Nonlinear aeroelastic analysis of a two-dimensional wing with control surface in supersonic flow
supersonic flow、control、chaotic response、nonlinear oscillation、harmonic excitation、the energy method、dynamic behaviors、analysis、two dimensional、limit cycle、method of、direction、range of、theory、simple、means、Based、main、idea
26
O3(力学)
2010-12-08(万方平台首次上网日期,不代表论文的发表时间)
401-407