Active control of panel flutter with piezoelectric transducers

Journal of Aircraft

Volumn 33, Issue 4, 1996, Pages 768-774

  Frampton, Kenneth D ^a,b   Clark, Robert L ^a,b   Dowell, Earl H ^a,b,c  

^a DUKE UNIVERSITY   (United States)

^b Dept of Mech Eng and Mat Science ^*

^c Aerospace Engineering Group

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMIC LOADS; AERODYNAMICS; APPROXIMATION THEORY; CONTROL SYSTEMS; DIGITAL FILTERS; FEEDBACK; FEEDBACK CONTROL; MATHEMATICAL MODELS; PIEZOELECTRIC TRANSDUCERS; POTENTIAL FLOW; STIFFNESS;

AERODYNAMIC MODELING; MASS EFFECT; RAYLEIGH-RITZ APPROACH;

FLUTTER (AERODYNAMICS);

EID: 0030193654     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.47013     Document Type: Article

References (16)

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