Output details
15 - General Engineering
University of Liverpool
Article title
Bifurcation Prediction of Large-Order Aeroelastic Models
Type
D - Journal article
DOI
Title of journal
AIAA Journal
Article number
-
Volume number
48
Issue number
6
First page of article
1037
ISSN of journal
1533-385X
Year of publication
2010
URL
-
Number of additional authors
1
Additional information
A method was developed to enable transonic aeroelastic stability prediction using very large dimension models derived from computational fluid dynamics. The method was subsequently successfully demonstrated for the analysis of an Airbus in-production aircraft with 250 million degrees of freedom, and this work is being industrialised under the TSB funded Conga project, as described in a statement from Tom Wilson from Airbus (contact Thomas.Wilson@Airbus.com; evidence file Badcock1-1.pdf).
Interdisciplinary
-
Cross-referral requested
-
Research group
None
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
