Nonlinear Aeroelastic Analysis of Joined-Wing Aircraft
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1487
Reference12 articles.
1. Weisshaar, T. and Lee, D. “Aeroelastic Tailoring of Joined-Wing Configurations,” Proceedings of the 43rd Structures, Structural Dynamics and Materials Conference, Denver, Colorado, April 2002, AIAA-2002-1207.
2. Livne, E. “Aeroelasticity of joined-wing airplane configurations - Past work and future challenges - a survey,” Proceedings of the 42nd Structures,Structural Dynamics and Materials Conference, Seattle, Washington, April 2001, AIAA2001-1370.
3. Blair, M. and Canfield, R. “A Joined- Wing Structural Weight Modeling Study,” Proceedings of the 43rd Structures,Structural Dynamics and Materials Conference, Denver, Colorado, April 2002, AIAA-2002-1337.
4. A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams
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