Abstract The investigation and formal approval of aircraft structures is a necessary step in ensuring initial and continued airworthiness. While component can be predicted using analytical tools, ultimately, the structures must be tested under flight conditions. Substantial over-engineering is unacceptable, due to weight constraints. This chapter therefore describes the main principles of structural approval of aircraft structures, by combination of analysis and test.


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    Title :

    First Principles of Structural Approval


    Contributors:

    Published in:

    Edition :

    2nd ed. 2018


    Publication date :

    2018-01-01


    Size :

    9 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English