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Mostrando ítems 1-10 de 64
On The Use Of The Wave Finite Element Method For Passive Vibration Control Of Periodic Structures
(Techno-PressDaejeon, 2016)
Modeling the growth of LT and TL-oriented fatigue cracks in longitudinally and transversely pre-strained Al 2524-T3 alloy
(2011-09-23)
The aluminum alloy 2524 (Al-Cu-Mg) was developed during the 90s mainly to be employed in aircraft fuselage panels, replacing the standard Al 2024. In the present analysis the fatigue crack growth (FCG) behavior of 2524-T3 ...
Modeling the growth of LT and TL-oriented fatigue cracks in longitudinally and transversely pre-strained Al 2524-T3 alloy
(2011-09-23)
The aluminum alloy 2524 (Al-Cu-Mg) was developed during the 90s mainly to be employed in aircraft fuselage panels, replacing the standard Al 2024. In the present analysis the fatigue crack growth (FCG) behavior of 2524-T3 ...
Multiscale analysis of multiple cracks in aircraft fuselage
(University of Technology Compiégne, 2018-11)
Metodología para simulación de fenómenos de perforación en placas debidos a fallas del tipo no contenida de turbinas de avión
(2009-06-19)
ABSTRACT: In this Project a Methodology is developed by using the finite element method (FEA), to simulate impact of debris from rotating parts that fail during operation of an aircraft engine uncontained by the engine ...
A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures
(2006-07-01)
Weight reduction and improved damage tolerance characteristics were the prime drivers to develop new family of materials for the aerospace/ aeronautical industry. Aiming this objective, a new lightweight Fiber/ Metal ...
A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures
(2006-07-01)
Weight reduction and improved damage tolerance characteristics were the prime drivers to develop new family of materials for the aerospace/ aeronautical industry. Aiming this objective, a new lightweight Fiber/ Metal ...
On the finite element modeling of fatigue crack growth in pressurized cylindrical shells
(ELSEVIER SCI LTD, 2009)
A methodology for the computational modeling of the fatigue crack growth in pressurized shell structures, based on the finite element method and concepts of Linear Elastic Fracture Mechanics, is presented. This methodology ...
Análise estrutural do conjunto asa-fuselagem de uma aeronave de aerodesign
(Joinville, SC, 2020-12-02)
A análise estrutural de uma aeronave é parte essencial do projeto, pois além de garantir segurança, a torna mais leve, eficiente e, consequentemente, econômica. A competição de aerodesign da Society of Automotive Engineers ...