3D beam truss subjected to a certain amount of force over its base. Using beam tools , the axial force , bending moments and shear force diagrams are drawn/calculated.
EITHER GEAR IS GIVEN A MOMENT OR RACK IS GIVEN A FORCE IN THE +Y DIRECTION
DEFORMATION AND VON MISES STRESS RESULTS ARE PLOTTED AND REACTIONS DUE TO THE APPLIED LOAD IS CALCULATED
Bolt and nut contact analsyis(axisymmetric)Vishnu R
Bolt and nut assembly, where the presence of contact between them make the physics to become nonlinear. Here 2D geometry is modeled and analyzed. Invoked various meshing methods to accurately capture the contact non linearity
Deformation, stress and strain were calculated
This is a course project report for an Eye End of Knuckle Joint using ANSYS. A step wise procedure of analysis is given in the report along with all the possible results. This report is a part of curriculum of the subject Finite Element Analysis (FEA) of BE Mechanical Engineering final year, University of Mumbai.
EITHER GEAR IS GIVEN A MOMENT OR RACK IS GIVEN A FORCE IN THE +Y DIRECTION
DEFORMATION AND VON MISES STRESS RESULTS ARE PLOTTED AND REACTIONS DUE TO THE APPLIED LOAD IS CALCULATED
Bolt and nut contact analsyis(axisymmetric)Vishnu R
Bolt and nut assembly, where the presence of contact between them make the physics to become nonlinear. Here 2D geometry is modeled and analyzed. Invoked various meshing methods to accurately capture the contact non linearity
Deformation, stress and strain were calculated
This is a course project report for an Eye End of Knuckle Joint using ANSYS. A step wise procedure of analysis is given in the report along with all the possible results. This report is a part of curriculum of the subject Finite Element Analysis (FEA) of BE Mechanical Engineering final year, University of Mumbai.
Analysis and Optimization Of Boring Process Parameters By Using Taguchi Metho...inventionjournals
International Journal of Engineering and Science Invention (IJESI) is an international journal intended for professionals and researchers in all fields of computer science and electronics. IJESI publishes research articles and reviews within the whole field Engineering Science and Technology, new teaching methods, assessment, validation and the impact of new technologies and it will continue to provide information on the latest trends and developments in this ever-expanding subject. The publications of papers are selected through double peer reviewed to ensure originality, relevance, and readability. The articles published in our journal can be accessed online.
The selection of optimal cutting parameters in turning operation is very important to
achieve high cutting performance. This paper deals with the optimization of performance
characteristics of turning EN-16 steel alloy using tungsten carbide inserts by Taguchi approach. The
experiments were performed on the basis of an L-18 orthogonal array given by Taguchi’s parameter
design approach. The performance characteristics such as thrust force and Material Removal Rate
(MRR) are optimized with the optimal combination of cutting parameters such as nose radius,
cutting speed, feed rate and depth of cut. Analysis of variance (ANOVA) is applied to identify the
most significant factor using MINITAB-16 software. The cutting parameters are varied to observe
the effects on performance characteristics and find the optimal results. Finally, confirmation tests are
performed to verify the experimental results. The results from the confirmation tests proved that the
performance characteristics such as thrust force and MRR are improved simultaneously through
optimal combination of process parameters obtained from Taguchi approach
Active Control of Tool Position in the Presence of Nonlinear Cutting Forces i...Waqas Tariq
This work presents a practical approach to the control of tool’s position, in orthogonal cutting, in the presence nonlinear dynamic cutting forces. The controller is Linear Quadratic Gaussian (LQG) type constructed from an augmented model of both, tool-actuator dynamics, and a nonlinear dynamic model relating tool displacement to cutting forces. The latter model is obtained using black-box system identification of experimental orthogonal cutting data in which tool displacement is the input and cutting force is the output. The controller is evaluated and its performance is demonstrated
Analysis and Optimization Of Boring Process Parameters By Using Taguchi Metho...inventionjournals
International Journal of Engineering and Science Invention (IJESI) is an international journal intended for professionals and researchers in all fields of computer science and electronics. IJESI publishes research articles and reviews within the whole field Engineering Science and Technology, new teaching methods, assessment, validation and the impact of new technologies and it will continue to provide information on the latest trends and developments in this ever-expanding subject. The publications of papers are selected through double peer reviewed to ensure originality, relevance, and readability. The articles published in our journal can be accessed online.
The selection of optimal cutting parameters in turning operation is very important to
achieve high cutting performance. This paper deals with the optimization of performance
characteristics of turning EN-16 steel alloy using tungsten carbide inserts by Taguchi approach. The
experiments were performed on the basis of an L-18 orthogonal array given by Taguchi’s parameter
design approach. The performance characteristics such as thrust force and Material Removal Rate
(MRR) are optimized with the optimal combination of cutting parameters such as nose radius,
cutting speed, feed rate and depth of cut. Analysis of variance (ANOVA) is applied to identify the
most significant factor using MINITAB-16 software. The cutting parameters are varied to observe
the effects on performance characteristics and find the optimal results. Finally, confirmation tests are
performed to verify the experimental results. The results from the confirmation tests proved that the
performance characteristics such as thrust force and MRR are improved simultaneously through
optimal combination of process parameters obtained from Taguchi approach
Active Control of Tool Position in the Presence of Nonlinear Cutting Forces i...Waqas Tariq
This work presents a practical approach to the control of tool’s position, in orthogonal cutting, in the presence nonlinear dynamic cutting forces. The controller is Linear Quadratic Gaussian (LQG) type constructed from an augmented model of both, tool-actuator dynamics, and a nonlinear dynamic model relating tool displacement to cutting forces. The latter model is obtained using black-box system identification of experimental orthogonal cutting data in which tool displacement is the input and cutting force is the output. The controller is evaluated and its performance is demonstrated
ANALYSIS AND MODELING OF SINGLE POINT CUTTING (HSS MATERIAL) TOOL WITH HELP O...IAEME Publication
The purpose of this article is to study the change of vibration on lathe machine by the change of tool material. Industrial vibration on analysis is a measurement tool used to identify, predict and prevent failure in any rotating machinery. By the vibration analysis on any mechanical component will improve the reliability of machine and lead to better machine efficiency and reduce down time for eliminating electrical and mechanical failure.
Stiffened Panels structures are widely used because they make the structure more cost-effective by offering a desirable strength/weight ratio, and is in so far that even small weight reduction of each of them can significantly affect the total empty weight of the structure. The reduction in the structural weight of ships gives valuable advantages such as; increasing their cargo-carrying efficiency, decrease in material cost supersedes the higher production costs, also lighter vessels requires engines with lower power, which means less emission of hazardous gases produced by marine diesel engines.
In this research a barge’s deck is evaluated by means of finite element analysis and optimized by parametric sensitivity analysis and numerical optimization methods, and the results would show that the deck structure could be developed further by utilizing the optimization techniques to reduce their weight by up to 9%.
The Effect of Process Parameters on Surface Roughness in Face Millinginventionjournals
International Journal of Engineering and Science Invention (IJESI) is an international journal intended for professionals and researchers in all fields of computer science and electronics. IJESI publishes research articles and reviews within the whole field Engineering Science and Technology, new teaching methods, assessment, validation and the impact of new technologies and it will continue to provide information on the latest trends and developments in this ever-expanding subject. The publications of papers are selected through double peer reviewed to ensure originality, relevance, and readability. The articles published in our journal can be accessed online.
The part is axisymmetrically modeled in solidworks(2D) before importing to ansys workbench where the boundary zones are identified and appropriate mesh settings is applied. The model is then imported in Fluent for analysis . Significant setting changes are Density based solver , Enhanced Eddy viscosity model with near wall treatment , solution steering , FMG initialization etc.
Horizontal axis wind turbine blade- 1way FSI analysisVishnu R
Combination of CFD and FEA analyses to assess the mechanical response of a wind turbine blade spinning clockwise as a consequence of wind blowing along the -z direction
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Buying new cosmetic products is difficult. It can even be scary for those who have sensitive skin and are prone to skin trouble. The information needed to alleviate this problem is on the back of each product, but it's thought to interpret those ingredient lists unless you have a background in chemistry.
Instead of buying and hoping for the best, we can use data science to help us predict which products may be good fits for us. It includes various function programs to do the above mentioned tasks.
Data file handling has been effectively used in the program.
The automated cosmetic shop management system should deal with the automation of general workflow and administration process of the shop. The main processes of the system focus on customer's request where the system is able to search the most appropriate products and deliver it to the customers. It should help the employees to quickly identify the list of cosmetic product that have reached the minimum quantity and also keep a track of expired date for each cosmetic product. It should help the employees to find the rack number in which the product is placed.It is also Faster and more efficient way.
Industrial Training at Shahjalal Fertilizer Company Limited (SFCL)MdTanvirMahtab2
This presentation is about the working procedure of Shahjalal Fertilizer Company Limited (SFCL). A Govt. owned Company of Bangladesh Chemical Industries Corporation under Ministry of Industries.
CFD Simulation of By-pass Flow in a HRSG module by R&R Consult.pptxR&R Consult
CFD analysis is incredibly effective at solving mysteries and improving the performance of complex systems!
Here's a great example: At a large natural gas-fired power plant, where they use waste heat to generate steam and energy, they were puzzled that their boiler wasn't producing as much steam as expected.
R&R and Tetra Engineering Group Inc. were asked to solve the issue with reduced steam production.
An inspection had shown that a significant amount of hot flue gas was bypassing the boiler tubes, where the heat was supposed to be transferred.
R&R Consult conducted a CFD analysis, which revealed that 6.3% of the flue gas was bypassing the boiler tubes without transferring heat. The analysis also showed that the flue gas was instead being directed along the sides of the boiler and between the modules that were supposed to capture the heat. This was the cause of the reduced performance.
Based on our results, Tetra Engineering installed covering plates to reduce the bypass flow. This improved the boiler's performance and increased electricity production.
It is always satisfying when we can help solve complex challenges like this. Do your systems also need a check-up or optimization? Give us a call!
Work done in cooperation with James Malloy and David Moelling from Tetra Engineering.
More examples of our work https://www.r-r-consult.dk/en/cases-en/
Saudi Arabia stands as a titan in the global energy landscape, renowned for its abundant oil and gas resources. It's the largest exporter of petroleum and holds some of the world's most significant reserves. Let's delve into the top 10 oil and gas projects shaping Saudi Arabia's energy future in 2024.
Water scarcity is the lack of fresh water resources to meet the standard water demand. There are two type of water scarcity. One is physical. The other is economic water scarcity.
Explore the innovative world of trenchless pipe repair with our comprehensive guide, "The Benefits and Techniques of Trenchless Pipe Repair." This document delves into the modern methods of repairing underground pipes without the need for extensive excavation, highlighting the numerous advantages and the latest techniques used in the industry.
Learn about the cost savings, reduced environmental impact, and minimal disruption associated with trenchless technology. Discover detailed explanations of popular techniques such as pipe bursting, cured-in-place pipe (CIPP) lining, and directional drilling. Understand how these methods can be applied to various types of infrastructure, from residential plumbing to large-scale municipal systems.
Ideal for homeowners, contractors, engineers, and anyone interested in modern plumbing solutions, this guide provides valuable insights into why trenchless pipe repair is becoming the preferred choice for pipe rehabilitation. Stay informed about the latest advancements and best practices in the field.
1. Project
First Saved Monday, October 17, 2016
Last Saved Monday, October 17, 2016
Product Version 16.0 Release
Save Project Before Solution No
Save Project After Solution No
2. Contents
Units
Model (A4)
o Geometry
Parts
o Construction Geometry
Path
o Coordinate Systems
o Connections
Contacts
Bonded - Line Body To Surface Body
o Mesh
o Named Selections
o Static Structural (A5)
Analysis Settings
Loads
Solution (A6)
Solution Information
Results
Beam Tool
Results
Results
Stress Tool
Safety Factor
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
C:UsersVishnu RajaranganAppDataLocalTempWB_VISHNU-PC_Vishnu
Rajarangan_10344_2unsaved_project_filesdp0SYSDMSYS.agdb
Type DesignModeler
3. Length Unit Meters
Element Control Program Controlled
Display Style Body Color
Bounding Box
Length X 8000. mm
Length Y 2000. mm
Length Z 2000. mm
Properties
Volume 1.7394e+009 mm³
Mass 13655 kg
Scale Factor
Value
1.
Statistics
Bodies 2
Active Bodies 2
Nodes 995
Elements 676
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:UsersVishnu RajaranganAppDataLocalTemp
Analysis Type 3-D
Decompose
Disjoint
Geometry
Yes
Enclosure and
Symmetry
Processing
Yes
4. TABLE 3
Model (A4) > Geometry > Parts
Object Name Line Body Surface Body
State Meshed
Graphics Properties
Visible Yes
Transparency 1
Definition
Suppressed No
Coordinate System Default Coordinate System
Reference Temperature By Environment
Offset Mode Refresh on Update
Offset Type Centroid Middle
Model Type Beam
Stiffness Behavior Flexible
Thickness 100. mm
Thickness Mode Refresh on Update
Material
Assignment Structural Steel
Nonlinear Effects Yes
Thermal Strain Effects Yes
Bounding Box
Length X 8000. mm
Length Y 2000. mm 0. mm
Length Z 2000. mm
Properties
Volume 1.3944e+008 mm³ 1.6e+009 mm³
Mass 1094.6 kg 12560 kg
Length 55777 mm
Cross Section Rect1
Cross Section Area 2500. mm²
Cross Section IYY 5.2083e+005 mm²·mm²
Cross Section IZZ 5.2083e+005 mm²·mm²
Centroid X 4000. mm
Centroid Y 0. mm
Centroid Z 1000. mm
Moment of Inertia Ip1 4.1867e+009 kg·mm²
Moment of Inertia Ip2 7.1173e+010 kg·mm²
Moment of Inertia Ip3 6.6987e+010 kg·mm²
Surface Area(approx.) 1.6e+007 mm²
Statistics
Nodes 544 451
Elements 276 400
Mesh Metric None
TABLE 4
Model (A4) > Construction Geometry
Object Name Construction Geometry
State Fully Defined
5. Display
Show Mesh No
TABLE 5
Model (A4) > Construction Geometry > Paths
Object Name Path
State Fully Defined
Definition
Path Type Edge
Suppressed No
Scope
Geometry 3 Edges
Coordinate Systems
TABLE 6
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. ]
Connections
TABLE 7
Model (A4) > Connections
Object Name Connections
State Fully Defined
Auto Detection
Generate Automatic Connection On Refresh Yes
Transparency
Enabled Yes
TABLE 8
Model (A4) > Connections > Contacts
Object Name Contacts
State Fully Defined
Definition
Connection Type Contact
6. Scope
Scoping Method Geometry Selection
Geometry All Bodies
Auto Detection
Tolerance Type Slider
Tolerance Slider 0.
Tolerance Value 21.213 mm
Use Range No
Face/Face No
Face/Edge No
Edge/Edge No
Priority Include All
Group By Bodies
Search Across Bodies
Statistics
Connections 1
Active Connections 1
TABLE 9
Model (A4) > Connections > Contacts > Contact Regions
Object Name Bonded - Line Body To Surface Body
State Fully Defined
Scope
Scoping Method Geometry Selection
Contact 10 Vertices
Target 2 Edges
Contact Bodies Line Body
Target Bodies Surface Body
Shell Thickness Effect No
Definition
Type Bonded
Scope Mode Manual
Trim Contact Program Controlled
Suppressed No
Advanced
Formulation Program Controlled
Penetration Tolerance Program Controlled
Elastic Slip Tolerance Program Controlled
Normal Stiffness Program Controlled
Update Stiffness Program Controlled
Pinball Region Program Controlled
Mesh
TABLE 10
Model (A4) > Mesh
Object Name Mesh
State Solved
7. Display
Display Style Body Color
Defaults
Physics Preference Mechanical
Relevance 0
Sizing
Use Advanced Size Function On: Curvature
Use Fixed Size Function For Sheets No
Relevance Center Coarse
Initial Size Seed Active Assembly
Smoothing Medium
Span Angle Center Coarse
Curvature Normal Angle Default (30.0 °)
Min Size Default (100.0 mm)
Max Face Size 200.0 mm
Growth Rate Default
Minimum Edge Length 2000.0 mm
Inflation
Use Automatic Inflation None
Inflation Option Smooth Transition
Transition Ratio 0.272
Maximum Layers 2
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
Use Sheet Thickness for Pinch No
Pinch Tolerance Default (90.0 mm)
Generate Pinch on Refresh No
Sheet Loop Removal No
Automatic Mesh Based Defeaturing On
Defeaturing Tolerance Default (75.0 mm)
Statistics
Nodes 995
Elements 676
8. Mesh Metric None
Named Selections
Static Structural (A5)
TABLE 11
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 12
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
9. Contact Miscellaneous No
General Miscellaneous No
Store Results At All Time Points
Analysis Data Management
Solver Files Directory D:New folderBeam Analysis_filesdp0SYSMECH
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 13
Model (A4) > Static Structural (A5) > Loads
Object Name Fixed Support Displacement Pressure
State Fully Defined
Scope
Scoping Method Geometry Selection
Geometry 1 Edge 1 Face
Definition
Type Fixed Support Displacement Pressure
Suppressed No
Define By Components Normal To
Coordinate System Global Coordinate System
X Component Free
Y Component 0. mm (ramped)
Z Component Free
Magnitude 0.2 MPa (ramped)
FIGURE 1
Model (A4) > Static Structural (A5) > Displacement
11. Solution (A6)
TABLE 14
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 15
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 16
Model (A4) > Static Structural (A5) > Solution (A6) > Results
Object Name Equivalent Stress Total Deformation
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Position Top/Bottom
Definition
Type Equivalent (von-Mises) Stress Total Deformation
By Time
Display Time Last
Calculate Time History Yes
Identifier
Suppressed No
Integration Point Results
Display Option Averaged
12. Average Across Bodies No
Results
Minimum 9.1792 MPa 0. mm
Maximum 123.12 MPa 16.238 mm
Minimum Occurs On Surface Body
Maximum Occurs On Surface Body
Information
Time 1. s
Load Step 1
Substep 1
Iteration Number 1
FIGURE 3
Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress
TABLE 17
Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress
Time [s] Minimum [MPa] Maximum [MPa]
1. 9.1792 123.12
FIGURE 4
Model (A4) > Static Structural (A5) > Solution (A6) > Equivalent Stress > Figure
13. FIGURE 5
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation
14. TABLE 18
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation
Time [s] Minimum [mm] Maximum [mm]
1. 0. 16.238
FIGURE 6
Model (A4) > Static Structural (A5) > Solution (A6) > Total Deformation > Figure
15. TABLE 19
Model (A4) > Static Structural (A5) > Solution (A6) > Beam Tool
Object Name Beam Tool
State Solved
Scope
Geometry All Line Bodies
TABLE 20
Model (A4) > Static Structural (A5) > Solution (A6) > Beam Tool > Results
Object Name Direct Stress Minimum Combined Stress Maximum Combined Stress
State Solved
Definition
Type Direct Stress Minimum Combined Stress Maximum Combined Stress
By Time
Display Time Last
Calculate Time History Yes
Identifier
Suppressed No
Integration Point Results
16. Display Option Averaged
Results
Minimum -299.19 MPa -312.91 MPa -295.69 MPa
Maximum 258.06 MPa 256.27 MPa 286.39 MPa
Information
Time 1. s
Load Step 1
Substep 1
Iteration Number 1
FIGURE 7
Model (A4) > Static Structural (A5) > Solution (A6) > Beam Tool > Direct Stress
TABLE 21
Model (A4) > Static Structural (A5) > Solution (A6) > Beam Tool > Direct Stress
Time [s] Minimum [MPa] Maximum [MPa]
1. -299.19 258.06
FIGURE 8
Model (A4) > Static Structural (A5) > Solution (A6) > Beam Tool > Direct Stress > Figure
19. FIGURE 11
Model (A4) > Static Structural (A5) > Solution (A6) > Beam Tool > Maximum Combined Stress
20. TABLE 23
Model (A4) > Static Structural (A5) > Solution (A6) > Beam Tool > Maximum Combined Stress
Time [s] Minimum [MPa] Maximum [MPa]
1. -295.69 286.39
FIGURE 12
Model (A4) > Static Structural (A5) > Solution (A6) > Beam Tool > Maximum Combined Stress >
Figure
21. TABLE 24
Model (A4) > Static Structural (A5) > Solution (A6) > Results
Object Name Axial Force
Total Bending
Moment
Total Shear-
Moment Diagram
Total Shear-
Moment
Diagram 2
Total Shear-
Moment Diagram
3
State Solved
Scope
Scoping
Method
Geometry Selection Path
Geometry All Line Bodies
Path Path
Definition
Type
Directional Axial
Force
Total Bending
Moment
Total Shear-Moment Diagram
By Time
Display Time Last
Coordinate
System
Solution
Coordinate
System
22. Calculate
Time History
Yes
Identifier
Suppressed No
Graphics
Display
Total Bending
Moment
Total Shear
Force
Total
Displacement
Integration Point Results
Display Option Unaveraged
Results
Minimum -7.4797e+005 N 23353 N·mm 91.831 N 4.6396 mm
Maximum 6.4516e+005 N
1.136e+006
N·mm
5.5668e+005
N·mm
524.02 N 12.494 mm
Information
Time 1. s
Load Step 1
Substep 1
Iteration
Number
1
Graph Controls
X-Axis S
FIGURE 13
Model (A4) > Static Structural (A5) > Solution (A6) > Axial Force
TABLE 25
Model (A4) > Static Structural (A5) > Solution (A6) > Axial Force
Time [s] Minimum [N] Maximum [N]
23. 1. -7.4797e+005 6.4516e+005
FIGURE 14
Model (A4) > Static Structural (A5) > Solution (A6) > Axial Force > Figure
FIGURE 15
Model (A4) > Static Structural (A5) > Solution (A6) > Total Bending Moment
24. TABLE 26
Model (A4) > Static Structural (A5) > Solution (A6) > Total Bending Moment
Time [s] Minimum [N·mm] Maximum [N·mm]
1. 23353 1.136e+006
FIGURE 16
Model (A4) > Static Structural (A5) > Solution (A6) > Total Bending Moment > Figure
25. FIGURE 17
Model (A4) > Static Structural (A5) > Solution (A6) > Total Shear-Moment Diagram
26. TABLE 27
Model (A4) > Static Structural (A5) > Solution (A6) > Total Shear-Moment Diagram
Length [mm] Total Shear Force [N] Total Bending Moment [N·mm] Total Displacement [mm]
0.
396.02
3.1402e+005 4.6396
200. 2.351e+005 5.2926
400. 1.5647e+005 6.033
600. 79001 6.8306
800. 23353 7.6553
1000. 86001 8.4772
1200. 1.6369e+005 9.2664
1400. 2.4236e+005 9.9928
1600. 3.2129e+005 10.626
1800. 4.0033e+005 11.137
2000.
4.7943e+005
11.495
91.831
60647
2200. 75687 11.754
34. TABLE 30
Model (A4) > Static Structural (A5) > Solution (A6) > Stress Safety Tools
Object Name Stress Tool
State Solved
Definition
Theory Max Equivalent Stress
Stress Limit Type Tensile Yield Per Material
TABLE 31
Model (A4) > Static Structural (A5) > Solution (A6) > Stress Tool > Results
Object Name Safety Factor
State Solved
Scope
Scoping Method Geometry Selection
Geometry All Bodies
Definition
Type Safety Factor
By Time
Display Time Last
Calculate Time History Yes
Identifier
Suppressed No
Integration Point Results
Display Option Averaged
Average Across Bodies No
Results
Minimum 2.0306
Minimum Occurs On Surface Body
Information
35. Time 1. s
Load Step 1
Substep 1
Iteration Number 1
FIGURE 23
Model (A4) > Static Structural (A5) > Solution (A6) > Stress Tool > Safety Factor
TABLE 32
Model (A4) > Static Structural (A5) > Solution (A6) > Stress Tool > Safety Factor
Time [s] Minimum Maximum
1. 2.0306 15.
Material Data
Structural Steel
TABLE 33
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