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....

Celý popis

Uloženo v:
Podrobná bibliografie
Hlavní autor: Evans, Rebecca L.
Korporace: Defence Science and Technology Organisation (Australia), Aeronautical and Maritime Research Laboratory (Australia)
Další autoři: Heller, Manfred
Médium: Kniha
Jazyk:English
Vydáno: Melbourne, Vic. : DSTO Aeronautical and Maritime Research Laboratory, 1996.
Edice:Technical report (Defence Science and Technology Organisation (Australia)) ; DSTO-TR-0409.
Témata:
Finite element method.
Strains and stresses.
Airframes.
Military research > Australia.
Materials > Research > Australia.
Plates (Engineering)
Adhesives.
On-line přístup: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

CARM 1 Store

Informace o exemplářích z: CARM 1 Store
Signatura: A1:AP32D0 F02143
Jednotka 1 Dostupné  Požadavek

Podobné jednotky