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Tuesday, May 5, 2020 | History

3 edition of Scaling effects in carbon/epoxy laminates under transverse quasi-staic loading found in the catalog.

Scaling effects in carbon/epoxy laminates under transverse quasi-staic loading

Scaling effects in carbon/epoxy laminates under transverse quasi-staic loading

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Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, Springfield, VA .
Written in English

    Subjects:
  • Scaling.,
  • Epoxy matrix composites.,
  • Impact tests.,
  • Static tests.,
  • Static loads.

  • Edition Notes

    Other titlesScaling effects in carbon epoxy laminates under transverse quasi-static loading.
    StatementAlan T. Nettles, Michael J. Douglas, Eric E. Estes.
    Series[NASA technical memorandum] -- NASA/TM-1999-209103., NASA technical memorandum -- 209103.
    ContributionsDouglas, Michael J., Estes, Eric E., Langley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL15548980M


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Scaling effects in carbon/epoxy laminates under transverse quasi-staic loading Download PDF EPUB FB2

Get this from a library. Scaling effects in carbon/epoxy laminates under transverse quasi-static loading. [A T Nettles; M J Douglas; Eric E Estes; Langley Research Center.]. laminates, but damage size-effects were significant.

The aim of the present work is to investigate ex- perimentally the impact scaling of low fibre-volume. The maximum principal stress of E-glass/epoxy layer in the PCB with mm thickness under the shock loading by the finite element analysis is MPa and is.

Full text of "A Comparison of Quasi-Static Indentation and Drop-Weight Impact Testing on Carbon-Epoxy Laminates" See other formats. Stout MG, Koss DA, Liu C, Idasetima J () Damage development in carbon/epoxy laminates under quasi-static and dynamic loading.

Compos .