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Strength Prediction of Adhesively Bonded Single Lap Joints with the eXtended Finite Element Method

Völkerink, Oliver und Kosmann, Jens und Schollerer, Martin und Holzhüter, Dirk und Hühne, Christian (2018) Strength Prediction of Adhesively Bonded Single Lap Joints with the eXtended Finite Element Method. Publindústria, Produção de Comunicação, Lda.. 12th European Adhesion Conference and 4th Luso-Brazilian conference on Adhesion and Adhesives, 2018-09-05 - 2018-09-07, Lissabon, Portugal. ISBN 978-989-8927-24-8.

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Kurzfassung

Because of the planar load introduction, its high strength over weight ratio, the avoidance of holes, corrosion resistance and component reduction, adhesively bonded joints attract increasing attention in the field of lightweight construction. Nonetheless, a reliable prediction of the joints’ behaviour in terms of stress and strength is still a tremendous challenge. In this study the eXtended Finite Element Method (XFEM) in combination with cohesive behaviour is used to model crack growth under quasi-static loading. The objective of this work is to study the influence of different continuum mechanical material models for the adhesive like the von Mises, linear and exponent Drucker-Prager model on XFEM strength predictions. It will be evaluated whether the strength prediction of joints mainly loaded in shear is more accurate with a high sophisticated material model. Therefore, strength predictions of Single Lap Joints (SLJ) with thick aluminium adherends according to ASTM D 5656 are performed. With the help of this example, the chosen continuum mechanics material models for the film adhesive are compared. The material parameters for the adhesive are derived from a number of specimen types with different load combinations. Herein, digital image correlation (DIC) data recorded during experimental tests are used to assess the material models in combination with the derived material parameters. Furthermore, with the experimental results the performed strength predictions are evaluated. In addition, a mesh convergence study for the adhesive bondline with regard to the predicted strength is carried out. It could be revealed that XFEM in combination with a suitable yield criterion and appropriate material parameters is a valid technique for the strength prediction of lap shear joints since the variance to the experiments is less than 1 %.

elib-URL des Eintrags:https://elib.dlr.de/121643/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Strength Prediction of Adhesively Bonded Single Lap Joints with the eXtended Finite Element Method
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Völkerink, Oliveroliver.voelkerink (at) dlr.dehttps://orcid.org/0000-0002-9589-1963NICHT SPEZIFIZIERT
Kosmann, JensJens.Kosmann (at) dlr.dehttps://orcid.org/0000-0002-2225-4832NICHT SPEZIFIZIERT
Schollerer, MartinMartin.Schollerer (at) dlr.dehttps://orcid.org/0000-0001-7015-9461NICHT SPEZIFIZIERT
Holzhüter, Dirkdirk.holzhueter (at) dlr.dehttps://orcid.org/0000-0003-1001-2366NICHT SPEZIFIZIERT
Hühne, ChristianChristian.Huehne (at) dlr.dehttps://orcid.org/0000-0002-2218-1223NICHT SPEZIFIZIERT
Datum:5 September 2018
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Seitenbereich:Seite 86
Herausgeber:
HerausgeberInstitution und/oder E-Mail-Adresse der HerausgeberHerausgeber-ORCID-iDORCID Put Code
da Silva, Lucas F. M.lucas (at) fe.up.ptNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Verlag:Publindústria, Produção de Comunicação, Lda.
ISBN:978-989-8927-24-8
Status:veröffentlicht
Stichwörter:XFEM, DIC, adhesive bonding, SLJ, single lap joint, strength prediction, FEM, Drucker-Prager, film adhesive, EA9695
Veranstaltungstitel:12th European Adhesion Conference and 4th Luso-Brazilian conference on Adhesion and Adhesives
Veranstaltungsort:Lissabon, Portugal
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:5 September 2018
Veranstaltungsende:7 September 2018
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Flugzeuge
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Aircraft Research
DLR - Teilgebiet (Projekt, Vorhaben):L - Simulation und Validierung (alt), L - Strukturen und Werkstoffe (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Faserverbundleichtbau und Adaptronik > Funktionsleichtbau
Hinterlegt von: Völkerink, Dr. Oliver
Hinterlegt am:13 Dez 2018 06:08
Letzte Änderung:24 Apr 2024 20:25

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