The current work is based on the implementation of the CODAM2 intralaminar damage model in CUF-Explicit, an explicit nonlinear dynamics solver based on the Carrera Unified Formulation (CUF). The CODAM2 model is based on the concept of continuum damage mechanics, and stress-based failure criteria are used to determine the onset of damage. The damage progression makes use of the crack-band theory to scale the fracture energies, thus ensuring mesh objectivity. The structural modelling is performed using high-order 2D theories based on CUF. 2D elements are used to model the structural geometry, and 1D expansions based on Lagrange polynomials are used to define the thickness, resulting in a layer-wise modelling approach. Numerical assessments are performed considering single elements and tensile coupons. The results are in good agreement with reference numerical solutions and experimental data, thus verifying the current implementation.

HIGH-FIDELITY DAMAGE ANALYSIS OF COMPOSITES USING A PLY-BASED CONTINUUM MODEL / Nagaraj, M. H.; Reiner, J.; Vaziri, R.; Carrera, E.; Petrolo, M.. - ELETTRONICO. - (2019), pp. 1113-1121. (Intervento presentato al convegno XXV International Congress of Aeronautics and Astronautics, AIDAA 2019 tenutosi a Rome nel 9-12 September 2019).

HIGH-FIDELITY DAMAGE ANALYSIS OF COMPOSITES USING A PLY-BASED CONTINUUM MODEL

M. H. Nagaraj;E. Carrera;M. Petrolo
2019

Abstract

The current work is based on the implementation of the CODAM2 intralaminar damage model in CUF-Explicit, an explicit nonlinear dynamics solver based on the Carrera Unified Formulation (CUF). The CODAM2 model is based on the concept of continuum damage mechanics, and stress-based failure criteria are used to determine the onset of damage. The damage progression makes use of the crack-band theory to scale the fracture energies, thus ensuring mesh objectivity. The structural modelling is performed using high-order 2D theories based on CUF. 2D elements are used to model the structural geometry, and 1D expansions based on Lagrange polynomials are used to define the thickness, resulting in a layer-wise modelling approach. Numerical assessments are performed considering single elements and tensile coupons. The results are in good agreement with reference numerical solutions and experimental data, thus verifying the current implementation.
2019
978-88-943960-1-0
File in questo prodotto:
File Dimensione Formato  
Nagaraj_RVCP_AIDAA2019.pdf

accesso aperto

Descrizione: Paper
Tipologia: 2. Post-print / Author's Accepted Manuscript
Licenza: Creative commons
Dimensione 490.86 kB
Formato Adobe PDF
490.86 kB Adobe PDF Visualizza/Apri
Pubblicazioni consigliate

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11583/2751834
 Attenzione

Attenzione! I dati visualizzati non sono stati sottoposti a validazione da parte dell'ateneo