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    Procedures Involved in The Ansys ACP17.2

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    Vijayanandh R
    The document describes a tensile analysis simulation of a glass fiber reinforced polymer (GFRP) composite material using ANSYS. The objective is to determine the maximum deformation of a composite specimen fixed at one end and loaded with 1000 N of axial force at the other end. The procedure involves modeling the specimen geometry and material properties in ANSYS ACP, generating the mesh and fabric layout, coupling to ANSYS static structural, applying boundary conditions, and solving for total deformation and strain energy results.

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    © All Rights Reserved
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    Procedures Involved in The Ansys ACP17.2

    Uploaded by

    Vijayanandh R
    47 views10 pages
    The document describes a tensile analysis simulation of a glass fiber reinforced polymer (GFRP) composite material using ANSYS. The objective is to determine the maximum deformation of a composite specimen fixed at one end and loaded with 1000 N of axial force at the other end. The procedure involves modeling the specimen geometry and material properties in ANSYS ACP, generating the mesh and fabric layout, coupling to ANSYS static structural, applying boundary conditions, and solving for total deformation and strain energy results.

    Original Description:

    Procedures involved in the Construction of Composite Materials using ANSYS ACP 17.2

    Original Title

    Procedures Involved in the Ansys ACP17.2

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    The document describes a tensile analysis simulation of a glass fiber reinforced polymer (GFRP) composite material using ANSYS. The objective is to determine the maximum deformation of a composite specimen fixed at one end and loaded with 1000 N of axial force at the other end. The procedure involves modeling the specimen geometry and material properties in ANSYS ACP, generating the mesh and fabric layout, coupling to ANSYS static structural, applying boundary conditions, and solving for total deformation and strain energy results.

    Copyright:

    © All Rights Reserved
    Download as DOCX, PDF, TXT or read online from Scribd
    Download as docx, pdf, or txt
    47 views10 pages

    Procedures Involved in The Ansys ACP17.2

    Uploaded by

    Vijayanandh R
    The document describes a tensile analysis simulation of a glass fiber reinforced polymer (GFRP) composite material using ANSYS. The objective is to determine the maximum deformation of a composite specimen fixed at one end and loaded with 1000 N of axial force at the other end. The procedure involves modeling the specimen geometry and material properties in ANSYS ACP, generating the mesh and fabric layout, coupling to ANSYS static structural, applying boundary conditions, and solving for total deformation and strain energy results.

    Copyright:

    © All Rights Reserved
    Download as DOCX, PDF, TXT or read online from Scribd
    Download as docx, pdf, or txt
    of 10

    KCT- AERONAUTICAL ENGINEERING

    LABORATORY WORK BOOK

    Exercise Number: 01

    Lab Code / Lab : U15AEP602 / Design and Simulation

    Course / Branch : BE / Aeronautical Engineering

    Title of the exercise : Tensile Analysis on Composite Material using Ansys


    ACP 17.2

    _______________________________________________________________________

    STEP 1: INTRODUCTION

    a) OBJECTIVE OF THE EXERCISE


     To determine the maximum deformation on the GFRP Composite material, which has been
    fixed at one end and other end is loaded with axial load of 1000 N.

    STEP 2: ACQUISITION

    a) Facilities required to do the exercise:


    ANSYS ACP – 17.2

    b) Problem Description:
    Tensile test is comes under normal test, which is used to estimate the mechanical properties of
    the given test specimen. In this simulation, the tensile test specimen is modelled with the help of
    ASTM D3039 also planned to construct composite laminate, in which five carbon fiber layers and
    epoxy resin are the major contributors. The detailed pictorial representation has been shown in the
    figure 1.

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

    Figure:

    Figure 1. Conceptual Design of Bullet with dimension

    c) Procedure for doing the exercise:


    1. Open “ ANSYS ACP (Pre) - 17.2”

    2. Double Click on "Engineering Data" in order to edit matrix and reinforcement


    properties.

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

    3. Select Composite Materials, in which select E-Glass UD and Epoxy Resin for test
    specimen

    4. Double click on geometry and then click look at option in XY plane.

    5. Create Test Specimen in design modeler tool, in which the ASTM D3039
    provides the dimensional information.

     Generate Tensile test specimen with the help of line tool in design modeler
    and named as sketch1.

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

     Generate surface : Concept - surface from Edges - select sketc1 - enter 0 in


    thickness.
     After this process, green tick enabled in Geometry to educate about its
    process completion.

    6. Double click on Model in order to execute discretization process.


     Assign thickness and reinforcement material to the modeled physical
    object.
     Generate Mesh
     After this process, green tick enabled in Model to educate about its process
    completion.

    7. Enable main contribution of composites (reinforcement and matrix ) and then


    Create Fabric in ANSYS ACP Pre 16.2, which are shown in the below diagram.

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

     In the fabric option, the properties of fiber such as directional young's


    modulus, bulk modulus are assigned, which are shown in the below
    diagram

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

    8. Generate Elements, which will be used for entire set-up (laminate).

    9. Generate Rosette - provide the directional information to the fiber. In the below
    diagram, red arrow shows the fiber direction, which is executed with the help of
    rosette.

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

    10. Generate Oriented Selection set - provide the directional information to the
    laminate. In the below diagram, dark pink arrow shows the laminate direction,
    which is executed with the help of Oriented Selection set.

    11. Generate Modeling Groups - In which, the number of fibers with different
    orientation can be easily executed, which are revealed in the next diagram.

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

    12. Generate Solid model, in which include the matrix as join material in-between the
    fibers.

    13. After this step, the green tick is enabled in set-up menu, which will be ready for
    coupling.

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

    14. With the help of on-way coupling, link set-up of ANSYS ACP 16. 2 to Model of
    Static Structural.

    15. Static structural---support---fixed support----click on one end of the test specimen-


    ---apply
    16. Static Structural----force----click on the other end---1000N---apply
    17. Click solution---total deformation---solve
    18. Note the maximum and minimum displacements

    STEP 3: RESULT

    Total Deformation Results

    Strain Energy Results

    Prof. Vijayanandh R, AP, AERO, KCT.


    KCT- AERONAUTICAL ENGINEERING

    Prof. Vijayanandh R, AP, AERO, KCT.

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