Optimal design of complex engineering systems, such as aircraft composite structures, can often be accomplished only by applying decomposition techniques. In this paper, the optimal design of a composite wing-box is addressed by using a two-level scheme based on the Genetic Algorithm meta-heuristic. The two-level optimization strategy was evaluated for variations both in the angular step of the composite layers and in the strength of material.

A two-level procedure based on Genetic Algorithms to optimize an aeronautical composite structure / Chiwiacowsky, L. D.; Gasbarri, Paolo;  monti, R.;  velho, H. F. C.;  gómez, A. T.. - ELETTRONICO. - (2012), pp. 1-6. (Intervento presentato al convegno 27th Symposium On Applied Computing tenutosi a Riva del Garda (Trento), Italy nel March 26-30, 2012).

A two-level procedure based on Genetic Algorithms to optimize an aeronautical composite structure

GASBARRI, Paolo;
2012

Abstract

Optimal design of complex engineering systems, such as aircraft composite structures, can often be accomplished only by applying decomposition techniques. In this paper, the optimal design of a composite wing-box is addressed by using a two-level scheme based on the Genetic Algorithm meta-heuristic. The two-level optimization strategy was evaluated for variations both in the angular step of the composite layers and in the strength of material.
2012
27th Symposium On Applied Computing
Wing Box; Composite; Wing Aeroelasticity; Optimization
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
A two-level procedure based on Genetic Algorithms to optimize an aeronautical composite structure / Chiwiacowsky, L. D.; Gasbarri, Paolo;  monti, R.;  velho, H. F. C.;  gómez, A. T.. - ELETTRONICO. - (2012), pp. 1-6. (Intervento presentato al convegno 27th Symposium On Applied Computing tenutosi a Riva del Garda (Trento), Italy nel March 26-30, 2012).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/418243
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