Experimental Exploration of Macro-fiber Composite Morphing Wing

摘要

In this paper, a experimental model of morphing swept-wing with carbon fiber is designed and driven by Macro-Fiber Composites (MFC). Dynamic analysis of the wing structure is carried out. The maximum twist angle of the carbon fiber structure driven by the MFC in the experiment is 10.72°. External excitation can be applied to the wing structure for its dynamic analysis and the modal performance of the structure is analyzed.