Numerical and experimental study of active flutter suppression with piezoelectric device for transonic cascade

Proceedings of the ASME Turbo Expo

Volumn 5, Issue PART B, 2008, Pages 849-859

  Watanabe, Toshinori ^a   Kazawa, Junichi ^a   Uzawa, Seiji ^b   Keim, Benjamin ^c  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c RWTH AACHEN UNIVERSITY   (Germany)

Author keywords

Active control; Aeroelasticity; Cascade flutter; Piezoelectric device; Smart structure

Indexed keywords

ACTIVE CONTROL; ACTIVE FLUTTER SUPPRESSION; AEROELASTICITY; BLADE OSCILLATIONS; BLADE VIBRATIONS; CASCADE FLUTTER; CONTROL METHODS; DESTABILIZATION EFFECTS; EXPERIMENTAL STUDIES; FLUTTER INSTABILITY; FLUTTER SUPPRESSION; LINEAR CASCADE; NUMERICAL AND EXPERIMENTAL STUDY; NUMERICAL STUDIES; OSCILLATORY BEHAVIORS; PASSAGE SHOCK; PHASE DIFFERENCE; REALISTIC APPLICATIONS; SMART STRUCTURE; STABILIZATION EFFECTS; TRAILING EDGES; UNSTEADY AERODYNAMIC FORCE;

CONTROL SYSTEM ANALYSIS; ELASTIC WAVES; ELASTICITY; PIEZOELECTRIC ACTUATORS; PIEZOELECTRIC TRANSDUCERS; PIEZOELECTRICITY; TRANSONIC FLOW; WIND TUNNELS;

FLUTTER (AERODYNAMICS);

EID: 69949177622     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2008-51467     Document Type: Conference Paper

References (9)

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