Aeroelastic modeling of active twist rotorblades using particle-wake aerodynamics and non-linear beam structural dynamics

ASME International Mechanical Engineering Congress and Exposition, Proceedings

Volumn , Issue , 2002, Pages 25-37

  Opoku, Daniel G ^a   Nitzsche, Fred ^a   Cheng, Tao ^b   Cesnik, Carlos E S ^c  

^a CARLETON UNIVERSITY   (Canada)

^b Massachusetts Institute of Technology Cambridge   (United States)

^c The Department of Civil and Environmental Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; AERODYNAMICS; MECHANICAL ENGINEERING; STRUCTURAL DYNAMICS; TECHNICAL PRESENTATIONS; WAKES;

ACOUSTIC COMPONENTS; ACTIVE TWIST; ACTIVE TWIST ROTOR; AEROACOUSTIC ANALYSIS; AEROELASTIC COUPLING; AEROELASTIC MODELING; BEAM ELEMENTS; FFOWCS WILLIAMS-HAWKINGS EQUATION; MIXED VARIATIONAL; MODEL SCALE; NON-LINEAR; NON-LINEAR BEAMS; PANEL METHODS; STRUCTURAL COMPONENT; VIBRATION STUDIES;

AEROELASTICITY;

EID: 78249287526     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/IMECE2002-32961     Document Type: Conference Paper

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