An example of global structural optimisation with genetic algorithms in the aerospace field

Computational Plasticity: Fundamentals and Applications - Proceedings of the 8th International Conference on Computational Plasticity, COMPLAS VIII

Volumn , Issue PART 2, 2005, Pages 1019-1022

  Gallet, C ^a   Salaun M ^b   Bouchet, E ^a  

^a AIRBUS   (France)

^b UNIVERSITÉ DE TOULOUSE   (France)

Author keywords

Buckling; Constrained optimisation; Genetic algorithm; S.Q.P.; Stiffened panel

Indexed keywords

AEROSPACE FIELD; COMPRESSIVE LOADS; FUSELAGE SECTIONS; NON-LINEAR CONSTRAINTS; OPTIMISATION METHOD; OPTIMISATIONS; S.Q.P.; STIFFENED PANEL; STRUCTURAL OPTIMISATION;

BUCKLING; FUSELAGES; STRUCTURAL OPTIMIZATION;

GENETIC ALGORITHMS;

EID: 84857165551     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Bruhn E.F. - Analysis and design of flight vehicle structures. Tri-State Offset Company 1965.
2. Rigal M. - Application des techniques d'optimisation au dimensionnement de l'extrados et de l'intrados d'un tronçon central de voilure. PhD report, INSA Toulouse, 2000.
3. Lemonge A. and Barbosa H. - An adaptative penalty scheme for genetic algorithms in structural optimisation. Int. J. Numer. Meth. Engng, 2004, 59, 703-736. (Pubitemid 38187977)
4. Gallet C. - Comparaison des technologies fuselage. PhD report, U.P.S. December 2005.