相关期刊:《Plasma Science and Technology》《Frontiers of Information Technology & Electronic Engineering》《Acta Mathematica Sinica,English Series》《Chemical Research in Chinese Universities》更多>>
National Natural Science Foundation of China(Nos.11172025,91116005);Research Fund for the Doctoral Program of Higher Education of China(No.20091102110015)
A rapid and efficient method for static aeroelastic analysis of a flexible slender wing when considering the structural geometric nonlinearity has been developed in this paper. A non-planar vortex lattice method herei...