Aerodynamic study of a 'humpy' propeller

B. G. Marinus; W. Bosschaerts; M. Roger

doi:10.1504/IJESMS.2012.044841

Aerodynamic study of a 'humpy' propeller

B. G. Marinus, W. Bosschaerts, M. Roger

Ecole Centrale de Lyon

Onderzoeksoutput: Bijdrage aan een tijdschrift › Artikel › peer review

Samenvatting

A detailed aerodynamic study of a 'humpy' high-speed propeller is presented. This propeller is the result of a bi-disciplinary optimisation procedure and features blade segments of wider chord bordered by narrow segments. The aerodynamic consequences of these regions are investigated and correlated to the aeroacoustic properties by comparison to an equivalent blade without hump.

Originele taal-2	Engels
Pagina's (van-tot)	27-35
Aantal pagina's	9
Tijdschrift	International Journal of Engineering Systems Modelling and Simulation
Volume	4
Nummer van het tijdschrift	1-2
DOI's	https://doi.org/10.1504/IJESMS.2012.044841
Status	Gepubliceerd - jan. 2012

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10.1504/IJESMS.2012.044841

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title = "Aerodynamic study of a 'humpy' propeller",

abstract = "A detailed aerodynamic study of a 'humpy' high-speed propeller is presented. This propeller is the result of a bi-disciplinary optimisation procedure and features blade segments of wider chord bordered by narrow segments. The aerodynamic consequences of these regions are investigated and correlated to the aeroacoustic properties by comparison to an equivalent blade without hump.",

keywords = "Aeroacoustics, Aerodynamics, Chord, Propeller",

author = "Marinus, {B. G.} and W. Bosschaerts and M. Roger",

note = "Funding Information: The authors thank the financial support from the National Research Foundation (NRF), Prime Minister's Office, Singapore under its Campus for Research Excellence and Technological Enterprise (CREATE) program.",

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AU - Roger, M.

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AB - A detailed aerodynamic study of a 'humpy' high-speed propeller is presented. This propeller is the result of a bi-disciplinary optimisation procedure and features blade segments of wider chord bordered by narrow segments. The aerodynamic consequences of these regions are investigated and correlated to the aeroacoustic properties by comparison to an equivalent blade without hump.

KW - Aeroacoustics

KW - Aerodynamics

KW - Chord

KW - Propeller

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Aerodynamic study of a 'humpy' propeller

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