On the importance of aerodynamic and structural geometrical nonlinearities in aeroelastic behavior of high-aspect-ratio wings

Author:

Patil M.J.,Hodges D.H.

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference12 articles.

1. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flow;Albano;AIAA Journal,1969

2. Hall, B., Preidikman, S., Mook, D.T., 1999. A time-domain simulation for evaluating smart wing concepts for reducing gust loads. 1999 ASME Mechanics and Materials Conference, Blacksburg, VA, USA.

3. A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams;Hodges;International Journal of Solids and Structures,1990

4. Kalman, T.P., Rodden, W.P., Giesing, J.P., 1969. Aerodynamic influence coefficients by the doublet lattice method for interfering nonplanar lifting surfaces oscillating in a subsonic flow. Technical Report DAC-67977, McDonnell Douglas Corporation.

5. Patil, M.J., 1999. Nonlinear aeroelastic analysis, flight dynamics, and control of a complete aircraft. Ph.D. Thesis, Georgia Institute of Technology, Atlanta, GA, USA.

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