Concurrent aerostructural topology optimization of a wing box

Author:

James Kai A.,Kennedy Graeme J.,Martins Joaquim R.R.A.

Publisher

Elsevier BV

Subject

Computer Science Applications,Mechanical Engineering,General Materials Science,Modelling and Simulation,Civil and Structural Engineering

Reference44 articles.

1. Grihon S, Krog L, Tucker A, Hertel K. A380 weight savings using numerical structural optimization. In: 20th AAAF colloquium on material for aerospace applications, Paris, France; 2004. p. 763–66.

2. Krog L,Tucker A. Topology optimization of aircraft wing box ribs. In: 10th AIAA/ISSMO multidisciplinary analysis and optimization conference, Albany, New York; 2004 [AIAA 2004-4481].

3. Buchanan S. Development of a wingbox rib for a passenger jet aircraft using design optimization and constrained to traditional design and manufacture requirements; 2007.

4. New topology optimization method for leading-edge ribs;Wang;J Aircraft,2011

5. Structural optimization complexity: what has moore’s law done for us?;Venkataraman;Struct Multi Optim,2004

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