Damage identification in composite panels using guided waves

R. Loendersloot; M. Moix-Bonet

Damage identification in composite panels using guided waves

R. Loendersloot, M. Moix-Bonet

Faculty of Engineering Technology

Research output: Contribution to conference › Paper › peer-review

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Abstract

A methodology for the identification of barely visible impact damage using guided waves on a typical aircraft composite structure is implemented. Delaminations and debondings have been introduced in two stiffened panels by means of impact loads.

Original language	English
Pages	1-14
Publication status	Published - 7 Sept 2015
Event	5th CEAS Air & Space Conference 2015: Challenges in European Aerospace - Delft, Netherlands Duration: 7 Sept 2015 → 11 Sept 2015 Conference number: 5

Conference

Conference	5th CEAS Air & Space Conference 2015
Country/Territory	Netherlands
City	Delft
Period	7/09/15 → 11/09/15

Keywords

IR-97412
METIS-308627

Access to Document

CEAS2015_197

Cite this

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title = "Damage identification in composite panels using guided waves",

abstract = "A methodology for the identification of barely visible impact damage using guided waves on a typical aircraft composite structure is implemented. Delaminations and debondings have been introduced in two stiffened panels by means of impact loads.",

keywords = "IR-97412, METIS-308627",

author = "R. Loendersloot and M. Moix-Bonet",

note = "CEAS 2015 paper no. 197; 5th CEAS Air & Space Conference 2015 : Challenges in European Aerospace ; Conference date: 07-09-2015 Through 11-09-2015",

year = "2015",

month = sep,

day = "7",

language = "English",

pages = "1--14",

}

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AU - Loendersloot, R.

AU - Moix-Bonet, M.

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N2 - A methodology for the identification of barely visible impact damage using guided waves on a typical aircraft composite structure is implemented. Delaminations and debondings have been introduced in two stiffened panels by means of impact loads.

AB - A methodology for the identification of barely visible impact damage using guided waves on a typical aircraft composite structure is implemented. Delaminations and debondings have been introduced in two stiffened panels by means of impact loads.

KW - IR-97412

KW - METIS-308627

M3 - Paper

SP - 1

EP - 14

T2 - 5th CEAS Air & Space Conference 2015

Y2 - 7 September 2015 through 11 September 2015

ER -