A New Approach for Aeroelastic Robust Stability Analysis
robust stability、unsteady aerodynamic、perturbation method、stability analysis、computational time、numerical results、fuel consumption、singular value
21
V21;TV1
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6页
417-422