Output details
15 - General Engineering
University of Liverpool
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Article title
Computational Study of Helicopter Rotor-Fuselage Aerodynamic Interactions
Type
D - Journal article
DOI
Title of journal
AIAA Journal
Article number
-
Volume number
47
Issue number
9
First page of article
2143
ISSN of journal
1533-385X
Year of publication
2009
URL
-
Number of additional authors
1
Additional information
Systematic computational study showed how the inner blade rotor aerodynamics is significantly influenced by the fuselage. The paper influenced the use of rotor-fuselage calculations for design within Agusta Westland (contact:James.Godman@agustawestland.com).
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
-