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Dynamic intralaminar fracture toughness of carbon/epoxy composites at intermediate strain rates using size effect

Yoo, Sanghyun und Catalanotti, Giuseppe und Dalli, Denis und Toso, Nathalie und Toso, Yves und Voggenreiter, Heinz (2019) Dynamic intralaminar fracture toughness of carbon/epoxy composites at intermediate strain rates using size effect. 1st European Conference on Crashworthiness of Composite Structures, 2019-11-19 - 2019-11-21, Belfast, UK.

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Kurzfassung

The design of composite transportation structures with improved crashworthiness behaviour requires a reliable and accurate dynamic material characterisation database covering various loading rates expected in crash events. For vehicle crash scenarios experimental results at strain rates up to 200 s-1 are particularly important. However, conducting dynamic testing at those strain rates with a high speed servo-hydraulic testing machine remains a challenge due to intrinsic aspects associated with inertia effect and stress wave propagation. The inertial effect known as system ringing is one of the major obstacles to obtain the true dynamic properties at intermediate strain rates, which results in unacceptable oscillations in load signals. Conducting compact tension (CT) tests is a typically first choice when measuring the intralaminar fracture toughness for fibre tensile failure. However, the CT specimens have several limitations when those used under dynamic loading rates. For example, inertial effects cause unsymmetrical opening of the CT specimens, which induce mixed mode fracture in the specimen. To overcome this limitation, G. Catalanotti proposed a new procedure using size effect law to measure the intralaminar fracture toughness for fibre tensile failure using double-edge notched tension (DENT) specimens. The tests using DENT specimens were successfully conducted under quasi-static loading and at loading strain rate of 60-1 using the split Hopkinson Tension Bar (SHTB) technique. This paper reports an experimental investigation on dynamic fracture toughness of IM7/8552 carbon/epoxy composites at intermediate strain rates. Dynamic tensile testing with three different sizes of DENT specimens is performed at the strain rates of 60 and 100 s-1 using a high-speed hydraulic testing machine. To that aim an improved load introduction device is used to handle the inertial effect during the testing. Obtained results from current work are then compared to previous results gained with SHTB technique. These results provide the competence of the proposed testing method to measure dynamic fracture toughness. This study is a first step towards the establishment of a reliable test method for measuring dynamic fracture toughness at intermediate strain rates.

elib-URL des Eintrags:https://elib.dlr.de/139141/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Dynamic intralaminar fracture toughness of carbon/epoxy composites at intermediate strain rates using size effect
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Yoo, SanghyunSanghyun.Yoo (at) dlr.dehttps://orcid.org/0000-0001-6924-1716NICHT SPEZIFIZIERT
Catalanotti, Giuseppeg.catalanotti (at) qub.ac.ukNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Dalli, Denisddalli01 (at) qub.ac.ukNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Toso, NathalieNathalie.Toso (at) dlr.dehttps://orcid.org/0000-0003-2803-1450NICHT SPEZIFIZIERT
Toso, YvesYves.Toso (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Voggenreiter, HeinzHeinz.Voggenreiter (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:November 2019
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Test method, Intermediate strain rates; Size effects; Intralaminar fracture toughness
Veranstaltungstitel:1st European Conference on Crashworthiness of Composite Structures
Veranstaltungsort:Belfast, UK
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:19 November 2019
Veranstaltungsende:21 November 2019
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 - Strukturen und Werkstoffe (alt)
Standort: Stuttgart
Institute & Einrichtungen:Institut für Bauweisen und Strukturtechnologie
Hinterlegt von: Yoo, Sanghyun
Hinterlegt am:08 Dez 2020 15:00
Letzte Änderung:24 Apr 2024 20:40

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