SHM of composite plates: vibration based method by using PZT sensors (2014)
- Authors:
- USP affiliated authors: TITA, VOLNEI - EESC ; MEDEIROS, RICARDO DE - EESC ; SARTORATO, MURILO - EESC
- Unidade: EESC
- Subjects: DANO; VIBRAÇÕES DE AERONAVES; ENGENHARIA AERONÁUTICA
- Language: Inglês
- Imprenta:
- Source:
- Título do periódico: Proceedings
- Conference titles: International Conference on Noise and Vibration Engineering - ISMA
-
ABNT
MEDEIROS, Ricardo de et al. SHM of composite plates: vibration based method by using PZT sensors. 2014, Anais.. Heverlee: KU Leuven, 2014. . Acesso em: 02 maio 2024. -
APA
Medeiros, R. de, Sartorato, M., Vandepitte, D., & Tita, V. (2014). SHM of composite plates: vibration based method by using PZT sensors. In Proceedings. Heverlee: KU Leuven. -
NLM
Medeiros R de, Sartorato M, Vandepitte D, Tita V. SHM of composite plates: vibration based method by using PZT sensors. Proceedings. 2014 ;[citado 2024 maio 02 ] -
Vancouver
Medeiros R de, Sartorato M, Vandepitte D, Tita V. SHM of composite plates: vibration based method by using PZT sensors. Proceedings. 2014 ;[citado 2024 maio 02 ] - A multiscale based continuum model: influence of crack sliding mode on composite materials damage evolution
- A finite element for active composite plates with peizoelectric layers and experimental validation
- Computational simulation using PZT as sensor elements for damage detection on impacted composite cylinders
- Vibration-based damage identification applied for composite plate: numerical analysis
- Numerical and experimental analyses about SHM metrics using piezoelectric materials
- A finite element for active composite plates with piezoelectric layers applied to composite cylinders
- Representative volume element based transverse shear characterisation of laminated composites
- Detecção de dano em cilindros de compósitos empregando material piezelétrico
- Numerical and analytical approaches for computing efffective elastic properties in composite materials under imperfect contact adherence
- Influence of the transversal shear effects on structural analysis of aircraft tails
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas