论文信息 - Nonlinearc Aeroelastic Analysis of an Airfoil Using CFD-Based Indicial Approach - 字舞流文

Nonlinearc Aeroelastic Analysis of an Airfoil Using CFD-Based Indicial Approach

Thisworkwas partially supported byKorea Research Foundation Grant (KRF-2004-003-D00067). Dong-Hyun Kim would like to acknowledge the support.

In Lee | Liviu Librescu | Dong-Hyun Kim | Piergiovanni Marzocca | Stephen Schober

[1] In Lee,et al. TRANSONIC AND LOW-SUPERSONIC AEROELASTIC ANALYSIS OF A TWO-DEGREE-OF-FREEDOM AIRFOIL WITH A FREEPLAY NON-LINEARITY , 2000 .

[2] Liviu Librescu,et al. Aeroelastic Response of Swept Aircraft Wings in a Compressible Flow Field , 2001 .

[3] Patrick Reisenthel,et al. Development of a nonlinear indicial model for maneuvering fighter aircraft , 1996 .

[4] Liviu Librescu,et al. Aeroelastic response of 2-D lifting surfaces to gust and arbitrary explosive loading signatures , 2001 .

[5] Liviu Librescu,et al. Aeroelastic response of a 2-D airfoil in a compressible flow field and exposed to blast loading , 2002 .

[6] In Lee,et al. Linear/nonlinear unsteady aerodynamic modeling of 2-D lifting surfaces via a combined CFD/analytical approach , 2003 .

[7] Oh Joon Kwon,et al. Nonlinear Aeroelastic Computations of a Wing/Pylon/Finned-Store Using Parallel Computing , 2005 .