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Numerical characterization of helicopter noise hemispheres

  • Published:2016-05 Issue: Volume:52 Page:18-28
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Gennaretti M.ORCID,Serafini J.ORCID,Bernardini G.ORCID,Castorrini A.,De Matteis G.,Avanzini G.

Funder

CleanSky Joint Undertaking Programme

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference42 articles.

1. Reduction of helicopter blade–vortex interaction noise by active rotor control technology;Yu;Prog. Aerosp. Sci.,1997

2. Blade–vortex interaction noise reduction with active twist smart rotor technology;Chen;Smart Mater. Struct.,2001

3. Simultaneous vibration and noise reduction in rotorcraft using aeroelastic simulation;Patt;J. Am. Helicopter Soc.,2006

4. Blade–vortex interaction noise characteristics of a full-scale active flap rotor;JanakiRam,2009

5. The influence of winglets on rotor aerodynamics;Muller,1986

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