Comparative study of the effects of sweep and humps on high-speed propeller blades

Onderzoeksoutput: Hoofdstuk in Boek/Rapport/CongresprocedureConferentiebijdragepeer review

Samenvatting

Previous work on multidisciplinary optimization of high-speed propeller blades led to the emergence of humpy blades with or without sweep. The present paper is intended to deliver more insight in the potential benefits of such blades by means of a comparative study of four blade designs. These designs differ only in their respective chord distribution and tip sweep. Comparisons will be given in terms of aerodynamic and aeroacoustic performance for the four designs operating either in identical ow conditions, hence different load, or in similar thrust conditions, hence slightly different ow conditions due to adaptation of the blade angle.

Originele taal-2Engels
Titel18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
UitgeverijAmerican Institute of Aeronautics and Astronautics Inc
ISBN van geprinte versie9781600869327
DOI's
StatusGepubliceerd - 2012
Evenement18th AIAA/CEAS Aeroacoustics Conference 2012 (33rd AIAA Aeroacoustics Conference) - , Verenigde Staten van Amerika
Duur: 4 jun. 20126 jun. 2012

Publicatie series

Naam18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)

Congres

Congres18th AIAA/CEAS Aeroacoustics Conference 2012 (33rd AIAA Aeroacoustics Conference)
Land/RegioVerenigde Staten van Amerika
Periode4/06/126/06/12

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