Effect of plate thickness on the in-plane and through-thickness stresses at a hole /

Effect of plate thickness on the in-plane and through-thickness stresses at a hole /

Holes exist in metallic aircraft structures for either design or construction reasons and their stress concentrating effect is such that they are common regions of fatigue crack initiation. A combined experimental and numerical study has been carried out to examine the influence of thickness on the...

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Bibliographische Detailangaben
1. Verfasser: Evans, R. L.
Körperschaften: Defence Science and Technology Organisation (Australia), Aeronautical and Maritime Research Laboratory (Australia)
Format: Buch
Sprache:English
Veröffentlicht: Melbourne : DSTO Aeronautical and Maritime Research Laboratory, 1996.
Schriftenreihe:Technical report (Defence Science and Technology Organisation (Australia)) ; DSTO-TR-0330.
Schlagworte:
Strains and stresses > Mathematical models.
Finite element method.
Aluminum alloys.
Aluminium alloys > Fatigue.
Aluminium alloys > Stress corrosion.
Holes.
Online Zugang:http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0330.pdf

Online

http://www.dsto.defence.gov.au/corporate/reports/DSTO-TR-0330.pdf

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