Static aeroelastic analysis of very flexible wings based on non-planar vortex lattice method-Reference-Cited by-同舟云学术

Static aeroelastic analysis of very flexible wings based on non-planar vortex lattice method

Published:2013-06 Issue:3 Volume:26 Page:514-521
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Xie Changchuan,Wang Libo,Yang Chao,Liu Yi

Funder

National Natural Science Foundation of China

Research Fund for the Doctoral Program of Higher Education of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference17 articles.

1. Patil MJ, Hodges DH. On the importance of aerodynamic and structural nonlinearities in aeroelastic behavior of high-aspect-ratio wings. AIAA-2000-1448; 2000.

2. Patil MJ, Hodges DH, Cesnik CES. Limit cycle oscillations in high-aspect-ratio wings. AIAA-1999-1464; 1999.

3. Patil MJ, Hodges DH, Cesnik CES. Characterizing the effects of geometrical nonlinearities on aeroelastic behavior of high-aspect-ratio wings. Williamsburg: International Forum on Aeroelasticity and Structural Dynamics; 1999.

4. Zhang J. Modeling and simulation of coupled nonlinear aeroelasticity and flight dynamics for flexible aircraft [dissertation]. Beijing: Beihang University, 2010 [Chinese].

5. Tang DM, Dowell EH. Comments on the ONERA stall aerodynamic model and its impact on aeroelastic stability. Journal of Fluid and Structure 1996; 10(4): 353-66.

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