NUMERICAL STUDY ON MORPHING INFLATABLE WING ACTUATED BY PNEUMATIC CELLS

摘要：

An inflated morphing wing actuated by pneumatic cells (muscles) is modeled using finite element method and its deformations with different actuation pressures are calculated.The aerodynamics performance of the morphed wing is simulated using computational fluid dynamics software.The results show that deflection of morphing wing increases the angle of attack,and it is found that the lift coefficient of the morphing wing is larger than that of the original wing in the same angle of attack as produced by wing morphing.

关键词： morphing wing inflated wing pneumatic muscle

作者: Z.F.Yu

作者单位: Institute of Aerospace Science & Technology Shanghai Jiao Tong University,Shanghai,200240,China

会议类型: 国际会议

会议名称: 第二届国际非均质材料力学会议(The Second International Conference on Heterogeneous Material Mechanics)

会议地点: 安徽黄山

会议语种:英文

页码: 1502-1505

在线出版日期: 2008-06-03（万方平台首次上网日期，不代表论文的发表时间）