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35th European Rotorcraft Forum 2009, ERF 2009

Volumn 1, Issue , 2009, Pages 551-563

Improvement of noise reduction and performance for a helicopter model rotor blade by active twist actuation

(2) Bailly, Joëlle a Delrieux, Yves a,b

a ONERA (France)

b Numerical Simulations and Acoustics Department (France)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE FLAPS; ACTIVE TWIST; BLADE TIP; BVI NOISE; DRAG MODEL; ELASTIC RESPONSE; EUROPEAN PROJECT; FLIGHT CONFIGURATIONS; GEOMETRY MODEL; HELICOPTER MODEL; INCIDENCE ANGLES; NOISE LEVELS; NOISE REDUCTIONS; POWER CONSUMPTION; POWER REDUCTIONS; PROFILE POWER; ROTOR BLADES; VORTEX LATTICES; WORK PACKAGES;

AIRCRAFT; OPTIMIZATION;

HELICOPTER ROTORS;

EID: 77952373141 PISSN: None EISSN: None Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper

Times cited : (5)

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