机译:Aeroelastic模型与Active Camber Morphing Wing的分析
Beihang Univ Sch Aeronaut Sci & Engn Beijing 100191 Peoples R China|Swansea Univ Coll Engn Swansea SA2 8PP W Glam Wales;
Swansea Univ Coll Engn Swansea SA2 8PP W Glam Wales;
Nanjing Univ Aeronaut & Astronaut Coll Aerosp Engn Nanjing 210016 Peoples R China;
Swansea Univ Coll Engn Swansea SA2 8PP W Glam Wales;
Univ Huddersfield Sch Comp & Engn Huddersfield HD1 3DH W Yorkshire England;
Swansea Univ Coll Engn Swansea SA2 8PP W Glam Wales;
Univ Bristol Dept Aerosp Engn Bristol BS8 1TR Avon England;
Morphing camber; Rigid-flexible structure; Flutter; Feedback control;