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High-fidelity modeling for health monitoring in honeycomb sandwich structures

Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSN › Conference contribution/Paper › peer-review

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High-fidelity modeling for health monitoring in honeycomb sandwich structures. / Luchinsky, Dmitry G.; Hafiychuk, Vasyl; Smelyanskiy, Vadim et al.
2011 Aerospace Conference, AERO 2011. IEEE, 2011. 5747569 (IEEE Aerospace Conference Proceedings).

Research output: Contribution in Book/Report/Proceedings - With ISBN/ISSN › Conference contribution/Paper › peer-review

Harvard

Luchinsky, DG, Hafiychuk, V, Smelyanskiy, V, Tyson, RW, Walker, JL & Miller, JL 2011, High-fidelity modeling for health monitoring in honeycomb sandwich structures. in 2011 Aerospace Conference, AERO 2011., 5747569, IEEE Aerospace Conference Proceedings, IEEE, 2011 IEEE Aerospace Conference, AERO 2011, Big Sky, MT, United States, 5/03/11. https://doi.org/10.1109/AERO.2011.5747569

APA

Luchinsky, D. G., Hafiychuk, V., Smelyanskiy, V., Tyson, R. W., Walker, J. L., & Miller, J. L. (2011). High-fidelity modeling for health monitoring in honeycomb sandwich structures. In 2011 Aerospace Conference, AERO 2011 Article 5747569 (IEEE Aerospace Conference Proceedings). IEEE. https://doi.org/10.1109/AERO.2011.5747569

Vancouver

Luchinsky DG, Hafiychuk V, Smelyanskiy V, Tyson RW, Walker JL, Miller JL. High-fidelity modeling for health monitoring in honeycomb sandwich structures. In 2011 Aerospace Conference, AERO 2011. IEEE. 2011. 5747569. (IEEE Aerospace Conference Proceedings). doi: 10.1109/AERO.2011.5747569

Author

Luchinsky, Dmitry G. ; Hafiychuk, Vasyl ; Smelyanskiy, Vadim et al. / High-fidelity modeling for health monitoring in honeycomb sandwich structures. 2011 Aerospace Conference, AERO 2011. IEEE, 2011. (IEEE Aerospace Conference Proceedings).

Bibtex

@inproceedings{efc467ff9619486784d2a9056fc8bf98,
title = "High-fidelity modeling for health monitoring in honeycomb sandwich structures",
abstract = "High-Fidelity Model of the sandwich composite structure with real geometry is reported. The model includes two composite facesheets, honeycomb core, piezoelectric actuator/sensors, adhesive layers, and the impactor. The novel feature of the model is that it includes modeling of the impact and wave propagation in the structure before and after the impact. Results of modeling of the wave propagation, impact, and damage detection in sandwich honeycomb plates using piezoelectric actuator/sensor scheme are reported. The results of the simulations are compared with the experimental results. It is shown that the model is suitable for analysis of the physics of failure due to the impact and for testing structural health monitoring schemes based on guided wave propagation.",
author = "Luchinsky, {Dmitry G.} and Vasyl Hafiychuk and Vadim Smelyanskiy and Tyson, {Richard W.} and Walker, {James L.} and Miller, {Jimmy L.}",
year = "2011",
month = may,
day = "13",
doi = "10.1109/AERO.2011.5747569",
language = "English",
isbn = "9781424473502",
series = "IEEE Aerospace Conference Proceedings",
publisher = "IEEE",
booktitle = "2011 Aerospace Conference, AERO 2011",
note = "2011 IEEE Aerospace Conference, AERO 2011 ; Conference date: 05-03-2011 Through 12-03-2011",

}

RIS

TY - GEN

T1 - High-fidelity modeling for health monitoring in honeycomb sandwich structures

AU - Luchinsky, Dmitry G.

AU - Hafiychuk, Vasyl

AU - Smelyanskiy, Vadim

AU - Tyson, Richard W.

AU - Walker, James L.

AU - Miller, Jimmy L.

PY - 2011/5/13

Y1 - 2011/5/13

N2 - High-Fidelity Model of the sandwich composite structure with real geometry is reported. The model includes two composite facesheets, honeycomb core, piezoelectric actuator/sensors, adhesive layers, and the impactor. The novel feature of the model is that it includes modeling of the impact and wave propagation in the structure before and after the impact. Results of modeling of the wave propagation, impact, and damage detection in sandwich honeycomb plates using piezoelectric actuator/sensor scheme are reported. The results of the simulations are compared with the experimental results. It is shown that the model is suitable for analysis of the physics of failure due to the impact and for testing structural health monitoring schemes based on guided wave propagation.

AB - High-Fidelity Model of the sandwich composite structure with real geometry is reported. The model includes two composite facesheets, honeycomb core, piezoelectric actuator/sensors, adhesive layers, and the impactor. The novel feature of the model is that it includes modeling of the impact and wave propagation in the structure before and after the impact. Results of modeling of the wave propagation, impact, and damage detection in sandwich honeycomb plates using piezoelectric actuator/sensor scheme are reported. The results of the simulations are compared with the experimental results. It is shown that the model is suitable for analysis of the physics of failure due to the impact and for testing structural health monitoring schemes based on guided wave propagation.

U2 - 10.1109/AERO.2011.5747569

DO - 10.1109/AERO.2011.5747569

M3 - Conference contribution/Paper

AN - SCOPUS:79955749910

SN - 9781424473502

T3 - IEEE Aerospace Conference Proceedings

BT - 2011 Aerospace Conference, AERO 2011

PB - IEEE

T2 - 2011 IEEE Aerospace Conference, AERO 2011

Y2 - 5 March 2011 through 12 March 2011

ER -