Journal of Aircraft, 2013, Volume : 50, Numéro : 6
This paper presents a stress intensity factor solution for cracks located in panels reinforced with arbitrarily located stringers. The new solution was...
Proceedings of the Institution of Mechanical Engineers, 1 novembre 2011, Volume : 226, Numéro : 11
This article presents the results obtained from the development of advanced damage tolerance analysis (DTA) and risk analysis methodologies and tools for...
55th AIAA/ASMe/ASCE/AHS/SC Structures, AIAA, janvier 2014
An optimization based methodology was developed to calculate equivalent initial flaw sizes (EIFS) consistent with multiple-site damage in-service findings. The...
28th Congress of the International Council of the Aeronautical Sciences 2012, 2012, Volume : 3
This paper presents some recent results of NRC research on risk assessment for aircraft structures. First, this paper briefly reviews the Canadian Forces (CF)...
ICAF 2011 Structural Integrity: Influence of Efficiency and Green Imperatives - Proceedings of the 26th Symposium of the International Committee on Aeronautical Fatigue, 2011
Damage tolerance analysis (DTA) of complex aircraft structures requires stress intensity correction factor (β-factor) solutions that cannot be accurately or...
12th International Conference on Fracture 2009, Curran Associates, 2009
Quantitative risk assessment (QRA) is now required by most aircraft structural integrity programs. One of the key components of an accurate QRA resides in the...