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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Detaylı Bibliyografya
Yazar: Evans, Rebecca L.
Kurumsal yazarlar: Defence Science and Technology Organisation (Australia), Aeronautical and Maritime Research Laboratory (Australia)
Diğer Yazarlar: Heller, Manfred
Materyal Türü: Kitap
Dil:English
Baskı/Yayın Bilgisi: Melbourne, Vic. : DSTO Aeronautical and Maritime Research Laboratory, 1996.
Seri Bilgileri:Technical report (Defence Science and Technology Organisation (Australia)) ; DSTO-TR-0409.
Konular:
Finite element method.
Strains and stresses.
Airframes.
Military research > Australia.
Materials > Research > Australia.
Plates (Engineering)
Adhesives.
Online Erişim:http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0409.pdf

Internet

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

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