Airfoil structural morphing based on S.M.A. actuator series: Numerical and experimental studies

Journal of Intelligent Material Systems and Structures

Volumn 22, Issue 10, 2011, Pages 987-1004

  Barbarino, S ^a   Pecora, R ^a   Lecce, L ^a   Concilio, A ^b   Ameduri, S ^b   De Rosa, L ^c  

^a UNIVERSITY OF NAPLES FEDERICO II   (Italy)

^b ITALIAN AEROSPACE RESEARCH CENTER   (Italy)

^c ALENIA SPAZIO   (Italy)

Author keywords

actuator.; hingeless flap; morphing; SMA; smart structures

Indexed keywords

ACTUATION CAPABILITY; AERODYNAMIC EFFICIENCY; DISCRETE COMPONENTS; EXTERNAL LOADS; FLIGHT REGIME; FULL SCALE; HINGELESS FLAP; MORPHING; NUMERICAL AND EXPERIMENTAL STUDY; OPTIMIZED CONFIGURATION; REGIONAL TRANSPORTATION; SHAPE MEMORY ALLOY; SMA; STATIC LOADS; STRUCTURAL ELEMENTS; STRUCTURAL INTEGRATION; VORTEX LATTICE METHOD; WING MORPHING; WING TRAILING EDGE;

AERODYNAMIC CONFIGURATIONS; AIRCRAFT; AIRFOILS; COMPUTER SIMULATION; FLEXIBLE WINGS; OPTIMIZATION; THERMOMECHANICAL TREATMENT; VORTEX FLOW;

ACTUATORS;

EID: 80052755580     PISSN: 1045389X     EISSN: 15308138     Source Type: Journal    
DOI: 10.1177/1045389X11416032     Document Type: Article

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