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Volumn 40, Issue 11, 2004, Pages 1283-1295
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Open-loop flutter analysis of a composite UAV model using the active stiffening effect
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Author keywords
Actuators; Flutter; Piezoelectric; Stiffening
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Indexed keywords
ACTUATORS;
ELECTRIC POTENTIAL;
FINITE ELEMENT METHOD;
FLUTTER (AERODYNAMICS);
LEAD COMPOUNDS;
PIEZOELECTRIC DEVICES;
STIFFNESS;
SURFACE TREATMENT;
VEHICLES;
OPEN-LOOP FLUTTER ANALYSIS;
PIEZOELECTRIC ACTUATORS;
STIFFENING;
LAMINATED COMPOSITES;
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EID: 2442566441
PISSN: 0168874X
EISSN: None
Source Type: Journal
DOI: 10.1016/j.finel.2003.06.004 Document Type: Article |
Times cited : (4)
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References (12)
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