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How to do a Basic Linear Finite Element Analysis in CATIA V5
Pedro Campos
in
Simulation & CAE
1
2
Intermediate
After this tutorial, hopefully you will be able to do a simple linear analysis using FEM (Finite Element Method). The steps are straight forward and the part used is available in my profile (foot peg - ATV). The idea behind this is seeing how it reacts to a Pressure of 125 KPa. All the units in this tutorials are in the IS (International System) but i will put the conversions Metric-Imperial. IF YOU HAVE ANY DOUBTS SUCH AS WHERE ARE THE COMMANDS LOCATED DON'T HESITATE TO CONTACT ME. Pedro José Silva Campos
mises
von
atv
element
finite
catia
catiav5
mesh
fem
HOW TO ANIMATE IN SOLID EDGE
Shafe Mohammad
in
Simulation & CAE
0
1
Beginner
In this tutorial I will show you how to give motors (rotary) to your mechanism Example of A Robotic Arm is taken
edge
animation
arm
motions
simulation
robot
solid
How to simulate a mechanism in ADAMS
VAHID ZADE AHMADI
in
Simulation & CAE
0
1
Intermediate
In this tutorial I show you how to make a mechanism & give the initial conditions & simulate it in ADAMS & how to get desired diagrams .
adams
Tutorial 86: Full ANSYS ACP tutorial
Armin Yousefi Kanani
in
FEM
6
1
Intermediate
Composite materials are created by combining two or more layered materials, each with different properties. These materials have become a standard for products that are both light and strong. Composites provide enough flexibility so products with complex shapes, such as boat hulls and surfboards, can be easily manufactured. Engineering layered composites involves complex definitions that include numerous layers, materials, thicknesses and orientations. The engineering challenge is to predict how well the finished product will perform under real-world working conditions. This involves considering stresses and deformations as well as a range of failure criteria. ANSYS Composite PrepPost provides all necessary functionalities for the analysis of layered composite structures.
analysis
fea
acp
material
composite
ansys
How To Do FEA of Welded Component In CATIA V5?
'Bhavesh Shiyani
in
FEM
0
0
Intermediate
Check Below Link ! https://www.youtube.com/watch?v=gyE4q5IcJfs
structural
cae
welding
analysis
gas
catia
gps
Tutorial 85: Determining the Fatigue Behavior of Composite Tensile Specimen
Armin Yousefi Kanani
in
FEM
3
0
Expert
Random vibration analysis is another spectral method. The purpose of a random vibration analysis is to determine some statistical properties of a structural response, normally the standard deviation (1σ) of a displacement, force, or stress. (1σ) Is used to determine fatigue life of structure. In this tutorial, first we will model tensile specimen in ACP tools. Then we need to find 10 modes of specimen between 0 Hz to 1500 Hz frequencies. After that we need to calculate Sigma RMS, N, occurrence and V0 to calculate life time of specimen. Agenda: Creating Composite Tensile specimen in ACP Importing ACP model into modal analysis Finding Mode Shapes Introduction of random vibration Applying boundary conditions Determining the fatigue behavior of composite tensile specimen
specimen
tensile
composite
behavior
fatigue
determining
Tutorial 84:Tensile Test
Armin Yousefi Kanani
in
FEM
3
0
Expert
Tensile testing, is also known as tension testing is a fundamental materials science test in which a sample is subjected to a controlled tension until failure. The results from the test are commonly used to select a material for an application, for quality control, and to predict how a material will react under other types of forces. In this tutorial, first we are going to model specimen geometry in CAD software then we will apply composite layers in ACP tools. In the next step, we are going to model two metal parts and then at the end we will combine models into static structural. Meshes can be imported into Mechanical from multiple systems. It is possible to combine composite shell, composite solid, and non-layered shell and solid meshes to perform mixed analysis. Agenda: Modeling solid composite specimen Add metal parts Transfer parts to ANSYS Mechanical Apply boundary conditions, loads and solve the model Evaluate solid model results in ANSYS Composite PrepPost
Tutorial 83: Creating Sandwich Composite Plate with Honeycomb Core
Armin Yousefi Kanani
in
FEM
3
0
Expert
Honeycomb structures are natural or man-made structures that have the geometry of a honeycomb to allow the minimization of the amount of used material to reach minimal weight and minimal material cost. The geometry of honeycomb structures can vary widely but the common feature of all such structures is an array of hollow cells formed between thin vertical walls. In this tutorial we are going to create sandwich composite plate. First, we will create two composite plates in two different ACP and then we will create honeycomb in mechanical model by using Honeycombcreator extension. Then, we will combine three models into static structural to do stress analysis. At the end we will do eigenvalue simulation. Agenda: Using two ACP to create two composite plates Creating Honeycomb by using honeycomb creator Apply boundary conditions, loads and solve the model
core
honeycomb
with
plate
composite
sandwich
creating
Tutorial 82: Natural Frequencies and Mode Shape of Composite Plate with Hole
Armin Yousefi Kanani
in
FEM
1
0
Intermediate
The modal analysis technique is used to determine the vibration characteristics (I,e, Natural frequencies and mode shapes) of linear elastic structures. Our goal is to determine the first 10 natural frequencies and mode shapes for the plate with the hole shown. In this tutorial, first we are going to model simple plate with hole in ACP tools then we are importing model into modal. In the next step, we will have short introduction to modal tools in ANSYS software and do simulation to find natural frequencies and mode shape of composite model. Agenda: Creating Plate with Hole in ACP Importing ACP model into modal analysis Applying boundary conditions Finding mode shapes
hole
with
plate
composite
shape
mode
frequencies
natural
Tutorial 81: Reinforced Beam with Combination of Steel and Composite Material
Armin Yousefi Kanani
in
FEM
4
0
Expert
Reinforced Concrete is a common building material for construction of facilities and structures. While concrete has high compressive strength, it has limited tensile strength. To overcome these tensile limitations, reinforcing bars are used in the tension side of concrete structures. In this tutorial, first we are going to model concreate geometry in mechanical model then we need to model 4 structural steel rebar in another mechanical model. at the end we are going to reinforced structural steel rebar by using 4 composite layers Agenda: Creating all models in CAD software Using three different type of materials Connecting two mechanical models and ACP into static structural Applying boundary conditions, loads and solve the model Applying variable pressure on beam
material
composite
steel
combination
with
beam
reinforced
Tutorial 80: Debonding in composite model
Armin Yousefi Kanani
in
FEM
2
0
Expert
Debonding is another type of interface/interphase failure, which is often classified as interfiber failure. It is simply attributed to the nature of the bond between fiber and matrix, whether occurring through a zero-thickness interface or an interphase region. Debonding is simply a loss of physica/chemical connection between the reinforcing material and the matrix. This could occur for part of a fiber, whole fibers, or many fibers. Simply we can say Debonding happen when two materials stop adhering to each other and Delamination when a laminated material becomes separated, perhaps induced by poor processing during production, impact in service or some other means. Agenda Set up properties for debonding separation inside engineering data Creating Composite model in ACP Using 2 solidmodels tools in ACP to create solid model use contact definitions with cohesive zone material inside Mechanical Introduction of Contact tools in mechanica Applying Boundary conditions and analysis settings Postprocessing
geometry
fea
software
acp
ansys
model
composite
debonding
Tutorial 79: Stress Analysis of Composite T-beam
Armin Yousefi Kanani
in
FEM
2
0
Intermediate
Composite fracture occurs at three modes, depending on three loading scenarios. Mode I is an opening or tensile mode, mode II fractures consist of a sliding or shear effect and mode III fractures occur due to a tearing or shear loading effect. This report will only be looking at fracture modes of type I and II. In practical occurrences of material fracture caused by cracking, especially in metals, mode I type of fracture is predominantly present. Agenda: Set up properties for delaminating interfaces inside engineering data define delaminating interfaces inside ACP Use predefined interfaces from ACP inside Mechanical Alternatively use contact definitions with cohesive zone material inside Mechanical Boundary conditions and analysis settings Postprocessing
T-beam
composite
analysis
stress
Tutorial 78: Stress Analysis of Composite T-beam
Armin Yousefi Kanani
in
FEM
2
0
Intermediate
ACP has a pre- and post-processing mode. In the pre-processing mode, all composite definitions can be created and are mapped to the geometry (FE mesh). These composite definitions are transferred to the FE model and the solver input file. In the post-processing mode, after a completed solution and the import of the result file(s), post-processing results (failure, safety, strains and stresses) can be evaluated and visualized. After a completed solution, the post-processing is used to evaluate the performance of the design and laminate. The post-processing functionality for Solid Models of ACP allows the mapping of ply wise results on to the reference surface of the solid model. This ensures that also failures occurring inside the laminate can be observed and investigated. Failure criteria are used to evaluate the strength of a composite structure. Several failure criteria can be defined, combined and configured in the Definitions object. Failure criteria definitions can be used for failure plots and sampling points. The critical failure mode for an element shown in failure plots and sampling points is the one with the lowest reserve factor. Agenda Connecting ACP to Static Structural Tools in Ansys Doing Stress Analysis Solving the model Analyzing Data in static Sturcutal Analyzing Data in Post-Processing
T-beam
composite
analysis
stress
Tutorial 77: Modelling Composite T-beam in ACP
Armin Yousefi Kanani
in
FEM
2
0
Intermediate
An Oriented Selection Set is an Element Set with additional information about the element orientations. The orientation direction of an Element Set is responsible for setting the stacking direction of the associated lay-up. The Reference Direction is responsible for setting the 0 direction of the associated layup. These two directions must be defined while other parameters like Selection Rules and Draping are optional. The laminate is modeled by defining different Oriented Selection Sets for the different regions. The modeling plies are then associated with the OSS and their order defines the stacking sequence of the laminate. The OSS feature allows you to define several offset directions for one element: OSS can overlap and can have different orientations. In this tutorial we are going to model T-Beam by defining various oriented selection sets. This beam is made from three main parts which are: Top and middle surface, Bonding and covering layers. Agenda: Using multiple oriented selection sets to define a complex composite layup Tapering of core materials Using multiple rosettes and different selection methods
fea
software
ansys
intermediate
acp
T-beam
composite
modelling
Tutorial 76: Stress Analysis of Composite Pressure Vessel (Solid modeling)
Armin Yousefi Kanani
in
FEM
3
1
Intermediate
Meshes can be imported into Mechanical from multiple systems. It is possible to combine composite shell, composite solid, and non-layered shell and solid meshes to perform mixed analysis. Mechanical does not allow overlap of node/element number from multiple systems; therefore, the import fails if the meshes from different systems are overlapping in node/element numbers. Meshes from upstream to downstream Mechanical Models are renumbered automatically to avoid any overlap. For every analysis system (mesh), you have the choice between automatic renumbering (default) and manual configuration. If automatic renumbering is disabled, you must ensure that the element/node numbering is unique for each mesh. In this tutorial, first we will model Composite pressure vessel in ACP then we will model metal parts in mechanical model and at the we will combine models in static structural. Agenda: Solid modeling of composite vessel Add metal parts Transfer parts to ANSYS Mechanical Apply boundary conditions, loads and solve the model Evaluate solid model results in ANSYS Composite PrepPost
solid
modeling
vessel
pressure
composite
analysis
stress
Tutorial 75: Find the Best Laminate Configuration of a Composite Tube under compressive load
Armin Yousefi Kanani
in
FEM
3
0
Expert
The Parameter feature connects Inputs and Outputs to the Parameter Interface in the Workbench project. There are three numerical variables which are diameter, laminate code and thickness. These variables should be applied to ascertain optimum condition for making composite. In this tutorial we are going to solve problem for specific laminated lay up to find critical buckling load on the composite tube model then by using parameter command in ANSYS we will ask software to solve problem for various laminate lay-up, thickness and tube diameter. Agenda: Modeling composite tube geometry in ACP tools Define input parameters for the ply angle of all eight defined plies Importing model into static structural and applying boundary conditions and force Solve the model and define output parameter for Eigenvalue amount Specify design variations in ANSYS Workbench and update all design points
load
compressive
under
tube
composite
configuration
laminate
best
find
Tutorial 74: Modeling Lug in ACP (complex geometry):
Armin Yousefi Kanani
in
FEM
3
0
Expert
Solid model settings control how the solid model is divided into elements in the thickness direction and how drop- and cut-off elements are handled. The level of detail required in the solid model depends on how accurate certain features are to be modeled. This depends on the judgment of the designer. Extrusion guides add more complex possibilities in shaping the model. The cut-off operation is analogous to machining a composite part after curing. In this tutorial we are going to use extrusion guide, cut off element and snap to geometry to create complex geometry. Agenda: Create complex composite model Import geometry for cut-off rule Creating Virtual Geometries Import geometry for Extrusion-guides feature Extrude solid composite using Extrusion- guides feature
complex
geometry
material
composite
acp
lug
modeling
Tutorial 73: Simulate Nonlinear Buckling Analysis of a Half-Symmetry Rectangular Beam with ls-dyna
Armin Yousefi Kanani
in
FEM
3
1
Expert
Simulate Nonlinear Buckling Analysis of a Half-Symmetry Rectangular Beam with ls-dyna
ls-dyna
with
beam
rectangular
Half-Symmetry
analysis
buckling
nonlinear
simulate
Tutorial 72: Modeling and testing single lap joint made with composite material by using contact debonding
Armin Yousefi Kanani
in
FEM
2
1
Beginner
Modeling and testing single lap joint made with composite material by using contact debonding
debonding
contact
using
by
material
composite
with
made
joint
lap
single
testing
modeling
Micro-pressure wave simulation
YE Yang
in
CFD
0
1
Beginner
i am doing my final project and i need to detect the train micro-pressure wave travels in a tunnel. But i don't know how to do it
boundary
computation
ensure
how
Tutorial 66: How to Model Progressive Damage on Composite Plate
Armin Yousefi Kanani
in
Simulation & CAE
2
2
Expert
The progressive damage plot object can display progressive damage results. The overall damage status can be displayed indicating whether no damage, some damage, or complete damage has occurred. The damage variables give an indication of how much the stiffness has reduced for fiber and matrix in tension or compression. The damage variable scale goes from 0 (no damage, 0% stiffness reduction) to the maximum stiffness reduction specified. The highest reduction possible is 1 (complete damage, 100% stiffness reduction Agenda: Defining the engineering properties Defining the damage initiation and damage variable Setup composite lay-up in ACP (Pre) Apply boundary conditions, loads and solve the model Solve Post processing
how
model
progressive
damage
composite
plate
ansys
acp
modeling
material
Tutorial 60: Simulate airbag inflation Workbench LS-DYNA (ACT Extension)
Armin Yousefi Kanani
in
Simulation & CAE
1
0
Beginner
Please find answer in my Youtube channel:
Other
simulate
airbag
inflation
workbench
ls-dyna
act
extension
Tutorial SolidWorks Simulation: Combined Loading
Fahad Rafi
in
Simulation & CAE
0
1
Beginner
SolidWorks Simulation Tutorial: Combined Loading
SOLIDWORKS
resultant
diagrams
total
moment
combined
loading
shear
force
normal
stress
beam
tutorial
simulation
solidworks
Tutorial SolidWorks Simulation: Truss Analysis by Method of Joints
Fahad Rafi
in
Simulation & CAE
0
1
Beginner
Video on YouTube,
SOLIDWORKS
method
finite
analysis
tutorial
element
joints
simulation
truss
solidworks
Tutorial 51: Crush of Filled Soda Can in ansys- Autodyn solver
Armin Yousefi Kanani
in
Simulation & CAE
0
0
Beginner
please check my youtube channel:
Other
autodyn
51
solver
filled
crush
tutorial
ansys
soda
can
tutorial 48: Crush an aluminum beverage can in ansys workbench
Armin Yousefi Kanani
in
Simulation & CAE
0
0
Beginner
Please check my youtube channel:
Other
47
crush
tutorial
workbench
ansys
beverage
can
aluminum
tutorial 46: Simulate the impact of a rod into a plate (Taylor Test)
Armin Yousefi Kanani
in
Simulation & CAE
0
0
Beginner
Please check my Youtube channel:
Other
taylor
into
simulate
46
tutorial
impact
plate
rod
test
Tutorial 46:Temperature Dependent Material simulation in Composite PrepPost Modeling
Armin Yousefi Kanani
in
Simulation & CAE
0
0
Beginner
Please check my youtube channel:
Other
46-temperature
preppost
dependent
tutorial
composite
simulation
material
modeling
Tutorial 36: How to import simulation data in NX 9 Siemens Nastaran after saving file
Armin Yousefi Kanani
in
Simulation & CAE
0
0
Beginner
Please check youtube link: https://www.youtube.com/watch?v=knr-nOEIAug
NX Unigraphics
struggle
closing
many
user
program
this
how
import
will
data
open
after
tutorial
saving
simulation
see
you
file
nx