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Output details

15 - General Engineering

University of Liverpool

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Output 18 of 103 in the submission

Article title

Computational Study of Helicopter Rotor-Fuselage Aerodynamic Interactions

Type

D - Journal article

DOI

10.2514/1.41287

Title of journal

AIAA Journal

Article number

Volume number

Issue number

First page of article

2143

ISSN of journal

1533-385X

Year of publication

2009

URL

Number of additional authors

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

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract