Abstract This chapter is an adjunct to Chap. 16 . The present chapter first summarizes the evolution of residual strength design requirements for metallic aircraft structures. There follows a concise discussion of the methods for assessing the residual strengths of aircraft structures, with the emphasis on testing and data requirements.
Residual Strength Requirements for Aircraft Structures
08.11.2016
14 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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