You are in : Home » Results & submissions » Select UOA » 12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering » View submission: Queen's University Belfast » Outputs » Detail

Output details

12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering

Queen's University Belfast

Return to search Previous output Next output

Output 29 of 143 in the submission

Article title

Buckling/post-buckling strength of friction stir welded aircraft stiffened panels

Type

D - Journal article

DOI

10.1177/0954410012468537

Title of journal

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Article number

Volume number

n/a

Issue number

n/a

First page of article

ISSN of journal

0954-4100

Year of publication

2012

URL

Number of additional authors

Additional information

The rigorous computational analysis represents the first publication of the quantified impact of friction stir welding on the static strength of large scale aircraft panel structure. The findings have led to further industrial collaboration, developing friction stir welding for wing panel assembly (Ken Poston, Head of Advanced Metallics: Strategic Technologies, Bombardier Aerospace).

Interdisciplinary

Cross-referral requested

Research group

None

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract