Output details

12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering

Output 37 of 635 in the submission

Article title

A moderate deflection composite helicopter rotor blade model with an improved cross-sectional analysis

Type

D - Journal article

DOI

Title of journal

International Journal of Solids and Structures

Article number

Volume number

Issue number

First page of article

2186

ISSN of journal

0020-7683

Year of publication

2009

URL

Number of additional authors

Additional information

Interdisciplinary

Cross-referral requested

Research group

A - Aeronautics

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract