Output details
15 - General Engineering
University of Liverpool
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Article title
Transonic Aeroelastic Instability Searches Using Sampling and Aerodynamic Model Hierarchy
Type
D - Journal article
Title of journal
AIAA Journal
Article number
-
Volume number
49
Issue number
6
First page of article
1191
ISSN of journal
1533-385X
Year of publication
2011
URL
-
Number of additional authors
1
Additional information
Sampling and approximation methods are developed to allow a transonic aeroelastic stability boundary to be rapidly generated using a coordinated search of a hierarchy of aerodynamic models of increasing complexity and computational cost. The method has been implemented into the production release of the German Aerospace center computational fluid dynamics code TAU which is used as a principle design tool by Airbus (markus.widhalm@dlr.de evidence file Timme1-1.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
-
