Recherche

Voici les éléments 11-17 de 17

Lamb waves scattering model for identification of damage parameters

Communication sans acte

BRIAND, William;

RÉBILLAT, Marc;

GUSKOV, Mikhail;

MECHBAL, Nazih (CBM Academy, 2022-05)

Generation of controlled delaminations in composites using symmetrical laser shock configuration

Article dans une revue avec comité de lecture

GHRIB, Meriem; BERTHE, Laurent; ECAULT, Romain; BEDREDDINE, Nas;

MECHBAL, Nazih;

GUSKOV, Mikhail;

RÉBILLAT, Marc (Elsevier, 2017)

Signal-based versus nonlinear model-based damage sensitive features for delamination quantification in CFRP composites

Communication avec acte

GHRIB, Meriem; BERTHE, Laurent;

MECHBAL, Nazih;

GUSKOV, Mikhail;

RÉBILLAT, Marc (2017)

LASER shock delamination generation and machine learning-based damage quantification in CFRP composites plates

Communication avec acte

GHRIB, Meriem; BERTHE, Laurent;

MECHBAL, Nazih;

GUSKOV, Mikhail;

RÉBILLAT, Marc (A. Benjeddou and Z. Aboura, 2018)

INVESTIGATION OF NONLINEAR LAMB WAVE/DAMAGE INTERACTION: NUMERICAL AND EXPERIMENTAL APPROACHES

Communication avec acte

LI, Xixi;

MONTEIRO, Eric;

MECHBAL, Nazih;

GUSKOV, Mikhail;

RÉBILLAT, Marc (A. Benjeddou, N. Mechbal and J.F. Deü, 2019)

Damage imaging post processing for delamination size assessment of CFRP aeronautic structures

Communication avec acte

BRIAND, William;

MECHBAL, Nazih;

GUSKOV, Mikhail;

RÉBILLAT, Marc (2020)

Damage Size Quantification Using Lamb Waves by Analytical Model Identification

Communication avec acte

BRIAND, William;

RÉBILLAT, Marc;

GUSKOV, Mikhail;

MECHBAL, Nazih (Springer International Publishing, 2022-06)

Recherche

Filtres

Lamb waves scattering model for identification of damage parameters

Generation of controlled delaminations in composites using symmetrical laser shock configuration

Signal-based versus nonlinear model-based damage sensitive features for delamination quantification in CFRP composites

LASER shock delamination generation and machine learning-based damage quantification in CFRP composites plates

INVESTIGATION OF NONLINEAR LAMB WAVE/DAMAGE INTERACTION: NUMERICAL AND EXPERIMENTAL APPROACHES

Damage imaging post processing for delamination size assessment of CFRP aeronautic structures

Damage Size Quantification Using Lamb Waves by Analytical Model Identification