RAIMONDO, ANTONIO
RAIMONDO, ANTONIO
DIPARTIMENTO DI SCIENZE E TECNOLOGIE AEROSPAZIALI
A fast numerical procedure for the simulation of inter-laminar damage growth in stiffened composite panels
2016-01-01 Riccio, A.; Damiano, M.; Raimondo, A.; Di Felice, G.; Sellitto, A.
A numerical approach for the evaluation of the local stress ratio in fatigue-driven delamination analysis
2019-01-01 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
2024-01-01 Raimondo, Antonio; Bisagni, Chiara
A numerical procedure for the simulation of skin–stringer debonding growth in stiffened composite panels
2014-01-01 Riccio, A.; Raimondo, A.; Di Felice, G.; Scaramuzzino, F.
A numerical study on the impact behaviour of natural fibres made honeycomb cores
2018-01-01 Riccio, A.; Raimondo, A.; Saputo, S.; Sellitto, A.; Battaglia, M.; Petrone, G.
A numerical/experimental study on the induction heating of adhesives for composite materials bonding
2018-01-01 Riccio, A.; Russo, A.; Raimondo, A.; Cirillo, P.; Caraviello, A.
A robust numerical approach for the simulation of skin–stringer debonding growth in stiffened composite panels under compression
2015-01-01 Riccio, A.; Raimondo, A.; Scaramuzzino, F.
A Study on Skin Delaminations Growth in Stiffened Composite Panels by a Novel Numerical Approach
2013-01-01 Riccio, A.; Raimondo, A.; Scaramuzzino, F.
Analysis of local stress ratio for delamination in composites under fatigue loads
2020-01-01 Raimondo, A.; Bisagni, C.
Cohesive analysis of a 3D benchmark for delamination growth under quasi-static and fatigue loading conditions
2022-01-01 Raimondo, A.; Davila, C. G.; Bisagni, C.
Comparison of numerical analyses of a composite wing component subjected to 4-point bending
2022-01-01 Bisagni, C.; Raimondo, A.; Atanasovska, I.; Milic, M.; Troian, R.; Frulla, G.; Polla, A.; Cora, O. N.; Bekci, M. L.; Henriques, B.; de Moura, M. F. S. F.; Almudaihesh, F.; Grigg, S.
Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model
2025-01-01 Miranda, Mário; Cini, Andrea; Raimondo, Antonio; Tita, Volnei
Delamination buckling and growth phenomena in stiffened composite panels under compression. Part I: An experimental study
2014-01-01 Riccio, A; Raimondo, A; Fragale, S; Camerlingo, F; Gambino, B; Toscano, C; Tescione, D
Delaminations buckling and growth phenomena in stiffened composite panels under compression. Part II: a numerical study
2013-01-01 Riccio, A; Raimondo, A; Caprio, F Di; Scaramuzzino, F
Detailed Methodologies for Integrated Delamination Growth and Fiber-Matrix Damage Progression Simulation
2015-01-01 Riccio, Aniello; Pietropaoli, Elisa; Raimondo, Antonio
Development and application of a numerical procedure for the simulation of the “Fibre Bridging” phenomenon in composite structures
2017-01-01 Riccio, A.; Russo, A.; Sellitto, A.; Raimondo, A.
Experimental and numerical investigation on the crashworthiness of a composite fuselage sub-floor support system
2018-01-01 Riccio, A.; Raimondo, A.; Di Caprio, F.; Fusco, M.; Sanità, P.
Experimental study of post-buckled single-stringer composite specimens under fatigue loads with different load levels and load ratios
2023-01-01 Paz, J.; Raimondo, A.; Bisagni, C.
Experimental study on post-buckled composite single-stringer specimens with initial delamination under fatigue loads
2021-01-01 Raimondo, A.; Mendez, J. P.; Bisagni, C.
Fatigue analysis of a post-buckled composite single-stringer specimen taking into account the local stress ratio
2020-01-01 Raimondo, A.; Bisagni, C.