Effects of blade aspect ratio and taper ratio on hovering performance of cycloidal rotor with large blade pitching amplitude

In recent years, a lot of research work has been carried out on the cycloidal rotors. However, it lacks thorough understanding about the effects of the blade platform shape on the hover efficiency of the cycloidal rotor, and the knowledge of how to design the platform shape of the blades. This paper...

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Bibliographic details
Volume: 32
Main Author: HU, Yu
FU, Xuyang
ZHANG, Hailang
WANG, Gengqi
FARHAT, Hussain
Format: Journal Article
Language: English
Place of publication: NEW YORK Elsevier Ltd 01.05.2019
published in: Chinese journal of aeronautics Vol. 32; no. 5; pp. 1121 - 1135
ORCID: 0000-0003-2739-3492
Data of publication: May 2019
ISSN: 1000-9361
Discipline: Engineering
Online Access: Fulltext
Database: Elsevier:ScienceDirect:Open Access
ScienceDirect Open Access Titles
Web of Science - Science Citation Index Expanded - 2019
Web of Knowledge
Science Citation Index Expanded
Web of Science
DOAJ Directory of Open Access Journals - Not for CDI Discovery
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