Generating the Best Stacking Sequence Table for the Design of Blended Composite Structures

    Research output: Contribution to conferencePaper

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    Abstract

    In order to improve the ability of a large-scale light-weight composite structure to carry tensile or compressive loads, stiffeners are added to the structure. The stiffeners divide the structure into several smaller panels. For a composite structure to be manufacturable, it is necessary that plies are continuous in multiple adjacent panels. To be able to prescribe a manufacturable design, an optimization algorithm can be coupled with a reference table for the stacking sequences (SST). As long as the ply stacks are selected from the SST, it is guaranteed that the design is manufacturable and all strength related guidelines associated with the design of composite structures are satisfied.
    An SST is made only based on strength related guidelines. Therefore, there exist a large number of possibilities for SSTs. Minimized mass is a typical goal in the design of aircraft structures. Different SSTs result in different values for the minimized mass. Thus it is crucial to perform optimization based on the SST which results in the lowest mass. This paper aims to introduce an approach to generate a unique SST resulting in the lowest mass. The proposed method is applied to the optimization problem of a stiffened composite structure resembling the skin of an aircraft wing box.
    Original languageEnglish
    Publication statusPublished - 1 Jun 2017
    Event12th World Congress of Structural and Multidisciplinary Optimisation - Technische Universität Braunschweig, Braunschweig, Germany
    Duration: 5 Jun 20179 Jun 2017
    http://www.wcsmo12.org/

    Conference

    Conference12th World Congress of Structural and Multidisciplinary Optimisation
    Abbreviated titleWCSMO12
    CountryGermany
    CityBraunschweig
    Period5/06/179/06/17
    Internet address

    Fingerprint

    Composite structures
    Skin
    Aircraft

    Keywords

    • blending
    • composite structures
    • stacking sequence table

    Cite this

    Farzan Nasab, F., Geijselaers, H. J. M., Baran, I., & de Boer, A. (2017). Generating the Best Stacking Sequence Table for the Design of Blended Composite Structures. Paper presented at 12th World Congress of Structural and Multidisciplinary Optimisation, Braunschweig, Germany.
    Farzan Nasab, F. ; Geijselaers, H. J.M. ; Baran, I. ; de Boer, A. / Generating the Best Stacking Sequence Table for the Design of Blended Composite Structures. Paper presented at 12th World Congress of Structural and Multidisciplinary Optimisation, Braunschweig, Germany.
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    title = "Generating the Best Stacking Sequence Table for the Design of Blended Composite Structures",
    abstract = "In order to improve the ability of a large-scale light-weight composite structure to carry tensile or compressive loads, stiffeners are added to the structure. The stiffeners divide the structure into several smaller panels. For a composite structure to be manufacturable, it is necessary that plies are continuous in multiple adjacent panels. To be able to prescribe a manufacturable design, an optimization algorithm can be coupled with a reference table for the stacking sequences (SST). As long as the ply stacks are selected from the SST, it is guaranteed that the design is manufacturable and all strength related guidelines associated with the design of composite structures are satisfied.An SST is made only based on strength related guidelines. Therefore, there exist a large number of possibilities for SSTs. Minimized mass is a typical goal in the design of aircraft structures. Different SSTs result in different values for the minimized mass. Thus it is crucial to perform optimization based on the SST which results in the lowest mass. This paper aims to introduce an approach to generate a unique SST resulting in the lowest mass. The proposed method is applied to the optimization problem of a stiffened composite structure resembling the skin of an aircraft wing box.",
    keywords = "blending, composite structures, stacking sequence table",
    author = "{Farzan Nasab}, F. and Geijselaers, {H. J.M.} and I. Baran and {de Boer}, A.",
    year = "2017",
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    note = "12th World Congress of Structural and Multidisciplinary Optimisation, WCSMO12 ; Conference date: 05-06-2017 Through 09-06-2017",
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    Farzan Nasab, F, Geijselaers, HJM, Baran, I & de Boer, A 2017, 'Generating the Best Stacking Sequence Table for the Design of Blended Composite Structures' Paper presented at 12th World Congress of Structural and Multidisciplinary Optimisation, Braunschweig, Germany, 5/06/17 - 9/06/17, .

    Generating the Best Stacking Sequence Table for the Design of Blended Composite Structures. / Farzan Nasab, F.; Geijselaers, H. J.M.; Baran, I.; de Boer, A.

    2017. Paper presented at 12th World Congress of Structural and Multidisciplinary Optimisation, Braunschweig, Germany.

    Research output: Contribution to conferencePaper

    TY - CONF

    T1 - Generating the Best Stacking Sequence Table for the Design of Blended Composite Structures

    AU - Farzan Nasab, F.

    AU - Geijselaers, H. J.M.

    AU - Baran, I.

    AU - de Boer, A.

    PY - 2017/6/1

    Y1 - 2017/6/1

    N2 - In order to improve the ability of a large-scale light-weight composite structure to carry tensile or compressive loads, stiffeners are added to the structure. The stiffeners divide the structure into several smaller panels. For a composite structure to be manufacturable, it is necessary that plies are continuous in multiple adjacent panels. To be able to prescribe a manufacturable design, an optimization algorithm can be coupled with a reference table for the stacking sequences (SST). As long as the ply stacks are selected from the SST, it is guaranteed that the design is manufacturable and all strength related guidelines associated with the design of composite structures are satisfied.An SST is made only based on strength related guidelines. Therefore, there exist a large number of possibilities for SSTs. Minimized mass is a typical goal in the design of aircraft structures. Different SSTs result in different values for the minimized mass. Thus it is crucial to perform optimization based on the SST which results in the lowest mass. This paper aims to introduce an approach to generate a unique SST resulting in the lowest mass. The proposed method is applied to the optimization problem of a stiffened composite structure resembling the skin of an aircraft wing box.

    AB - In order to improve the ability of a large-scale light-weight composite structure to carry tensile or compressive loads, stiffeners are added to the structure. The stiffeners divide the structure into several smaller panels. For a composite structure to be manufacturable, it is necessary that plies are continuous in multiple adjacent panels. To be able to prescribe a manufacturable design, an optimization algorithm can be coupled with a reference table for the stacking sequences (SST). As long as the ply stacks are selected from the SST, it is guaranteed that the design is manufacturable and all strength related guidelines associated with the design of composite structures are satisfied.An SST is made only based on strength related guidelines. Therefore, there exist a large number of possibilities for SSTs. Minimized mass is a typical goal in the design of aircraft structures. Different SSTs result in different values for the minimized mass. Thus it is crucial to perform optimization based on the SST which results in the lowest mass. This paper aims to introduce an approach to generate a unique SST resulting in the lowest mass. The proposed method is applied to the optimization problem of a stiffened composite structure resembling the skin of an aircraft wing box.

    KW - blending

    KW - composite structures

    KW - stacking sequence table

    M3 - Paper

    ER -

    Farzan Nasab F, Geijselaers HJM, Baran I, de Boer A. Generating the Best Stacking Sequence Table for the Design of Blended Composite Structures. 2017. Paper presented at 12th World Congress of Structural and Multidisciplinary Optimisation, Braunschweig, Germany.