Active wing design with integrated flight control using piezoelectric macro fiber composites

Smart Materials and Structures

Volumn 18, Issue 3, 2009, Pages

  Paradies, Rolf ^a,b   Ciresa, Paolo ^a,c  

^a SWISS FEDERAL LABORATORIES FOR MATERIALS SCIENCE AND TECHNOLOGY   (Switzerland)

^b Prose AG   (Switzerland)

^c BOMBARDIER TRANSPORTATION   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE COMPOSITES; DESIGN MODELS; DYNAMIC TESTS; FLIGHT CONTROL; FLUID DYNAMICS MODEL; FULLY-COUPLED; MACRO FIBER COMPOSITE; NUMERICAL MODELS; PIEZOELECTRIC ELEMENTS; ROLL MOMENT; WING DESIGN;

DESIGN; FEATURE EXTRACTION; FLOW STRUCTURE; NUMERICAL METHODS; PIEZOELECTRIC ACTUATORS; PIEZOELECTRIC TRANSDUCERS; PIEZOELECTRICITY; REMOTELY OPERATED VEHICLES; TESTING; UNMANNED AERIAL VEHICLES (UAV);

WINGS;

EID: 68549121148     PISSN: 09641726     EISSN: 1361665X     Source Type: Journal    
DOI: 10.1088/0964-1726/18/3/035010     Document Type: Article

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