Analysis and flexible structural modeling for oscillating wing utilizing aeroelasticity

Chinese Journal of Aeronautics

Volumn 21, Issue 5, 2008, Pages 402-410

  Shao, Ke ^a   Wu, Zhigang ^a   Yang, Chao ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Aeroelasticity; Analysis; Excite; Flexible structure; Modal characteristics; Oscillation wing

Indexed keywords

AERODYNAMICS; AEROELASTICITY; ELASTIC WAVES; FIXED WINGS; FLEXIBLE STRUCTURES; FLUTTER (AERODYNAMICS); FREQUENCY RESPONSE; INTEGRAL EQUATIONS; STRUCTURAL DESIGN;

AERODYNAMIC FORCES; ANALYSIS; ANALYTICAL RESULTS; EXCITE; FREQUENCY RESPONSE ANALYSIS; MODAL CHARACTERISTICS; STRUCTURAL MODELING; UNSTEADY AERODYNAMICS;

FLEXIBLE WINGS;

EID: 55549141161     PISSN: 10009361     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1000-9361(08)60052-7     Document Type: Article

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