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

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Résumé

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.

langue originaleAnglais
titre18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
EditeurAmerican Institute of Aeronautics and Astronautics Inc
ISBN (imprimé)9781600869327
Les DOIs
étatPublié - 2012
Evénement18th AIAA/CEAS Aeroacoustics Conference 2012 (33rd AIAA Aeroacoustics Conference) - , États-Unis
Durée: 4 juin 20126 juin 2012

Série de publications

Nom18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)

Une conférence

Une conférence18th AIAA/CEAS Aeroacoustics Conference 2012 (33rd AIAA Aeroacoustics Conference)
Pays/TerritoireÉtats-Unis
période4/06/126/06/12

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