Open Access

ARTICLE

Aeroelasticity analysis of folding wing with structural nonlinearity using modified DLM

Yingge Ni¹, Peicheng Li², Hui Zhao¹, Shengjun Qiao¹

1 School of Aircraft Engineering, Xi’an Aeronautical University, China
2 School of Aeronautics, Northwestern Polytechnical University, China

* Corresponding Author: Yingge Ni ()