Aeroelastic tailoring using fiber orientation and topology optimization

Author:

De Leon D. M.,de Souza C. E.,Fonseca J. S. O.,da Silva R. G. A.

Publisher

Springer Science and Business Media LLC

Subject

Control and Optimization,Computer Graphics and Computer-Aided Design,Computer Science Applications,Control and Systems Engineering,Software

Reference42 articles.

1. Abdalla MM, Breuker RD, Gürdal Z (2007) Aeroelastic tailoring of variable-stiffness slender wings for minimum compliance. In: International forum on aeroelasticity and structural dynamics 2007. Sweden

2. Ahmad S, Irons BM, Zienkievicz OC (1970) Analysis of thick and thin shell structure by curved finite elements. Int J Numer Methods Eng 2:419–451

3. Albano E, Rodden WP (1969) A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows. AIAA J 7(2):279–285. Errata, AIAA J 7(11):2192

4. Allemang RJ (2003) The modal assurance criterion - twenty years of use and abuse. Sound and vibrations, pp 14–21

5. Bendsøe MP, Sigmund O (2003) Topology optimization - theory, methods and applications. Springer - Verlag

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