Design and control of a morphing chevron for takeoff and cruise noise reduction

Collection of Technical Papers - 11th AIAA/CEAS Aeroacoustics Conference

Volumn 2, Issue , 2005, Pages 1174-1188

  Mabe, James H ^a,c   Cabell, Randolph H ^b   Butler, G W ^a  

^a BOEING COMPANY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMICS; AIR; CONTROL SYSTEMS; NICKEL ALLOYS; NOZZLES; SHAPE MEMORY EFFECT; TITANIUM ALLOYS; TURBOFAN ENGINES;

AMBIENT AIR; CHEVRONS; SERRATED AERODYNAMIC DEVICES;

NOISE ABATEMENT;

EID: 29244480353     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2889     Document Type: Conference Paper

References (12)

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