Version: Next

11. Results

11.1 Static Analysis Results

11.1.1 Load Combinations

Function: Input load combinations.
Command:

Select "Results" > "Load Combinations" from the main menu;

Load Combination Window Operation Load Combination Window Operation

Input
- Name
  
  Name of the load combination.
- Type
  - Superposition: Linearly superpose the results of each load case, outputting only one result item.
  - Discrimination: Superpose the analysis results of each load case after judgment, outputting Max, Min, and All three result items. If the result of a load case is greater than 0, it is superposed in Max; if the result is less than 0, it is superposed in Min; All is the maximum absolute value of Max and Min.
  - Envelope: Obtain the envelope value of each load case result, outputting Max, Min, and All three result items. Max is the maximum value of each load case result, Min is the minimum value of each load case result, All is the maximum absolute value of Max and Min.
  - Square Root of Sum of Squares (SRSS): Treat the response of each random variable as an independent random variable, and use the statistical square root of sum of squares rule to combine the effects of multiple random variables, outputting the SRSS result.
    - For multiple independent random variables $X_{1}, X_{2},..., X_{n},$ each random variable has a coefficient $a_{1}, a_{2},..., a_{n},$ the calculation expression of the SRSS method is:
    $\mathrm{S R S S}={\sqrt{( a_{1} X_{1} )^{2}+( a_{2} X_{2} )^{2}+...+( a_{n} X_{n} )^{2}}}$
  - Absolute Sum (ABSSUM): Used for quickly assessing the maximum load a structure may be subjected to under multiple load cases. By assuming that the maximum responses of all load cases occur simultaneously, the absolute values of the maximum responses of each load case (regardless of direction) are added together to output a total response estimate ABSSUM.
    - For multiple random variables $X_{1}, X_{2},..., X_{n},$ each random variable has a coefficient $a_{1}, a_{2},..., a_{n},$ the calculation expression of the ABSSUM method is:
    $ABSSUM= |a_1 X_1| + |a_2X_2| + ...+ |a_nX_n |$
  - Permanent Force Others Discrimination: Except for permanent action type loads (bridge completion total and components, dead load action types in additional load cases) which use forced superposition, the analysis results of other type load cases are superposed after judgment, outputting Max, Min, and All three result items. If the result of a load case is greater than 0, it is superposed in Max; if the result is less than 0, it is superposed in Min; All is the maximum absolute value of Max and Min.
- Description
  
  Description of the load combination.
- Load Cases
  
  Select load cases participating in the load combination from the load case list.
- Load Factors
  
  Input the combination coefficients for the selected load cases participating in the load combination.

11.1.2 Reactions

Function: View reaction results.
Command:

Select "Results" > "Results" > "Reactions" from the main menu;

Select "Results" > "Tables" > "Reactions" from the main menu;

Reaction Window Operation Reaction Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view reactions.
- Components
  
  Select the component type of reactions to view:
  
  FX: Reaction component in the X-axis direction of the global coordinate system or x direction of the node local coordinate system.
  
  FY: Reaction component in the Y-axis direction of the global coordinate system or y direction of the node local coordinate system.
  
  FZ: Reaction component in the Z-axis direction of the global coordinate system or z direction of the node local coordinate system.
  
  FXYZ: Output FX, FY, FZ simultaneously.
  
  MX: Moment reaction component about the X-axis of the global coordinate system or x-axis of the node local coordinate system.
  
  MY: Moment reaction component about the Y-axis of the global coordinate system or y-axis of the node local coordinate system.
  
  MZ: Moment reaction component about the X-axis of the global coordinate system or z-axis of the node local coordinate system.
  
  MXYZ: Output MX, MY, MZ simultaneously.
  
  🧐Note: If the node local coordinate system where the support is located has been defined, the viewed reaction components are node local coordinate system results.
- Display Type
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Arrow Size Scale: Scale of reaction arrow size on the model interface.

11.1.3 Deformation

Function: View deformation results.
Command:

Select "Results" > "Deformation" from the main menu;

Deformation Window Operation Deformation Window Operation

Input

Load Case/Combination

Select the load case/combination for which to view deformation.

Components

Select the component type of deformation to view:


DX	Deformation component in the X-axis direction of the global coordinate system
DY	Deformation component in the Y-axis direction of the global coordinate system
DZ	Deformation component in the Z-axis direction of the global coordinate system
RX	Rotation component about the X-axis of the global coordinate system
RY	Rotation component about the Y-axis of the global coordinate system
RZ	Rotation component about the X-axis of the global coordinate system
DXY	√(DX^2+DY^2)
DYZ	√(DY^2+DZ^2)
DXZ	√(DX^2+DZ^2)
DXYZ	√(DX^2+DY^2+DZ^2)

Display Type

Contour

Deformation: Display deformation shape on the model interface

Values: Display values on the model interface.

Legend: Display legend on the model interface.

Before Deformation: Display shape before deformation on the model interface.

11.1.4 Concurrent Reactions

11.1.4.1 Self-Concurrent Reactions (Table Only)

Function: View concurrent reactions of live loads or support settlement loads. That is, the extreme value results of each support reaction component and the values of other reaction components of the same support occurring simultaneously. Currently supports querying self-concurrent results of live load cases, support settlement cases, and load combinations containing the above type cases.
Note: Live load fatigue related cases do not output self-concurrent reactions.
Command:

Select "Results" > "Tables" > "Self-Concurrent Reactions" from the main menu;
Input
- Support Nodes
  
  Select support nodes.
- Selection Type
  
  Can quickly add support nodes through selection type.
- Load Case/Load Combination
  
  Select live load cases, support settlement cases, and load combinations containing the above type cases for which to view results.
- Display Items
  
  Select reaction components to view self-concurrent reaction results of each support when the extreme value of that component occurs.

11.1.4.2 Fully Concurrent Reactions (Table Only)

Function: View fully concurrent reaction results, that is, the extreme value results of each support reaction component, other reaction components of the same support occurring simultaneously, and reaction values of all other supports occurring simultaneously. Currently only supports querying fully concurrent results of support settlement cases and load combinations containing settlement cases.
Note: Settlement cases and live load cases (except fatigue related live load cases) output fully self-concurrent reactions, and live load calculation requires checking whether to track before calculation.
Command:

Select "Results" > "Tables" > "Fully Concurrent Reactions" from the main menu;
Input
- Support Nodes
  
  Select support nodes.
- Selection Type
  
  Can quickly add support nodes through selection type.
- Load Case/Load Combination
  
  Select live load cases, support settlement cases, and load combinations containing the above type cases for which to view results.

11.1.5 Concurrent Internal Forces

Function: View self-concurrent internal force results of beam elements or composite beam elements, that is, the extreme value results of each beam element's internal force component and the values of other internal force components of the same element occurring simultaneously. Currently supports querying self-concurrent results of live load cases, support settlement cases, and load combinations containing the above type cases.
Command:

Select "Results" > "Tables" > "Beam Element Self-Concurrent Internal Forces" or "Composite Beam Element Self-Concurrent Internal Forces" from the main menu;
Input
- Element
  
  Select beam or composite beam element numbers.
- Selection Type
  
  Can quickly add elements through selection element type, structure group, etc.
- Load Case/Load Combination
  
  Select live load cases, support settlement cases, and load combinations containing the above type cases for which to view results.
- Position Number
  
  Select I/J end of the element to view self-concurrent internal force results of each element when the extreme value at that end occurs.
- Display Items
  
  Select internal force components to view self-concurrent internal force results of each element when the extreme value of that component occurs.

11.1.6 Node Displacements

Function: View node displacement results.
Command:

Select "Results" > "Tables" > "Node Displacements" from the main menu;
Table Display

Node: Node number

Load: Load case/combination

DX: Displacement component in X direction under global coordinate system

DY: Displacement component in Y direction under global coordinate system

DZ: Displacement component in Z direction under global coordinate system

RX: Rotation component about X axis under global coordinate system

RY: Rotation component about Y axis under global coordinate system

RZ: Rotation component about Z axis under global coordinate system

11.1.7 Truss Element Internal Forces

Function: View truss internal force results.
Command:

Select "Results" > "Results" > "Internal Forces" > "Truss Element Internal Forces" from the main menu;

Select "Results" > "Tables" > "Internal Forces" > "Truss Element Internal Forces" from the main menu;

Truss Element Internal Forces Window Operation Truss Element Internal Forces Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view internal forces.
- Display Type
  
  Line Chart: Display line chart on the model interface.
  
  Deformation: Display deformation shape on the model interface
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Before Deformation: Display shape before deformation on the model interface.

11.1.8 Beam Element Internal Forces

Function: View beam internal force results.
Command:

Select "Results" > "Results" > "Internal Forces" > "Beam Element Internal Forces" from the main menu;

Select "Results" > "Tables" > "Internal Forces" > "Beam Element Internal Forces" from the main menu;

Beam Element Internal Forces Window Operation Beam Element Internal Forces Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view internal forces.
- Components
  
  Select the component type of internal forces to view:
  
  Fx: Axial force.
  
  Fy: Shear force in the y direction of the element local coordinate system.
  
  Fz: Shear force in the z direction of the element local coordinate system.
  
  Mx: Moment about the x-axis of the element local coordinate system.
  
  My: Moment about the y-axis of the element local coordinate system.
  
  Mz: Moment about the z-axis of the element local coordinate system.
- Display Type
  
  Line Chart: Display line chart on the model interface.
  
  Deformation: Display deformation shape on the model interface
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Before Deformation: Display shape before deformation on the model interface.

11.1.9 Composite Beam Element Internal Forces

Function: View composite beam internal force results.
Command:

Select "Results" > "Results" > "Internal Forces" > "Composite Beam Element Internal Forces" from the main menu;

Select "Results" > "Tables" > "Internal Forces" > "Composite Beam Element Internal Forces" from the main menu;

Composite Beam Element Internal Forces Window Operation Composite Beam Element Internal Forces Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view internal forces.
- Section
  
  Select whether to calculate main material separately, auxiliary material separately, or main material + auxiliary material.
- Components
  
  Select the component type of internal forces to view:
  
  Fx: Axial force.
  
  Fy: Shear force in the y direction of the element local coordinate system.
  
  Fz: Shear force in the z direction of the element local coordinate system.
  
  Mx: Moment about the x-axis of the element local coordinate system.
  
  My: Moment about the y-axis of the element local coordinate system.
  
  Mz: Moment about the z-axis of the element local coordinate system.
- Display Type
  
  Line Chart: Display line chart on the model interface.
  
  Deformation: Display deformation shape on the model interface
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Before Deformation: Display shape before deformation on the model interface.

11.1.10 Plate Element Internal Forces

Function: View plate internal force results.
Command:

Select "Results" > "Results" > "Internal Forces" > "Plate Element Internal Forces" from the main menu;

Select "Results" > "Tables" > "Internal Forces" > "Plate Element Internal Forces" from the main menu;

Plate Element Internal Forces Window Operation Plate Element Internal Forces Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view internal forces.
- Internal Force Options
  
  Element: Display contours using stresses at each node of the element.
  
  Node Average: Display contours using average node stresses at shared node positions of elements sharing the node.
- Components
  
  Select the component type of internal forces to view:
  
  Element Coordinate System: Output internal force distribution per unit width along each plate element local coordinate system direction.
  ❓ $F_{ij}$ : $i$ -force action plane, $j$ -force action direction, sign convention:
  - When the normal direction of the force action plane is consistent with a certain element coordinate axis direction, and the force action direction j is consistent with the element coordinate axis direction, it is positive (+);
  - When the normal direction of the force action plane is opposite to a certain element coordinate axis direction, and the force action direction j is opposite to the element coordinate axis direction, it is positive (+). $M_{ij}$ : $i$ -force action plane, $j$ -axis parallel to moment rotation direction, sign convention:
  - When i≠j, according to the right-hand rule, when the thumb direction is consistent with the normal direction of the force action plane, it is positive (+);
  - When i=j, when the positive/top surface of the plate (normal direction action surface) is in tension during moment action, it is positive (+). Fxx: Axial force per unit width in the x direction of the element local coordinate system.
  Fyy: Axial force per unit width in the y direction of the element local coordinate system.
  
  Fxy: Shear force per unit width in the x-y plane of the element local coordinate system or user coordinate system (in-plane shear) (Fxy=Fyx).
  
  Mxx: Moment per unit width about the x-axis of the element local coordinate system.
  
  Myy: Moment per unit width about the y-axis of the element local coordinate system.
  
  Mxy: Torque per unit width acting in the plane perpendicular to the x-axis of the local coordinate system or user coordinate system, rotating about the x-axis (Mxy=Myx).
- Display Type
  
  Deformation: Display deformation shape on the model interface
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Before Deformation: Display shape before deformation on the model interface.

11.1.11 Truss Element Stresses

Function: View truss stress results.
Command:

Select "Results" > "Results" > "Stresses" > "Truss Element Stresses" from the main menu;

Select "Results" > "Tables" > "Stresses" > "Truss Element Stresses" from the main menu;

Truss Element Stresses Window Operation Truss Element Stresses Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view stresses.
- Display Type
  
  Line Chart: Display line chart on the model interface.
  
  Deformation: Display deformation shape on the model interface
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Before Deformation: Display shape before deformation on the model interface.

11.1.12 Beam Element Stresses

Function: View beam stress results.
Command:

Select "Results" > "Results" > "Stresses" > "Beam Element Stresses" from the main menu;

Select "Results" > "Tables" > "Stresses" > "Beam Element Stresses" from the main menu;

Beam Element Stresses Window Operation Beam Element Stresses Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view stresses.
- Stresses
  
  Select the component type of stresses to view:
  
  Axial Force Component: Axial stress produced by axial force.
  
  Mz Component: Stress produced by moment about the z-axis of the element local coordinate system.
  
  My Component: Stress produced by moment about the z-axis of the element local coordinate system.
  
  Combined: Stress produced by axial force plus moments in two directions.
  
  Calculation position can select envelope (selecting the maximum value of combined stress among four points), upper left, upper right, lower right, lower left
- Display Type
  
  Line Chart: Display line chart on the model interface.
  
  Deformation: Display deformation shape on the model interface
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Before Deformation: Display shape before deformation on the model interface.

11.1.13 Composite Beam Element Stresses

Function: View composite beam stress results.
Command:

Select "Results" > "Results" > "Stresses" > "Composite Beam Element Stresses" from the main menu;

Select "Results" > "Tables" > "Stresses" > "Composite Beam Element Stresses" from the main menu;

Composite Beam Element Stresses Window Operation Composite Beam Element Stresses Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view stresses.
- Section
  
  Select whether to calculate main material separately, auxiliary material separately, or main material + auxiliary material.
- Stresses
  
  Select the component type of stresses to view:
  
  Axial Force Component: Axial stress produced by axial force.
  
  Mz Component: Stress produced by moment about the z-axis of the element local coordinate system.
  
  My Component: Stress produced by moment about the z-axis of the element local coordinate system.
  
  Combined: Stress produced by axial force plus moments in two directions.
  
  Calculation position can select envelope (selecting the maximum value of combined stress among four points), upper left, upper right, lower right, lower left
- Display Type
  
  Line Chart: Display line chart on the model interface.
  
  Deformation: Display deformation shape on the model interface
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Before Deformation: Display shape before deformation on the model interface.

11.1.14 Plate Element Stresses

Function: View plate stress results.
Command:

Select "Results" > "Results" > "Stresses" > "Plate Element Stresses" from the main menu;

Select "Results" > "Tables" > "Stresses" > "Plate Element Stresses" from the main menu;

Plate Element Stresses Window Operation Plate Element Stresses Window Operation

Input
- Load Case/Combination
  
  Select the load case/combination for which to view stresses.
- Internal Force Options
  
  Element: Display contours using stresses at each node of the element.
  
  Node Average: Display contours using average node stresses at shared node positions of elements sharing the node.
- Position
  
  Plate Top: Stress at the top edge in the z direction of the plate element local coordinate system.
  
  Plate Bottom: Stress at the bottom edge in the z direction of the plate element local coordinate system.
  
  Maximum Absolute Value: Maximum value among absolute values of stresses at the top and bottom surfaces.
- Components
  
  Select the component type of stresses to view:
  
  Sigxx: Axial force stress in the x direction of the element local coordinate system.
  
  Sigyy: Axial force stress in the y direction of the element local coordinate system.
  
  Sigxy: Shear stress in the x-y plane of the element local coordinate system.
- Display Type
  
  Deformation: Display deformation shape on the model interface
  
  Values: Display values on the model interface.
  
  Legend: Display legend on the model interface.
  
  Before Deformation: Display shape before deformation on the model interface.

11.1.15 Constraint Equations (Table Only)

Function: View constraint equations.
Command:

Select "Results" > "Tables" > "Constraint Equations" from the main menu;

Constraint Equations Window Operation Constraint Equations Window Operation

Input
- Constraint Equations
  
  Select constraint equations.
- Selection Type
  
  Can quickly add constraint equations through selection type.

11.1.16 Elastic Links (Table Only)

Function: View elastic link results.
Command:

Select "Results" > "Tables" > "Elastic Links" from the main menu;

Elastic Links Window Operation Elastic Links Window Operation

Input
- Elastic Links
  
  Select elastic links.
- Selection Type
  
  Can quickly add elastic links through selection type.

11.1.17 Cable Element Unstressed Length

Function: View unstressed cable length of cable elements.
Command:

Select "Results > Static Analysis > Unstressed Cable Length" from the main menu;
Input
- Element
  
  Select cable elements.
- Selection Type
  
  Can quickly add cable elements through selection type.

11.1.18 Prestressing Tendon Results

Not yet available

11.1.19 Construction Stage Warning Settings

Function: Whether to perform construction stage warning, set warning items.
Command: Select "Results > Construction Stage Warning > Warning Settings" from the main menu;

Input
- Construction Stage Warning
  
  Check this item to automatically perform construction stage result warning calculation after construction stage calculation is completed (or after opening a project with construction stage results). If there are over-limit results, an alarm will be issued immediately.
- Start Construction Stage
  
  Set the start construction stage for result warning calculation.
- End Construction Stage
  
  Set the end construction stage for result warning calculation.
- Member Internal Force Warning
  
  Set internal force warning items for rod, beam, cable, plate, and composite beam elements.
  
  Structure Group: Perform warning analysis on internal forces of members in the structure group.
  
  Internal Force Components: Specify unit internal force components for warning, including Fx, Fy, Fz, Mx, My, Mz.
  
  Internal Force Upper Limit: If unit internal force is higher than this value, an alarm will be issued.
  
  Internal Force Lower Limit: If unit internal force is lower than this value, an alarm will be issued.
- Member Stress Warning
  
  Set stress warning items for rod, beam, cable, and plate elements.
  
  Structure Group: Perform warning analysis on member stresses in the structure group (except composite beams).
  
  Limit Definition Method: Includes two definition methods, 1) User-defined; 2) Design strength/Safety factor.
  
  Stress Upper Limit: User-defined method, if unit stress is higher than this value, an alarm will be issued.
  
  Stress Lower Limit: User-defined method, if unit stress is lower than this value, an alarm will be issued.
  
  Safety Factor: Design strength divided by safety factor method, the program automatically obtains design tensile and compressive strengths based on the unit's material type, and determines stress upper and lower limit values after dividing by the safety factor.
- Composite Beam Stress Warning
  
  Set stress warning items for composite beam elements.
  
  Structure Group: Perform warning analysis on composite beam stresses in the structure group.
  
  Limit Definition Method: Includes two definition methods, 1) User-defined; 2) Design strength/Safety factor.
  
  Main/Auxiliary Material Stress Upper Limit: User-defined method, if the unit's main/auxiliary material stress is higher than this value, an alarm will be issued.
  
  Main/Auxiliary Material Stress Lower Limit: User-defined method, if the unit's main/auxiliary material stress is lower than this value, an alarm will be issued.
  
  Safety Factor: Design strength divided by safety factor method, the program automatically obtains design tensile and compressive strengths based on the unit's material type, and determines stress upper and lower limit values after dividing by the safety factor.
- Support Reaction Warning
  
  Set warning items for support reactions, elastic link forces, and constraint equation forces.
  
  Boundary Group: Perform warning analysis on support reactions, elastic link forces, and constraint equation forces in the boundary group.
  
  Reaction Components: Specify reaction components for warning, including Fx, Fy, Fz, Mx, My, Mz.
  
  Reaction Upper Limit: If reaction component is higher than this value, an alarm will be issued.
  
  Reaction Lower Limit: If reaction component is lower than this value, an alarm will be issued.
  
  You can batch add warning items for specified structure groups or boundary groups, delete all or specified warning items, and directly edit warning items in the warning item table. After warning settings are completed, click OK to start warning analysis.

11.1.20 Warning Results

Function: View warning result table.
Command: Select "Results > Construction Stage Warning > Warning Results" from the main menu, click OK.

Input
- Construction Stage Member Internal Force/Stress Warning
  
  Select element type to display warning internal force and stress results.
- Construction Stage Reaction Warning
  
  Select constraint type to display warning reaction results.
- Construction Stage
  
  Select construction stage to display warning results.

11.1.21 Warning Display

Function: View warning result graphics.
Command: Select "Results > Construction Stage Warning > Warning Display" from the main menu.

Input
- Member Internal Force Over-limit: Display over-limit internal force results of rod, beam, cable, plate, and composite beam elements.
  
  Construction Stage: Select construction stage to display over-limit results.
  
  Over-limit Type: Select over-limit result type, including all, exceeding upper limit, below lower limit.
  
  Values: Whether to display specific over-limit values.
- Member Stress Over-limit: Display over-limit stress results of rod, beam, cable, and plate elements.
  
  Construction Stage: Select construction stage to display over-limit results.
  
  Over-limit Type: Select over-limit result type, including all, exceeding upper limit, below lower limit.
  
  Values: Whether to display specific over-limit values.
- Composite Beam Internal Force Over-limit: Display over-limit internal force results of composite beam elements.
  
  Construction Stage: Select construction stage to display over-limit results.
  
  Over-limit Type: Select over-limit result type, including all, main material exceeding upper limit, main material below lower limit, auxiliary material exceeding upper limit, auxiliary material below lower limit.
  
  Values: Whether to display specific over-limit values.
- Support Reaction Over-limit: Display over-limit results of support reactions, elastic link forces, and constraint equation forces.
  
  Construction Stage: Select construction stage to display over-limit results.
  
  Over-limit Type: Select over-limit result type, including all, exceeding upper limit, below lower limit.
  
  Values: Whether to display specific over-limit values.

11.1.22 Generate Verification Cases

Function: Perform further verification on over-limit reinforced concrete and prestressed concrete members, and generate verification reports.
Command: Select "Results > Construction Stage Warning > Generate Verification Cases" from the main menu.

Case Name: User fills in the name of the generated verification case.

Material Type: Select materials of members to be verified.

Code: Select verification code. Currently supports two codes, "Code for Design of Highway Reinforced Concrete and Prestressed Concrete Bridges and Culverts" (JTG3362-2018), and "Code for Design of Concrete Structures of Railway Bridges and Culverts" (TB10092-2017 J462-2017).

Structure Type: Includes reinforced concrete members, fully prestressed members, Class A members, and Class B members.

After determining the above input items, click "Generate Verification Cases" to enter the concrete structure verification case page, see 12. Verification.

11.2 Dynamic Analysis Results

11.2.1 Table Result Output

11.2.1.1 Time History Tables

(1) Node Reactions

Function: Output time history data of single node reactions.
Command: Results > Time History Tables > Node Reactions

Node Reaction Table Activation Dialog Node Reaction Table Activation Dialog

Input

Node: Select nodes with constrained boundaries.

Time History Load Case: Select time history load case name with calculation results.

Node Reaction Table Result Schematic Node Reaction Table Result Schematic

(2) Deformation

Function: Output time history data of single node displacement/velocity/acceleration.
Command:

Results > Time History Tables > Deformation > Displacement

Results > Time History Tables > Deformation > Velocity

Results > Time History Tables > Deformation > Acceleration

Node Displacement Table Activation Dialog Node Displacement Table Activation Dialog

Input

Node: Select nodes to output displacement results.

Time History Load Case: Select time history load case name with calculation results.

Node Displacement Table Result Schematic Node Displacement Table Result Schematic

(3) Internal Forces

Function: Output time history data of single element internal forces.
Command:

Results > Time History Tables > Internal Forces > Truss Element Internal Forces

Results > Time History Tables > Internal Forces > Beam Element Internal Forces

Results > Time History Tables > Internal Forces > Plate Element Internal Forces

Results > Time History Tables > Internal Forces > Boundary Element Internal Forces

Element Internal Force Table Activation Dialog Element Internal Force Table Activation Dialog

Input

Element: Select elements to output internal force results.

Time History Load Case: Select time history load case name with calculation results.

Position Number: Select position to output element internal force.

Element Internal Force Table Result Schematic Element Internal Force Table Result Schematic

(4) Stresses

Function: Output time history data of single element stresses.
Command:

Results > Time History Tables > Stresses > Truss Element Stresses

Results > Time History Tables > Stresses > Beam Element Stresses

Results > Time History Tables > Stresses > Plate Element Stresses

Element Stress Table Activation Dialog Element Stress Table Activation Dialog

Input

Element: Select elements to output stress results.

Time History Load Case: Select time history load case name with calculation results.

Position Number: Select position to output element stress.

Element Stress Table Result Schematic Element Stress Table Result Schematic