Concrete beam with impactor on top

Project

First Saved Thursday, October 20, 2016

Last Saved Thursday, October 20, 2016

Product Version 16.0 Release

Save Project Before Solution No

Save Project After Solution No

Contents

Units

Model (A4) o Geometry

Parts REBAR

Parts o Coordinate Systems o Symmetry

Symmetry Region o Connections

Contacts No Separation - CONCRETE To IMPACTER

o Mesh o Named Selections o Static Structural (A5)

Analysis Settings Loads Solution (A6)

Solution Information Results

Material Data o Structural Steel

Units

TABLE 1

Unit System Metric (mm, kg, N, s, mV, mA) Degrees RPM Celsius

Angle Degrees

Rotational Velocity RPM

Temperature Celsius

Model (A4)

Geometry

TABLE 2 Model (A4) > Geometry

Object Name Geometry

State Fully Defined

Definition

Source D:\New folder\RC BEAM STATIC STRUCTURAL

ANALYSIS_files\dp0\SYS\DM\SYS.agdb

Type DesignModeler

Length Unit Meters

Element Control Program Controlled

Display Style Body Color

Bounding Box

Length X 2750. mm

Length Y 420. mm

Length Z 250. mm

Properties

Volume 2.7674e+008 mm³

Mass 2172.4 kg

Scale Factor Value 1.

Statistics

Bodies 6

Active Bodies 6

Nodes 11754

Elements 2430

Mesh Metric None

Basic Geometry Options

Parameters Yes

Parameter Key DS

Attributes No

Named Selections No

Material Properties No

Advanced Geometry Options

Use Associativity Yes

Coordinate Systems No

Reader Mode Saves Updated File

No

Use Instances Yes

Smart CAD Update No

Compare Parts On Update No

Attach File Via Temp File Yes

Temporary Directory C:\Users\Vishnu Rajarangan\AppData\Local\Temp

Analysis Type 3-D

Decompose Disjoint Geometry

Yes

Enclosure and Symmetry Processing

Yes

TABLE 3 Model (A4) > Geometry > Parts

Object Name CONCRETE IMPACTER

State Meshed

Graphics Properties

Visible Yes

Transparency 1

Definition

Suppressed No

Stiffness Behavior Flexible

Coordinate System Default Coordinate System

Reference Temperature By Environment

Material

Assignment Structural Steel

Nonlinear Effects Yes

Thermal Strain Effects Yes

Bounding Box

Length X 2750. mm 100. mm

Length Y 400. mm 20. mm

Length Z 250. mm

Properties

Volume 2.75e+008 mm³ 5.e+005 mm³

Mass 2158.7 kg 3.925 kg

Centroid X 1375. mm 1849.9 mm

Centroid Y 200. mm 410. mm

Centroid Z 125. mm

Moment of Inertia Ip1 4.0027e+007 kg·mm² 20574 kg·mm²

Moment of Inertia Ip2 1.3717e+009 kg·mm² 23714 kg·mm²

Moment of Inertia Ip3 1.3892e+009 kg·mm² 3401.7 kg·mm²

Statistics

Nodes 11202 108

Elements 2200 10

Mesh Metric None

TABLE 4 Model (A4) > Geometry > CONCRETE > Command Snippet

Object Name Commands (APDL)

State Fully Defined

File

File Name

File Status File not found

Definition

Suppressed No

Target Mechanical APDL

Input Arguments

ARG1

ARG2

ARG3

ARG4

ARG5

ARG6

ARG7

ARG8

ARG9

Model (A4) > Geometry > CONCRETE > Commands (APDL)

! Commands inserted into this file will be executed just after material

definitions in /PREP7.

! The material number for this body is equal to the parameter "matid".

! Active UNIT system in Workbench when this object was created: Metric

(mm, kg, N, s, mV, mA)

! NOTE: Any data that requires units (such as mass) is assumed to be in

the consistent solver unit system.

! See Solving Units in the help system for more information.

ET,MATID,SOLID65

R,MATID,0,0,0,0,0,0

RMORE,0,0,0,0,0

MP,EX,MATID,29250

MP,PRXY,MATID,0.2

MPTEMP,MATID,0

TB,CONCR,MATID,1,9

TBTEMP,22

TBDATA,1,0.3,0.8,1.5,25

TB,MISO,MATID,1,35,0

TBTEMP,22

TBPT,,0.0001,2.925

TBPT,,0.0002,5.7

TBPT,,0.0003,8.325

TBPT,,0.0004,10.8

TBPT,,0.0005,13.125

TBPT,,0.0006,15.3

TBPT,,0.0007,17.325

TBPT,,0.0008,19.2

TBPT,,0.0009,20.925

TBPT,,0.001,22.5

TBPT,,0.0011,23.925

TBPT,,0.0012,25.2

TBPT,,0.0013,26.325

TBPT,,0.0014,27.3

TBPT,,0.0015,28.125

TBPT,,0.0016,28.8

TBPT,,0.0017,29.325

TBPT,,0.0018,29.7

TBPT,,0.0019,29.925

TBPT,,0.002,30

TBPT,,0.0021,30

TBPT,,0.0022,30

TBPT,,0.0023,30

TBPT,,0.0024,30

TBPT,,0.0025,30

TBPT,,0.0026,30

TBPT,,0.0027,30

TBPT,,0.0028,30

TBPT,,0.0029,30

TBPT,,0.003,30

TBPT,,0.0031,30

TBPT,,0.0032,30

TBPT,,0.0033,30

TBPT,,0.0034,30

TBPT,,0.0035,30

TABLE 5 Model (A4) > Geometry > Body Groups

Object Name REBAR

State Meshed

Graphics Properties

Visible Yes

Definition

Suppressed No



Bounding Box

Length X 2750. mm

Length Y 0. mm

Length Z 150. mm

Properties


Mass 9.7655 kg

Statistics

Nodes 444

Elements 220

Mesh Metric None

TABLE 6 Model (A4) > Geometry > REBAR > Parts

Object Name Line Body Line Body Line Body Line Body

State Meshed

Graphics Properties

Visible Yes

Transparency 1

Definition

Suppressed No


Reference Temperature By Environment

Offset Mode Refresh on Update

Offset Type Centroid

Model Type Beam

Material


Nonlinear Effects Yes

Thermal Strain Effects Yes

Bounding Box

Length X 2750. mm

Length Y 0. mm

Length Z 0. mm

Properties


Mass 2.4414 kg

Length 2750. mm

Cross Section Circular1

Cross Section Area 113.09 mm²

Cross Section IYY 1017.7 mm²·mm²

Cross Section IZZ 1017.7 mm²·mm²

Statistics

Nodes 111

Elements 55

Mesh Metric None

TABLE 7 Model (A4) > Geometry > REBAR > Line Body > Command Snippet


State Fully Defined

File

File Name


Definition

Suppressed No


Input Arguments

ARG1

ARG2

ARG3

ARG4

ARG5

ARG6

ARG7

ARG8

ARG9

Model (A4) > Geometry > REBAR > Line Body > Commands (APDL)









ET,MATID,LINK180

MPDATA,EX,MATID,,2e5

MPDATA,PRXY,MATID,,0.3

TB,BISO,MATID,1,2

TBDATA,,460,2100

R,MATID,12,,0



State Fully Defined

File

File Name


Definition

Suppressed No


Input Arguments

ARG1

ARG2

ARG3

ARG4

ARG5

ARG6

ARG7

ARG8

ARG9










ET,MATID,LINK180



TB,BISO,MATID,1,2

TBDATA,,460,2100

R,MATID,12,,0



State Fully Defined

File

File Name


Definition

Suppressed No


Input Arguments

ARG1

ARG2

ARG3

ARG4

ARG5

ARG6

ARG7

ARG8

ARG9










ET,MATID,LINK180



TB,BISO,MATID,1,2

TBDATA,,460,2100

R,MATID,12,,0



State Fully Defined

File

File Name


Definition

Suppressed No


Input Arguments

ARG1

ARG2

ARG3

ARG4

ARG5

ARG6

ARG7

ARG8

ARG9










ET,MATID,LINK180



TB,BISO,MATID,1,2

TBDATA,,460,2100

R,MATID,12,,0

Coordinate Systems

TABLE 11 Model (A4) > Coordinate Systems > Coordinate System

Object Name Global Coordinate System

State Fully Defined

Definition

Type Cartesian

Coordinate System ID 0.

Origin

Origin X 0. mm

Origin Y 0. mm

Origin Z 0. mm

Directional Vectors

X Axis Data [ 1. 0. 0. ]

Y Axis Data [ 0. 1. 0. ]

Z Axis Data [ 0. 0. 1. ]

Symmetry

TABLE 12 Model (A4) > Symmetry

Object Name Symmetry

State Fully Defined

TABLE 13 Model (A4) > Symmetry > Symmetry Region

Object Name Symmetry Region

State Fully Defined

Scope

Scoping Method Geometry Selection

Geometry 1 Face

Definition

Scope Mode Manual

Type Symmetric

Coordinate System Global Coordinate System

Symmetry Normal X Axis

Suppressed No

Connections

TABLE 14 Model (A4) > Connections

Object Name Connections

State Fully Defined

Auto Detection

Generate Automatic Connection On Refresh Yes

Transparency

Enabled Yes

TABLE 15 Model (A4) > Connections > Contacts

Object Name Contacts

State Fully Defined

Definition

Connection Type Contact

Scope


Geometry All Bodies

Auto Detection

Tolerance Type Slider

Tolerance Slider 0.

Tolerance Value 6.9827 mm

Use Range No

Face/Face Yes

Face/Edge No

Edge/Edge No

Priority Include All

Group By Bodies

Search Across Bodies

Statistics

Connections 1

Active Connections 1

TABLE 16 Model (A4) > Connections > Contacts > Contact Regions

Object Name No Separation - CONCRETE To IMPACTER

State Fully Defined

Scope


Contact 1 Face

Target 1 Face

Contact Bodies CONCRETE

Target Bodies IMPACTER

Definition

Type No Separation

Scope Mode Automatic

Behavior Program Controlled

Trim Contact Program Controlled

Trim Tolerance 6.9827 mm

Suppressed No

Advanced

Formulation MPC

Detection Method Program Controlled

Pinball Region Program Controlled

Geometric Modification

Contact Geometry Correction None

Target Geometry Correction None

Mesh

TABLE 17 Model (A4) > Mesh

Object Name Mesh

State Solved

Display

Display Style Body Color

Defaults

Physics Preference Mechanical

Relevance 0

Sizing

Use Advanced Size Function Off

Relevance Center Coarse

Element Size 50.0 mm

Initial Size Seed Active Assembly

Smoothing Medium

Transition Fast

Span Angle Center Coarse

Minimum Edge Length 20.0 mm

Inflation

Use Automatic Inflation None

Inflation Option Smooth Transition

Transition Ratio 0.272

Maximum Layers 5

Growth Rate 1.2

Inflation Algorithm Pre

View Advanced Options No

Patch Conforming Options

Triangle Surface Mesher Program Controlled

Patch Independent Options

Topology Checking No

Advanced

Number of CPUs for Parallel Part Meshing Program Controlled

Shape Checking Standard Mechanical

Element Midside Nodes Program Controlled

Straight Sided Elements No

Number of Retries Default (4)

Extra Retries For Assembly Yes

Rigid Body Behavior Dimensionally Reduced

Mesh Morphing Disabled

Defeaturing

Pinch Tolerance Please Define

Generate Pinch on Refresh No

Automatic Mesh Based Defeaturing On

Defeaturing Tolerance Default

Statistics

Nodes 11754

Elements 2430

Mesh Metric None

FIGURE 1 Model (A4) > Mesh > Figure

FIGURE 2 Model (A4) > Mesh > Figure 2

Named Selections

TABLE 18 Model (A4) > Named Selections > Named Selections

Object Name Supports

State Fully Defined

Scope


Geometry 6 Nodes

Definition

Send to Solver Yes

Visible Yes

Program Controlled Inflation Exclude

Statistics

Type Manual

Total Selection 6 Nodes

Suppressed 0

Used by Mesh Worksheet No

Static Structural (A5)

TABLE 19 Model (A4) > Analysis

Object Name Static Structural (A5)

State Solved

Definition

Physics Type Structural

Analysis Type Static Structural

Solver Target Mechanical APDL

Options

Environment Temperature 22. °C

Generate Input Only No

TABLE 20 Model (A4) > Static Structural (A5) > Analysis Settings

Object Name Analysis Settings

State Fully Defined

Step Controls

Number Of Steps 1.

Current Step Number 1.

Step End Time 1. s

Auto Time Stepping Program Controlled

Solver Controls

Solver Type Program Controlled

Weak Springs Program Controlled

Solver Pivot Checking Program Controlled

Large Deflection Off

Inertia Relief Off

Restart Controls

Generate Restart Points Program Controlled

Retain Files After Full Solve

No

Nonlinear Controls

Newton-Raphson Option Program Controlled

Force Convergence Program Controlled

Moment Convergence Program Controlled

Displacement Convergence

Program Controlled

Rotation Convergence Program Controlled

Line Search Program Controlled

Stabilization Off

Output Controls

Stress Yes

Strain Yes

Nodal Forces No

Contact Miscellaneous No

General Miscellaneous No

Store Results At All Time Points

Analysis Data Management

Solver Files Directory D:\New folder\RC BEAM STATIC STRUCTURAL

ANALYSIS_files\dp0\SYS\MECH\

Future Analysis None

Scratch Solver Files Directory

Save MAPDL db No

Delete Unneeded Files Yes

Nonlinear Solution No

Solver Units Active System

Solver Unit System nmm

TABLE 21 Model (A4) > Static Structural (A5) > Loads

Object Name Pressure Nodal Displacement

State Fully Defined

Scope

Scoping Method Geometry Selection Named Selection

Geometry 1 Face

Named Selection Supports

Definition

Type Pressure Displacement

Define By Normal To

Magnitude 9. MPa (ramped)

Suppressed No

Coordinate System Nodal Coordinate System

X Component Free

Y Component 0. mm (ramped)

Z Component 0. mm (ramped)

FIGURE 3 Model (A4) > Static Structural (A5) > Pressure

FIGURE 4 Model (A4) > Static Structural (A5) > Nodal Displacement

TABLE 22 Model (A4) > Static Structural (A5) > Command Snippet


State Fully Defined

File

File Name


Definition

Suppressed No


Input Arguments

ARG1

ARG2

ARG3

ARG4

ARG5

ARG6

ARG7

ARG8

ARG9

Model (A4) > Static Structural (A5) > Commands (APDL)

! Commands inserted into this file will be executed just prior to the ANSYS

SOLVE command.

! These commands may supersede command settings set by Workbench.






/PREP7

ESEL,S,ENAME,,65

ESEL,A,ENAME,,180

ALLSEL,BELOW,ELEM

CEINTF,0.001,

ALLSEL,ALL

/SOLU

OUTRES,ALL,ALL

Solution (A6)

TABLE 23 Model (A4) > Static Structural (A5) > Solution

Object Name Solution (A6)

State Solved

Adaptive Mesh Refinement

Max Refinement Loops 1.

Refinement Depth 2.

Information

Status Done

Post Processing

Calculate Beam Section Results No

TABLE 24 Model (A4) > Static Structural (A5) > Solution (A6) > Solution Information

Object Name Solution Information

State Solved

Solution Information

Solution Output Solver Output

Newton-Raphson Residuals 0

Update Interval 2.5 s

Display Points All

FE Connection Visibility

Activate Visibility Yes

Display All FE Connectors

Draw Connections Attached To All Nodes

Line Color Connection Type

Visible on Results No

Line Thickness Single

Display Type Lines

TABLE 25 Model (A4) > Static Structural (A5) > Solution (A6) > Results

Object Name Equivalent Stress Maximum Principal Stress

State Solved

Scope


Geometry 1 Body All Bodies

Definition

Type Equivalent (von-Mises) Stress Maximum Principal Stress

By Time

Display Time Last

Calculate Time History Yes

Identifier

Suppressed No

Integration Point Results

Display Option Averaged

Average Across Bodies No

Results

Minimum 5.1037e-020 MPa -33.625 MPa

Maximum 29.773 MPa 154.06 MPa

Minimum Occurs On IMPACTER

Maximum Occurs On IMPACTER

Information

Time 1. s

Load Step 1

Substep 1

Iteration Number 1

FIGURE 5 Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress

TABLE 26 Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress

Time [s] Minimum [MPa] Maximum [MPa]

1. 5.1037e-020 29.773

FIGURE 6 Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress > Figure

FIGURE 7 Model (A4) > Static Structural (A5) > Solution (A6) > Maximum Principal Stress

TABLE 27 Model (A4) > Static Structural (A5) > Solution (A6) > Maximum Principal Stress

Time [s] Minimum [MPa] Maximum [MPa]

1. -33.625 154.06

TABLE 28 Model (A4) > Static Structural (A5) > Solution (A6) > Command Snippet


State Solved

File

File Name


Definition

Suppressed No

Output Search Prefix my_

Invalidate Solution No


Input Arguments

ARG1

ARG2

ARG3

ARG4

ARG5

ARG6

ARG7

ARG8

ARG9

Results

Model (A4) > Static Structural (A5) > Solution (A6) > Commands (APDL)

! Commands inserted into this file will be executed immediately after the

ANSYS /POST1 command.






/SHOW,png

/ANG,1,

/VIEW,1,0,0,0 !Use these values to change the view

/DEVICE,VECTOR,ON

SET,Last !Outputs final result set

PLCRACK

FIGURE 8 Model (A4) > Static Structural (A5) > Solution (A6) > Commands (APDL) > Post Output

Material Data

Structural Steel

TABLE 29 Structural Steel > Constants

Density 7.85e-006 kg mm^-3

Coefficient of Thermal Expansion 1.2e-005 C^-1

Specific Heat 4.34e+005 mJ kg^-1 C^-1

Thermal Conductivity 6.05e-002 W mm^-1 C^-1

Resistivity 1.7e-004 ohm mm

TABLE 30 Structural Steel > Compressive Ultimate Strength

Compressive Ultimate Strength MPa

0

TABLE 31 Structural Steel > Compressive Yield Strength

Compressive Yield Strength MPa

250

TABLE 32 Structural Steel > Tensile Yield Strength

Tensile Yield Strength MPa

250

TABLE 33 Structural Steel > Tensile Ultimate Strength

Tensile Ultimate Strength MPa

460

TABLE 34 Structural Steel > Isotropic Secant Coefficient of Thermal Expansion

Reference Temperature C

22

TABLE 35 Structural Steel > Alternating Stress Mean Stress

Alternating Stress MPa Cycles Mean Stress MPa

3999 10 0

2827 20 0

1896 50 0

1413 100 0

1069 200 0

441 2000 0

262 10000 0

214 20000 0

138 1.e+005 0

114 2.e+005 0

86.2 1.e+006 0

TABLE 36 Structural Steel > Strain-Life Parameters

Strength Coefficient MPa

Strength Exponent

Ductility Coefficient

Ductility Exponent

Cyclic Strength Coefficient MPa

Cyclic Strain Hardening Exponent

920 -0.106 0.213 -0.47 1000 0.2

TABLE 37 Structural Steel > Isotropic Elasticity

Temperature C Young's Modulus MPa Poisson's Ratio Bulk Modulus MPa Shear Modulus MPa

2.e+005 0.3 1.6667e+005 76923

TABLE 38 Structural Steel > Isotropic Relative Permeability

Relative Permeability

10000

Concrete beam with impactor on top

Engineering

Transcript of Concrete beam with impactor on top