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    Transverse shear stiffness for double "V" corrugated-core sandwich panel

    New search for: Sapowith, A.D.

    Report adapts principles of C.LIBOVE and R.E.HUBKA to predict one of elastic constants for this panel; value of this constant represents transverse shear stiffness of panel; formulas and charts for evaluation of constant and experimental data.

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    Transverse shear stiffness for double "V" corrugated-core sandwich panel

    New search for: Sapowith, A.D.

    Report adapts principles of C.LIBOVE and R.E.HUBKA to predict one of elastic constants for this panel; value of this constant represents transverse shear stiffness of panel; formulas and charts for evaluation of constant and experimental data.

    Access

    Access via TIB
    Check availability in my library

    Transverse shear stiffness for double "V" corrugated-core sandwich panel

    New search for: Sapowith, A.D.

    Report adapts principles of C.LIBOVE and R.E.HUBKA to predict one of elastic constants for this panel; value of this constant represents transverse shear stiffness of panel; formulas and charts for evaluation of constant and experimental data.

    Access

    Access via TIB
    Check availability in my library

    Access

    Access via TIB
    Check availability in my library

    Page navigation

    Document information
    Similar titles

    Export, share and cite

    Document information
    Title:

    Transverse shear stiffness for double "V" corrugated-core sandwich panel

    Additional title:

    Aero/Space Eng

    Contributors:

    Sapowith, A.D. (author)

    Published in:

    Aero/Space Engineering ; 18

    Publication date:

    1959

    Size:

    4 pages

    Type of media:

    Article (Journal)

    Type of material:

    Print

    Language:

    English

    Keywords:

    Aircraft manufacture

    © Metadata Copyright Elsevier B. V. All rights reserved.

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