Two stage damage tolerance evaluation of an aircraft fuselage panel with a circumferential crack and a broken stringer
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
01.01.2013
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2013
|On damage tolerance design of fuselage structure. Circumferential cracks
Tema Archiv | 1987
|On damage tolerance design of fuselage structure - circumferential cracks
Tema Archiv | 1987
|Influence of Bonded Crack Retarders on Damage Tolerance Performance of Fuselage Panel
Springer Verlag | 2019
|Aspects of Damage Tolerance of Aircraft Fuselage Structures
British Library Conference Proceedings | 2008
|