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Volumn 3, Issue , 2004, Pages 2355-2366
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Impact of actuation concepts on morphing aircraft structures
a,b a,b a,b a,b a,b |
Author keywords
[No Author keywords available]
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Indexed keywords
INTEGRATED ACTUATION SYSTEM;
LOAD CAPACITY;
MORPHING AIRCRAFT STRUCTURES (MAS);
QUALITY FUNCTION DEPLOYMENT (QFD);
SPACE MISSIONS;
ACTUATORS;
AEROSPACE VEHICLES;
CONSTRAINT THEORY;
FLOW CONTROL;
FLUTTER (AERODYNAMICS);
OPTIMIZATION;
PIEZOELECTRIC MATERIALS;
QUALITY CONTROL;
STRUCTURAL DESIGN;
TORQUE CONTROL;
TRANSONIC AERODYNAMICS;
WIND TUNNELS;
AVIATION;
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EID: 16244379832
PISSN: 02734508
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (65)
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References (10)
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