An adaptive wing for a small-aircraft application with a configuration of fibre Bragg grating sensors

Smart Materials and Structures

Volumn 19, Issue 8, 2010, Pages

  Mieloszyk, M ^a   Krawczuk, M ^a,b   Zak, A ^a   Ostachowicz, W ^a,c  

^a INSTITUTE OF FLUID FLOW MACHINERY   (Poland)

^b GDANSK UNIVERSITY OF TECHNOLOGY   (Poland)

^c GDYNIA MARITIME UNIVERSITY   (Poland)

Author keywords

[No Author keywords available]

Indexed keywords

ABAQUS; AIRCRAFT; ELECTRIC SENSING DEVICES; FIBER BRAGG GRATINGS; FINITE ELEMENT METHOD; SHAPE-MEMORY ALLOY;

ADAPTIVE WING; CONTROL STRATEGIES; FIBRE BRAGG GRATING SENSORS; FINITE ELEMENT PACKAGES; NUMERICAL CALCULATION; SHAPE MEMORY ALLOY ACTUATORS; SMALL AIRCRAFT; TWISTING ANGLE;

WINGS;

EID: 85062822350     PISSN: 09641726     EISSN: 1361665X     Source Type: Journal    
DOI: 10.1088/0964-1726/19/8/085009     Document Type: Article

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