Effect of bonded insert shape and adhesive thickness on critical stresses in a loaded plate /

Effect of bonded insert shape and adhesive thickness on critical stresses in a loaded plate /

This report presents the results of finite element analyses conducted to calculate the magnitude of adhesive stresses for a large plate with a bonded insert, and study the interaction of key parameters including (i) insert shape, and (ii) adhesive modulus and thickness, with maximum plate stresses....

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Bibliographic Details
Main Author: Evans, Rebecca L.
Corporate Authors: Defence Science and Technology Organisation (Australia), Aeronautical and Maritime Research Laboratory (Australia)
Other Authors: Heller, Manfred
Format: Book
Language:English
Published: Melbourne, Vic. : DSTO Aeronautical and Maritime Research Laboratory, 1996.
Series:Technical report (Defence Science and Technology Organisation (Australia)) ; DSTO-TR-0409.
Subjects:
Finite element method.
Strains and stresses.
Airframes.
Military research > Australia.
Materials > Research > Australia.
Plates (Engineering)
Adhesives.
Online Access:http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0409.pdf

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http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0409.pdf

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