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    Composite Design Methodology: Design of Composite Trails for the U.S. Army’s M198 Howitzer, A Case Study

    Source: Journal of Mechanical Design:;1996:;volume( 118 ):;issue: 002::page 286
    Author:
    E. Sancaktar
    ,
    K. R. Miner
    ,
    M. West
    DOI: 10.1115/1.2826882
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Analysis and design of a fiber reinforced organic composite trail pair for the U.S. Army M198 Howitzer is presented as a case study in composite material design methodology. For this purpose mechanics analysis is performed using the computer program: MIC-MAC composites design and ANSYS 4.4A finite element analysis. The analyses includes composite lamination, material optimization, adhesive bonding, buckling, deflection, stress and failure analysis and validates the practicability of the proposed constant cross-section graphite/epoxy trail. The use of PC based spreadsheet MIC-MAC program, initially, allows efficient and inexpensive evaluation of several alternative designs including different geometries and materials before the finite element program is employed with the few final design choices to rule out failure in stress, deflection and buckling modes. However, superposition principles need to be used to describe the complex loading configuration as a collection of mechanically equivalent individual load modes such as midspan loaded beam, cantilever beam under torsion, in-plane loaded plate etc. in order to be able to utilize the MIC-MAC program initially. Fabrication plans are also proposed for the trail pair.
    keyword(s): Composite materials , Design , Design methodology , Stress , Buckling , Deflection , Finite element analysis , Optimization , Adhesives , Fibers , Cantilever beams , Manufacturing , Bonding , Failure , Failure analysis , Graphite , Laminations , Army , Computer software , Epoxy adhesives AND Torsion ,
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      Composite Design Methodology: Design of Composite Trails for the U.S. Army’s M198 Howitzer, A Case Study

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/117428
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    • Journal of Mechanical Design

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    contributor authorE. Sancaktar
    contributor authorK. R. Miner
    contributor authorM. West
    date accessioned2017-05-08T23:51:08Z
    date available2017-05-08T23:51:08Z
    date copyrightJune, 1996
    date issued1996
    identifier issn1050-0472
    identifier otherJMDEDB-27636#286_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117428
    description abstractAnalysis and design of a fiber reinforced organic composite trail pair for the U.S. Army M198 Howitzer is presented as a case study in composite material design methodology. For this purpose mechanics analysis is performed using the computer program: MIC-MAC composites design and ANSYS 4.4A finite element analysis. The analyses includes composite lamination, material optimization, adhesive bonding, buckling, deflection, stress and failure analysis and validates the practicability of the proposed constant cross-section graphite/epoxy trail. The use of PC based spreadsheet MIC-MAC program, initially, allows efficient and inexpensive evaluation of several alternative designs including different geometries and materials before the finite element program is employed with the few final design choices to rule out failure in stress, deflection and buckling modes. However, superposition principles need to be used to describe the complex loading configuration as a collection of mechanically equivalent individual load modes such as midspan loaded beam, cantilever beam under torsion, in-plane loaded plate etc. in order to be able to utilize the MIC-MAC program initially. Fabrication plans are also proposed for the trail pair.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleComposite Design Methodology: Design of Composite Trails for the U.S. Army’s M198 Howitzer, A Case Study
    typeJournal Paper
    journal volume118
    journal issue2
    journal titleJournal of Mechanical Design
    identifier doi10.1115/1.2826882
    journal fristpage286
    journal lastpage293
    identifier eissn1528-9001
    keywordsComposite materials
    keywordsDesign
    keywordsDesign methodology
    keywordsStress
    keywordsBuckling
    keywordsDeflection
    keywordsFinite element analysis
    keywordsOptimization
    keywordsAdhesives
    keywordsFibers
    keywordsCantilever beams
    keywordsManufacturing
    keywordsBonding
    keywordsFailure
    keywordsFailure analysis
    keywordsGraphite
    keywordsLaminations
    keywordsArmy
    keywordsComputer software
    keywordsEpoxy adhesives AND Torsion
    treeJournal of Mechanical Design:;1996:;volume( 118 ):;issue: 002
    contenttypeFulltext
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