Evaluation of experimental, commercially fabricated sandwich structure plastic landing mat made of glass fabric reinforced phenolic resin honeycomb core bonded top and bottom to glass reinforced epoxy resin facings; determination and comparison of structural properties of plastic mat and steel mat; laboratory tests indicated major deficiency in strength of adhesive bond between extruded aluminum connectors and facings of plastic mat; traffic tests were conducted with single-wheel load of 50,000 lb and tire pressure of 200 psi on mat-surfaced subgrade with average initial CBR of 14.


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    Titel :

    Engineering tests of T13 plastic airplane landing mat


    Weitere Titelangaben:

    U S Waterways Experiment Station -- Tech Report


    Beteiligte:
    Turner, R. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    51 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Engineering tests of T14 plastic airplane landing mat

    Green, H.L. | Engineering Index Backfile | 1967




    Engineering tests of modified T12 plastic airplane landing mat

    Green, H.L. | Engineering Index Backfile | 1968