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Thermal preconditioning study for bolted tension joints in pultruded GRP plate

Research output: Contribution to Journal/Magazine › Journal article › peer-review

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Thermal preconditioning study for bolted tension joints in pultruded GRP plate. / Turvey, Geoffrey; Wang, Ping.
In: Composite Structures, Vol. 77, No. 4, 01.02.2007, p. 509-513.

Research output: Contribution to Journal/Magazine › Journal article › peer-review

Harvard

Turvey, G & Wang, P 2007, 'Thermal preconditioning study for bolted tension joints in pultruded GRP plate', Composite Structures, vol. 77, no. 4, pp. 509-513. https://doi.org/10.1016/j.compstruct.2005.08.023

APA

Turvey, G., & Wang, P. (2007). Thermal preconditioning study for bolted tension joints in pultruded GRP plate. Composite Structures, 77(4), 509-513. https://doi.org/10.1016/j.compstruct.2005.08.023

Vancouver

Turvey G, Wang P. Thermal preconditioning study for bolted tension joints in pultruded GRP plate. Composite Structures. 2007 Feb 1;77(4):509-513. Epub 2005 Oct 10. doi: 10.1016/j.compstruct.2005.08.023

Author

Turvey, Geoffrey ; Wang, Ping. / Thermal preconditioning study for bolted tension joints in pultruded GRP plate. In: Composite Structures. 2007 ; Vol. 77, No. 4. pp. 509-513.

Bibtex

@article{fad77b73ad374a5f8e1181eead44af2c,
title = "Thermal preconditioning study for bolted tension joints in pultruded GRP plate",
abstract = "Thermocouples have been used to monitor the time versus temperature rise response at the centre of four sizes of pultruded GRP plate used in bolted tension joints in order to demonstrate that all of the GRP plate is at the required temperature prior to testing the joints to failure. A simple one-dimensional finite element (FE) model has also been developed and used to predict time versus temperature rise response. The experimental and numerical results confirm that a thermal preconditioning period of 30 min duration is more than adequate for all of the pultruded GRP plates to achieve the actual test temperatures of 40, 60 and 80 °C.",
keywords = "Temperature, Pultrusions, GRP, Joints, Plates",
author = "Geoffrey Turvey and Ping Wang",
year = "2007",
month = feb,
day = "1",
doi = "10.1016/j.compstruct.2005.08.023",
language = "English",
volume = "77",
pages = "509--513",
journal = "Composite Structures",
issn = "0263-8223",
publisher = "Elsevier Ltd",
number = "4",

}

RIS

TY - JOUR

T1 - Thermal preconditioning study for bolted tension joints in pultruded GRP plate

AU - Turvey, Geoffrey

AU - Wang, Ping

PY - 2007/2/1

Y1 - 2007/2/1

N2 - Thermocouples have been used to monitor the time versus temperature rise response at the centre of four sizes of pultruded GRP plate used in bolted tension joints in order to demonstrate that all of the GRP plate is at the required temperature prior to testing the joints to failure. A simple one-dimensional finite element (FE) model has also been developed and used to predict time versus temperature rise response. The experimental and numerical results confirm that a thermal preconditioning period of 30 min duration is more than adequate for all of the pultruded GRP plates to achieve the actual test temperatures of 40, 60 and 80 °C.

AB - Thermocouples have been used to monitor the time versus temperature rise response at the centre of four sizes of pultruded GRP plate used in bolted tension joints in order to demonstrate that all of the GRP plate is at the required temperature prior to testing the joints to failure. A simple one-dimensional finite element (FE) model has also been developed and used to predict time versus temperature rise response. The experimental and numerical results confirm that a thermal preconditioning period of 30 min duration is more than adequate for all of the pultruded GRP plates to achieve the actual test temperatures of 40, 60 and 80 °C.

KW - Temperature

KW - Pultrusions

KW - GRP

KW - Joints

KW - Plates

U2 - 10.1016/j.compstruct.2005.08.023

DO - 10.1016/j.compstruct.2005.08.023

M3 - Journal article

VL - 77

SP - 509

EP - 513

JO - Composite Structures

JF - Composite Structures

SN - 0263-8223

IS - 4

ER -