Abstract This chapter describes the methods by which an aeroplane’s main flight structure is proven to be fit for purpose, through a combination of analysis and test, explaining that the use of numerical (finite element) methods is usually unsuitable as an approval tool. Special cases where approval by test only are described. Materials fatigue is also considered, describing the philosophy behind achieving fatigue resistant structures.
Approving an Aircraft’s Main Flight Structure
Initial Airworthiness ; 123-138
2nd ed. 2018
01.01.2018
16 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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