Output details
15 - General Engineering
University of Liverpool
Article title
Framework for Establishing Limits of Tabular Aerodynamic Models for Flight Dynamics Analysis
Type
D - Journal article
Title of journal
Journal of Aircraft
Article number
-
Volume number
48
Issue number
1
First page of article
42
ISSN of journal
1533-3868
Year of publication
2011
URL
-
Number of additional authors
5
Additional information
A methodology was developed to define, by simulating aircraft manoeuvres in computational fluid dynamics, the limits of the widely used aerodynamic tabular model for flight dynamics analysis. The demonstration of the ability to build and test aircraft aerodynamic tabular models led to EPSRC funding for the investigation of aircraft flexibility on flight control (EP/I014594/1 - evidence file Badcock4-1.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
-
