RAIMONDO, ANTONIO

RAIMONDO, ANTONIO  

DIPARTIMENTO DI SCIENZE E TECNOLOGIE AEROSPAZIALI  

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Risultati 1 - 13 di 13 (tempo di esecuzione: 0.018 secondi).
Titolo Data di pubblicazione Autori File
A numerical approach for the evaluation of the local stress ratio in fatigue-driven delamination analysis 1-gen-2019 Raimondo A.Bisagni C.
A Numerical Assessment of the Influence of Local Stress Ratio in the Fatigue Analysis of Post-Buckled Composite Single-Stringer Specimen 1-gen-2024 Raimondo, AntonioBisagni, Chiara
Analysis of local stress ratio for delamination in composites under fatigue loads 1-gen-2020 Raimondo A.Bisagni C.
Cohesive analysis of a 3D benchmark for delamination growth under quasi-static and fatigue loading conditions 1-gen-2022 Raimondo A.Bisagni C. +
Comparison of numerical analyses of a composite wing component subjected to 4-point bending 1-gen-2022 Bisagni C.Raimondo A. +
Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model 1-gen-2025 Raimondo, Antonio +
Experimental study of post-buckled single-stringer composite specimens under fatigue loads with different load levels and load ratios 1-gen-2023 Raimondo A.Bisagni C. +
Experimental study on post-buckled composite single-stringer specimens with initial delamination under fatigue loads 1-gen-2021 Raimondo A.Bisagni C. +
Fatigue analysis of a post-buckled composite single-stringer specimen taking into account the local stress ratio 1-gen-2020 Raimondo A.Bisagni C.
Influence of interface ply orientation on delamination growth in composite laminates 1-gen-2021 Raimondo A.Bisagni C. +
Numerical Investigation of the R-Curve Effect in Delamination of Composite Materials Using Cohesive Elements 1-gen-2024 Raimondo, Antonio
Numerical study of quasi-static and fatigue delamination growth in a post-buckled composite stiffened panel 1-gen-2020 Raimondo A.Bisagni C. +
Study of conduction welded C-struts for a thermoplastic composite fuselage 1-gen-2025 Raimondo, AntonioBisagni, Chiara +