Analysis and Flexible Structural Modeling for Oscillating Wing Utilizing Aeroelasticity
unsteady aerodynamic、range of application、flexible structures、frequency response、analytical method、aerodynamic force、kinetic equation、wing aircraft、time response
21
V21;TU5
National Natural Science Foundation of China 10432040,90716006
2009-02-16(万方平台首次上网日期,不代表论文的发表时间)
共9页
402-410