Technical problems associated with fuel containment and damage tolerance of composite material wings for transport aircraft were identified. The major tasks are the following: (1) the preliminary design of damage tolerant wing surface using composite materials; (2) the evaluation of fuel sealing and lightning protection methods for a composite material wing; and (3) an experimental investigation of the damage tolerant characteristics of toughened resin graphite/epoxy materials. The test results, the test techniques, and the test data are presented.


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    Titel :

    Fuel Containment and Damage Tolerance for Large Composite Primary Aircraft Structures. Phase 1. Testing


    Beteiligte:
    J. P. Sandifer (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    501 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch