论文信息 - Nonlinear flutter characteristics of composite missile wing in transonic/low-supersonic flows - 字舞流文

Nonlinear flutter characteristics of composite missile wing in transonic/low-supersonic flows

This work was supported through funding from the Korea Ministry of Science and Technology. The authors acknowledge the support (Subject 2000-N-NL-01-C-250) of the National Research Laboratory Program.

In Lee | Dong-Hyun Kim

[1] L. Librescu,et al. Nonclassical effects on divergence and flutter of anisotropic swept aircraft wings , 1996 .

[2] Pong-Jeu Lu,et al. Flutter analysis of cantilever composite plates in subsonic flow , 1989 .

[3] In Lee,et al. Transonic and supersonic flutter characteristics of a wing-box model with tip stores , 2001 .

[4] T. Weisshaar. Aeroelastic Tailoring of Forward Swept Composite Wings , 1981 .

[5] V. B. Venkayya,et al. Aeroelastic Tailoring of Composite Structures , 1999 .

[6] I Lee,et al. Transonic Steady And Unsteady Aerodynamics For Wings Using Three Dimensional Euler Equations , 2001 .

[7] I. Lottati,et al. Flutter and divergence aeroelastic characteristics for composite forward swept cantilevered wing , 1985 .