text input file could exceed the
    1000 property group limitation and Redraw Solid
    would not use the correct property group. (No
    GPRF issued)
  • An abort will no longer occur when creating
    finite elements using the Create Finite Elements
    Using Grid option. (No GPRF issued)

6
Version 27.1
  • Corrections and Enhancements for Version 27.1 of
    GTSTRUDL
  • Dynamics
  • If joint constraints exist in the model, the
    assembly of the consistent mass and damping
    matrices now operates more efficiently.
    Previously, large demands on memory allocation
    occurred if joint constraints were present.
  • GTMenu
  • Member properties with variable pipe properties
    are now brought into GTMenu correctly. The
    members will be displayed correctly by Redraw
    Solid using the properties of the first variable
    segment. The properties will also be brought
    back to GTSTRUDL correctly. Previously in
    Version 27.0, variable pipe properties were
    brought into GTMenu incorrectly and Redraw Solid
    would draw incorrectly if variable pipe
    properties existed. (No GPRF issued)
  • An abort will no longer occur when entering
    GTMenu with a model which contains Superelement
    and Group definitions. (No GPRF issued)
  • The Mode Bar in GTMenu is no longer disabled
    following an Inquire using either a right mouse
    click or the use of the Inquire button. (No GPRF
    issued)

7
Versions 27.1 (cont)
  • Nonlinear Analysis
  • Nonlinear analysis will no longer abort when
    linear elastic connections are present and
    multiple loading conditions are active for the
    nonlinear analysis (GPRF 2003.5)
  • Nonlinear Dynamic Analysis
  • Nonlinear dynamic analysis now produces correct
    results for the case where the sign of the axial
    strain in tension/compression only, linear
    geometry frame members reverses between time
    points. (No GPRF issued)
  • Reinforced Concrete Design
  • The diameter of circular steel cage reinforcement
    is now reported correctly for the CP110 and
    BS8110 concrete design for round columns using
    the PRINT REINFORCEMENT command. (GPRF 2003.6)
  • An abort in Proportioning columns designed using
    the ACI codes will no longer occur during the
    capacity check phase. (GPRF 2003.7)

8
Electronic Documentation
  • PDF Electronic versions of Reference Manuals will
    no longer be Draft and will contain latest
    changes to documentation Revision S.

9
GTSTRUDL Startup Model Wizard
  • New Tank Option on the Model Wizard for Circular
    Tanks with flat or hemispherical top and/or
    bottom

10
Model WizardNew Tank Wizard
  • Geometry and top and bottom specification

11
Model WizardNew Tank Wizard (cont)
  • Graphical display of geometry created using Tank
    Model Wizard while generating the model

12
Model WizardNew Tank Wizard
  • Thickness and support specification including
    soil springs on bottom

13
Model WizardNew Tank Wizard
  • Self-weight, internal pressure, and hydrostatic
    load specification

14
Model Wizard
  • The Finite Element Mesh Model Wizard now includes
    In-Plane springs and Compression Only options for
    springs normal to the plane of the element. The
    Compression Only spring option will create a
    nonlinear spring curve and nonlinear spring
    elements. In-plane springs will be elastic
    springs.

15
Model WizardIn-Plane Springs and Compression
Only Springs
Compression only option
In-plane springs
16
Model WizardIn-Plane Springs and Compression
Only Springs Output
17
Model Wizard
  • The Model Wizard can now be executed directly
    from the GTSTRUDL Output Window as shown below

18
GTSTRUDL Output Window
  • The Import DXF option has been enhanced to
    convert lines and polylines into Construction
    Points and Lines which can later be used in
    GTMenu to create the model. The next dialog is
    shown on the next slide.

19
GTSTRUDL Output WindowImport DXF
New option to create Construction Points and
Lines
20
GTSTRUDL Output WindowImport DXF
  • A new Properties tabbed dialog is available for
    Construction Points and Lines. The primary use
    is to establish the starting ids for the Points
    and Lines.

21
GTSTRUDL Output WindowAnalysis
  • New options available under Analysis
  • New Hyper-Column Solver for solving large
    problems. More data on this is on later slides.

22
GTSTRUDL Output WindowAnalysis
  • Displacement control is now available in the
    Pushover Analysis dialog which is shown on the
    next slide. When displacement control is enabled
    and a pushover analysis load increment encounters
    convergence difficulties, the pushover analysis
    will switch to displacement control. The user
    may select joint displacement dofs to monitor
    and control.

23
GTSTRUDL Output WindowAnalysis Pushover Dialog
Displacement Control Option
24
GTSTRUDL Output WindowAnalysis
  • A new Cable Analysis Wizard and dialogs have been
    implemented to facilitate the use of Cable
    Analysis

Cable additions
25
GTSTRUDL Output WindowAnalysis Cable Prestress
Analysis
  • The Cable Analysis Steps option will guide you
    through the steps for a cable prestress analysis.

26
GTSTRUDL Output WindowAnalysis Cable Prestress
Analysis Step 1
  • Define the cable network as well as sag and
    initial tension and the prestressing algorithm

27
GTSTRUDL Output WindowAnalysis Cable Prestress
Analysis Step 2
  • Specify Cable Prestress Analysis Control Data and
    the Prestress Loading Condition

28
GTSTRUDL Output WindowAnalysis Cable Prestress
Analysis Step 3
  • Execute the cable prestress analysis in Step 3
    (Perform Cable Prestress Analysis Command)

29
GTSTRUDL Output WindowResults
  • New results datasheets have been added for Member
    End Forces, Section Forces, and Section Stresses.
    The Joint Displacement datasheet has been
    revised. An example of the new Member End Forces
    datasheet is shown on the next slide.

30
GTSTRUDL Output WindowNew Member End Force
Datasheet
31
GTSTRUDL Output WindowNew Member End Force
Datasheet
  • In addition to the Sort and Filter functions that
    have been available in the Joint Displacement
    datasheet, you can now directly Print from the
    new datasheet

32
GTSTRUDL Output Window
  • The Dynamic Analysis Inactive Modes dialog now
    has an option which will write the active mode or
    all data to the Output Window in three columns
    with the mode number and descending mass
    participation percentages for the X, Y, and Z
    directions.

33
GTSTRUDL Output WindowInactive Mode Dialog
New Write to Text Window button
34
GTSTRUDL Output WindowOutput to Output Window
from Inactive Model Dialog
35
GTSTRUDL Output WindowSteel Design
  • A new option has been added to specify
    constraints of a section property to another
    section property of the same member. For
    example, constrain YDZD of the same member. The
    modified Constraint dialog is shown on the next
    slide.

36
GTSTRUDL Output WindowSteel Design Member
Constraints
37
GTSTRUDL Output WindowSteel Design Member
Constraints
  • Member constraints created using the dialog are
    now compressed so similar constraints are
    combined. Previously, user specified constraints
    were displayed one line per member.

38
GTSTRUDL Output WindowSteel Design
  • New parameters required to check and design the
    profiles added to the LRFD3 code have been added
    to the Parameters dialog. Also, the new LRFD3
    Tables have been added to the Parameters dialog.

39
GTSTRUDL Output WindowSteel Design
  • The Steel Design Wizard now allows you to bypass
    some of the steps using defaults that are
    commonly used.

40
GTSTRUDL Output WindowSteel Design
  • A new button has been added to the end of the
    Steel Design Wizard to create an input file (.gti
    file) and a database file (.gts). The input
    file contains analysis as well as the commands to
    execute the steel design process including
    PARAMETERS and CHECK commands.

41
GTSTRUDL Output WindowSteel Design
New Create Input File option
42
GTSTRUDL Output WindowSteel Design
  • Create Cross Section Proeprties has been modified
    to use GTSTRUDL to create the Tables. The
    advantage of using GTSTRUDL to create the Table
    is that user can use long pathname. Also a new
    default option has been added to the Create
    Database which allows the user to display the
    results.

43
GTMenu
  • Display model will now display the thickness of
    2D elements by color filling the interior of the
    element. Example is on the next slide.

44
GTMenuColor by thickness for finite elements
45
GTMenu
  • New Boundary Outline Option under the Display and
    Label Settings which will display the outline of
    edges where only one finite element is attached
    to an edge. This is useful for locating problems
    in finite element models where two regions are
    joined but a gap still exists even after removing
    duplicate joints

46
GTMenuBoundary Outline
  • Original model unable to see problem even after
    checking for duplicate joints with reasonable
    tolerance

47
GTMenuBoundary Outline
  • Example illustrating problems with model using
    boundary outline

48
GTMenuBoundary Outline
  • Display Label and Settings dialog has been
    modified to include Boundary Outline and Shrink
    settings

49
GTMenuBoundary Outline
  • The Boundary outline option is also available in
    the Display Model dialog and under the Options
    Model Display dialog.

50
GTMenu
  • Principal stresses may not be displayed using
    vectors for two-dimensional finite elements. The
    values of the principal stress as well as the
    angle with respect to the planar coordinate
    system may be labeled as shown on the next slide.

51
GTMenuPrincipal Stress Vectors
52
GTMenuPrincipal Stress Vectors
53
GTMenuPrincipal Stress Vectors
  • New dialog for principal stress vectors

54
GTMenu
  • Member forces at the ends of members may now be
    labeled (listed) on the graphical display of the
    structure.

55
GTMenu
  • New dialog for member force listing. Components
    can be selected as well as the start and end of
    the members.

56
GTMenuMember force listing
57
GTMenuMember Force listing
  • The member forces may also be output in the
    Inquire Output pop-up

58
GTMenu
  • New HotKey sequences have been added for the
    Display Window to label joints, members, and
    elements
  • LJ Label Joints
  • LM Label Members and Finite Elements
  • LA Label all joints, members, and finite
    elements
  • Other New HotKeys
  • W to initiate Windowing (Zoom) on the display
  • lt and gt to rotate structure in the plane of the
    screen
  • A to redraw the screen (again)

59
GTMenu
  • A new button has been added to the Create
    Supports dialog to Draw Supports

60
GTMenu
  • Table section longnames are displayed in Display
    Model and also listed using Inquire in the Output
    Box

61
GTMenu
  • When a duplicate is found, the original name is
    now displayed in addition to the duplicate name

62
GTMenuDuplicate Joints
  • The Duplicate Joint, Member, and Element dialogs
    and the Floating Joint dialog now have the option
    to send the output to a File or the Output Window
    as shown on the previous slide.
  • The information sent to a File or the Output
    Window now has a line describing how the output
    was produced as shown below.

63
GTMenu
  • Label settings are now saved in a given session
    and are retained when cycling between GTMenu and
    the GTSTRUDL Output Window
  • A scroll bar has been added to allow viewing long
    load titles and dependent load descriptions
  • The Create Member Property Prismatic and Create
    Material Group dialogs now have a button which
    will bring up the Calculator pop-up to facilitate
    the computation of properties.

64
GTMenu
  • When creating a new loading, all currently used
    load names are now listed and classified to help
    in choosing the name for a new loading.

65
GTMenu
  • A new option to create joints has been
    implemented. This option creates the joints by
    intersecting coordinates or spacing along one of
    the global axes with any number of lines.

66
GTMenuProject Axis on Lines
  • New option under Create Joints to Project Axis on
    Lines

67
GTMenuProject Axis on Lines
  • Specify lines to project axis onto
  • Lines

68
GTMenuProject Axis on Lines
  • Specify spacing in a table

69
GTMenuProject Axis on Lines
  • New joints are then created on lines using the
    coordinates or spacing from the table on the
    previous slide

70
GTMenu
  • GTMenu Point Coordinates and Lines are now
    written to the GTMenu Input File. Two new
    commands have been implemented to read the Point
    and Line information
  • GTMenu Point Coordinates
  • GTMenu Line Incidences

71
GTMenuInput File with Points and Lines
  • Example of the Point and Line data now in the
    input file is shown below

72
GTMenu
  • The GTMenu input file generator can now be
    accessed from Command Mode by the following
    command
  • GTMenu Generate Input File filename

73
GTMenu
  • A minimum of twenty-one (21) sections are now
    used by default to compute a member diagram or
    envelope regardless of section specifications.
    Eleven (11) sections are used to draw the
    deformed shape of a member.
  • The boundary nodes of a Superelement can be
    listed in GTMenu in an Inquire box by specifying
    the name of the Superelement in list mode.

74
GTMenu
  • When labeling the displacements on a deformed
    shape between the ends of a member, a preview
    line has been implemented which points to the
    nearest section location where the displacements
    will be labeled.

75
GTMenu
  • Appropriate linking buttons have been added to
    the Line/Curve dialog. These buttons allow the
    user to go directly to the Create Members or
    Create Elements dialogs as shown on the next
    slide.
  • Linking buttons have also been added to the
    Translate Joints to Points and Create Points in
    Circular Arc dialogs.

76
GTMenuLinking buttons in Create Line dialog
Linking buttons to go directly to Generate dialogs
77
GTMenu
  • Section property groups are now alphabetized to
    make selection easier when choosing a Section
    property for a member
  • When using Print Preview and Edit in GTMenu, the
    Scope Editor file is now automatically Saved
    without a name change. The default file name has
    been changed to Temp00x.SSC.

78
Dynamics
  • The INERTIA OF JOINTS FROM LOAD command has been
    extended to include the conversion of
    translational force load components of both
    member and finite element loads to translational
    joint masses. Member loads are no longer
    converted to Member Added Mass but are converted
    directly to joint inertias. You can use the
    PRINT DYNAMIC JOINT INERTIA command to verify
    this.

79
Dynamics
  • Efficiency improvements have been made to the
    assembly of dynamic mass and composite modal
    damping matrices. Models which contained rigid
    bodies and a large number of specified damping
    ratios for joint inertias are now able to
    assemble.

80
Dynamics
  • Efficiency improvements have been made with
    regard to the assembly and use of the damping
    matrix for dynamic analyses. When damping data
    have been specified, the damping matrix is now
    assembled on demand and only when needed. For
    instance, the following sequence does not require
    damping matrices to be assembled
  • Assemble for Dynamics
  • Perform Eigenvalue Analysis

81
Finite Elements
  • The CALCULATE SOIL SPRING VALUES command has been
    modified to allow the creation of in-plane
    springs and compression only springs. The
    in-plane springs will be a ratio of the normal
    springs. The compression only springs will be
    modeled using nonlinear spring elements which
    will be created automatically.

82
General
  • The DEAD LOAD and SELF WEIGHT commands have been
    enhanced to include two- and three-dimensional
    finite elements in the computation of element and
    joint dead loads.
  • The SUMMARY for LIST SECTION FORCES now has an
    option to include corresponding forces, e.g. for
    the section and load that causes the max MZ, you
    can also get the associated FX and FY.

83
General
  • The UNITS command has been modified to include
    mass units as follows
  • STANDARD
  • STDMASS
  • UNITS GRAM
  • KGM
  • MTNM

84
General
  • New commands have been implemented to delete
    joints or members that do not have any data
    associated with them
  • DELETE JOINTS WITHOUT JOINT - COORDINATES
  • DELETE MEMBERS WITHOUT -
  • MEMBER INCIDENCES
  • DELETE ELEMENTS WITHOUT - ELEMENT INCIDENCES

85
General
  • A new AREA LOAD command has been added. The AREA
    LOAD command is used to distribute loadings over
    defined regions of a structure to surrounding
    members as member loads. The member loads are
    applied in a global direction. The area must be
    completed enclosed by members. One way or two
    way load distribution options are available.

86
GeneralArea Load
87
General
  • New LIST SUM FORCES command which may be used to
    calculate and report the summation of forces and
    moments at a specified point from a specified set
    of member and finite element nodal forces for
    all active static loading conditions. This
    command is similar to, but more general than, the
    CALCULATE RESULTANT command.

88
GeneralLIST SUM FORCES
89
GeneralLIST SUM FORCES
  • The force and moment summation is computed for
    all active static loading conditions for which
    member end forces and finite element nodal forces
    have been computed by a prior STIFFNESS ANALYSIS
    or by the CREATE PSEUDO STATIC, COMBINE, and
    CREATE LOAD COMBINATION commands.

90
GeneralLIST SUM FORCES
  • In the case of a pseudo static loading condition
    created from a response spectrum modal
    combination such as RMS or CQC, a force and
    moment summation is computed first for each mode
    of the root response spectrum load. The final
    mode combination force and moment summation is
    then computed by applying the mode combination
    rule of the pseudo static loading to the
    individual modal force and moment summations.

91
GTTABLE
  • GTTABLE commands that are used to create table
    database are now available in GTSTRUDL. This
    means that you can use GTSTRUDL to create a table
    database. Table input files now can be executed
    by GTSTRUDL or GTTABLE.

92
New Static Analysis Solver
  • A new static analysis solver has been implemented
    which is based on a blocked active column solver.
    The new solver is used when the following
    command is issued
  • STIFFNESS ANALYSIS GTHCS
  • where GTHCS stands for Georgia Tech Hyper-Column
    Solver.
  • This solver is more efficient for very large
    problems and will solve problems which might not
    otherwise be solved due to the 2GB Windows
    limitation.

93
New Static Analysis Solver
  • An example of the efficiency of the new static
    solver versus the existing solver is shown below
  • Number of Joints 14,698 (6DOF)
  • Band 468
  • Time to solve using existing solver 4,242 sec
  • Time to solve using GTHCS solver 2,840 sec

94
Nonlinear Analysis
  • Pushover Analysis will be brought to release
    status in Version 28.
  • Pushover Analysis now contains a new switchable
    displacement control option. When displacement
    control is enabled and a pushover analysis load
    increment encounters convergence difficulties,
    the pushover analysis will switch to displacement
    control. The user may select joint displacement
    dofs to monitor and control.

95
Nonlinear Analysis
  • The primary stress-strain model due to Toader,
    Popov, et.al. used in plastic hinge analysis has
    been replaced by the more widely known models
    described by Priestley, et.al.
  • The LIST CABLE LENGTHS command has been added for
    the output of the computed unstressed length of
    cable elements.

96
Nonlinear Dynamic Analysis
  • Nonlinear dynamic analysis now supports the
    assembly of proportional and non-proportional
    stiffness and damping matrices from all sources.
    In previous versions, the damping factors from
    the CONSTANTS command were not supported.

97
Scope Editor
  • You can now Copy and Paste from the clipboard.
    This allows copying from one Scope Editor (.SSC)
    file to another.
  • You can now create a paragraph of text. The new
    Paragraph option is available under Tools. An
    example is shown on the next slide.

98
Scope Editor
Paragraph created using the new Paragraph option
99
Scope Editor
  • New options are now available which will create
    only Horizontal or Vertical lines.
  • You can now edit line end points. This will
    allow you to zoom in and properly connect
    intersecting lines which is especially useful
    when creating a border for a template.
  • A Time/Date stamp is now available under Tools.

100
Steel Tables
  • The following tables from AISC LRFD Third Edition
    have been implemented
  • 2L-EQ-L3 Equal legs Double Angle, 2L, shapes from
    Table 1-14.
  • 2L-LL-L3 Long legs back-to-back Double Angle,
    2L, shapes from Table 1-14.
  • 2L-SL-L3 Short legs back-to-back Double Angles,
    2L, shapes from Table 1-14.
  • 2LALL-L3 All Double Angles, 2L, shapes from Table
    1-14. This includes equal legs, long legs, and
    short legs back-to-back shapes.

101
Steel TablesAISC LRFD Third Edition
  • W-LRFD3W shapes from Table 1-1.
  • M/S/HPL3 M, S, and HP shapes from Tables
  • 1-2, 1-3, and 1-4.
  • C-LRFD3 American Standard Channels and
    Miscellaneous Channels from Tables 1-5 and 1-6.
  • WT-LRFD3 Structural Tees split from W, M, and S
    shapes included in Tables 1-8, 1-9, and 1-10.

102
Steel Design
  • Three new cross-sections have been added to the
    LRFD3 code. The new cross-sections are Channel,
    Tee, and Plate Girder. You may design and code
    check based on axial and bending effects for
    these cross-sections. One new parameter has been
    added for the channel cross-section and 10 new
    parameters for the plate girder cross-section.

103
Steel Design
  • Double angle cross-sections under bi-axial
    bending now can be designed and code checked
    based on the LRFD3 code. Previously, double
    angle cross-sections could be code checked based
    on the tension or compression force only. Now,
    you can code check or design double angles based
    on axial and bending effects. LRFD3 code check
    for double angles considers members under tension
    , compression considering flexural-torsional
    buckling, modified column slenderness, check or
    design number of connectors, major and minor axis
    bending checks, major and minor axis shear
    checks, and combined axial and bending check.
    Three new parameters have been added for the
    double angle cross-sections code check based on
    the LRFD3 code.

104
Steel Design
  • User specified values for yield and tensile
    strength parameters (FYLD, FTS, Py, Fy, Fu, etc.)
    are now checked for a range of possible valid
    values. There are times that the user specifies
    yield or tensile strength values (parameter FYLD,
    FTS, Py, Fy, Fu, etc.) in the wrong units or
    mistypes the parameter values which may result in
    an incorrect code check. If the user specified
    values for yield or tensile strength which is
    smaller than 20.0 ksi (24.82 MPa) or larger than
    200.0 ksi (8963.18 MPa), a warning message is
    issued.

105
Steel Design
  • Joint, member, and load list options of the steel
    design and connection design commands are now
    checked for non-existing joints, members, or
    loads. If a user specifies joint, member, or
    load names that do not exist, an error message
    will be output listing the user specified joints,
    members, or loads that do not exist.

106
New Cell Tower Add-On Module
  • A new Add-On Module will be available for the
    automated modeling, analysis, and design of
    monopole and latticed cell towers. Rob Abernathy
    will be presenting this later today and seeking
    input from you.

107
Future Enhancements
  • New optional dynamic analysis eigenvalue equation
    solvers and data structures which bypass
    Microsofts 2GB limitation on the page file.
  • Efficiency improvements in Steel Design for large
    models - especially those with a large number of
    design loading conditions.

108
Future Enhancements (cont)
  • Graphically specify Area Loads
  • Allow a 2-point line to be specified using "Start
    and End" mode, as for Member generation.
    Currently "End to End" mode is assumed.
  • Expand the Member and Element generation Spacing
    option, "Defined by Line/Curve", to accept an
    n-point line of up to 500 segments. Currently it
    is limited to 50 segments

109
Future Enhancements (cont)
  • Multiple windows to allow for result display in a
    separate window than the model display
  • Graphically specify joints and elements to be
    used with CALCULATE RESULTANT
  • Label Values on Diagrams and Envelopes
    automatically max and mins
  • Mirror option under Copy Model in GTMenu
  • List the contents of a Group in an Inquire box.
    Currently the contents can only be displayed
    graphically

110
Future Enhancements (cont)
  • Add the option to Split Members to interpolate
    eccentricities between the start and end of the
    split members
  • Locate a Global Plane with a pick on the
    structure. Currently a Global Plane requires a
    coordinate value
  • Ability to click on a member and have a graphical
    summary of the results on just that member in a
    separate Window that can be printed

111
Future Enhancements (cont)
  • SELECT or CHECK based on maximum forces
  • Modify ASD9 code to allow for E to be specified
    such as when designing in a high temperature
    environment
  • ACI 318-2002

112
Future Enhancements (cont)
  • Continue expanding the model data and results
    which are available in Data Sheets. Use the new
    datasheets which allow printing.
  • Select reinforcing steel for concrete slabs
    analyzed with finite elements.
  • Design of steel structures subjected to
    displacement constraints.

113
Future Enhancements (cont)
  • Graphically display plastic hinge status and
    other pushover information
  • Create nonlinear spring and cable information in
    the input file created by GTMenu

114
Future Enhancements (cont)
  • ISO 2000 equivalent static earthquake load
  • Hysteretic behavior for plastic hinges and
    nonlinear member end connections
  • Custom cross-section fiber geometry specification
    for plastic hinges using basic circles, rings,
    and rectangle areas

115
Future Enhancements (cont)
  • Generalizing nonlinear frame member model to
    support large finite rotation behavior
  • Center of stiffness computation in dynamic
    analysis

116
What do we need?
  • As you break out into your committees, please
    provide us with a prioritized list of the
    features that you would like to see. Please be
    specific especially when requesting model wizard,
    design codes (which codes and which cross
    sections) or datasheet requests.
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