Multi-site delamination analysis using virtual crack closure technique for a composite aircraft wing flap

Research output: Chapter in Book/Report/Conference proceedingConference contributionScientificpeer-review

Standard

Multi-site delamination analysis using virtual crack closure technique for a composite aircraft wing flap. / Jokinen, Jarno; Kanerva, Mikko; Saarela, Olli.

31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. ICAS, International Council of the Aeronautical Sciences, 2018.

Research output: Chapter in Book/Report/Conference proceedingConference contributionScientificpeer-review

Harvard

Jokinen, J, Kanerva, M & Saarela, O 2018, Multi-site delamination analysis using virtual crack closure technique for a composite aircraft wing flap. in 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. ICAS, International Council of the Aeronautical Sciences, International Council Of The Aeronautical Sciences Congress, Belo Horizonte, Brazil, 09/09/2018.

APA

Jokinen, J., Kanerva, M., & Saarela, O. (2018). Multi-site delamination analysis using virtual crack closure technique for a composite aircraft wing flap. In 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018 ICAS, International Council of the Aeronautical Sciences.

Vancouver

Jokinen J, Kanerva M, Saarela O. Multi-site delamination analysis using virtual crack closure technique for a composite aircraft wing flap. In 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. ICAS, International Council of the Aeronautical Sciences. 2018

Author

Jokinen, Jarno ; Kanerva, Mikko ; Saarela, Olli. / Multi-site delamination analysis using virtual crack closure technique for a composite aircraft wing flap. 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. ICAS, International Council of the Aeronautical Sciences, 2018.

Bibtex - Download

@inproceedings{114144a920054af29dad6163e17c4a14,
title = "Multi-site delamination analysis using virtual crack closure technique for a composite aircraft wing flap",
abstract = "In this study, we investigate the application of virtual crack closure technique (VCCT) for a multi-site delamination damage in the F-18 Hornet fighter aircraft's wing flap. The work focuses on the interaction between multiple delamination sites at different ply interfaces. The effects of numerical analysis parameters, such as energy release rate tolerance, on the criticality of the delamination and on the delamination growth are also studied.",
keywords = "Fighter aircraft, Finite element analysis, Flap, Multi-site damage",
author = "Jarno Jokinen and Mikko Kanerva and Olli Saarela",
year = "2018",
month = "1",
day = "1",
language = "English",
booktitle = "31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018",
publisher = "ICAS, International Council of the Aeronautical Sciences",

}

RIS - Download

TY - GEN

T1 - Multi-site delamination analysis using virtual crack closure technique for a composite aircraft wing flap

AU - Jokinen, Jarno

AU - Kanerva, Mikko

AU - Saarela, Olli

PY - 2018/1/1

Y1 - 2018/1/1

N2 - In this study, we investigate the application of virtual crack closure technique (VCCT) for a multi-site delamination damage in the F-18 Hornet fighter aircraft's wing flap. The work focuses on the interaction between multiple delamination sites at different ply interfaces. The effects of numerical analysis parameters, such as energy release rate tolerance, on the criticality of the delamination and on the delamination growth are also studied.

AB - In this study, we investigate the application of virtual crack closure technique (VCCT) for a multi-site delamination damage in the F-18 Hornet fighter aircraft's wing flap. The work focuses on the interaction between multiple delamination sites at different ply interfaces. The effects of numerical analysis parameters, such as energy release rate tolerance, on the criticality of the delamination and on the delamination growth are also studied.

KW - Fighter aircraft

KW - Finite element analysis

KW - Flap

KW - Multi-site damage

UR - http://www.scopus.com/inward/record.url?scp=85060455628&partnerID=8YFLogxK

M3 - Conference contribution

BT - 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018

PB - ICAS, International Council of the Aeronautical Sciences

ER -

ID: 31626820