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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    Title :

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


    Contributors:

    Publication date :

    1983


    Size :

    501 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English