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Volumn 3, Issue , 2006, Pages 2189-2193
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Investigation of the effect of deformable trailing edge geometry control systems on flutter velocity
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Author keywords
Aeroservoelasticity; Control; Stability
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Indexed keywords
FATIGUE LOAD REDUCTION;
FLUTTER VELOCITIES;
PD CONTROL;
TIME LAG;
TRAILING EDGE GEOMETRIES;
WIND-TUNNEL TESTING;
AEROSERVOELASTICITY;
CONTROL;
CONVERGENCE OF NUMERICAL METHODS;
DEFORMATION;
EXHIBITIONS;
FLUTTER (AERODYNAMICS);
THREE DIMENSIONAL COMPUTER GRAPHICS;
WIND POWER;
CONTROL SYSTEMS;
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EID: 84876546478
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (5)
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References (9)
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