PARALLEL GENETIC ALGORITHM IMPLEMENTATION IN MULTIDISCIPLINARY ROTOR BLADE DESIGN

Authors
Citation
J. Lee et P. Hajela, PARALLEL GENETIC ALGORITHM IMPLEMENTATION IN MULTIDISCIPLINARY ROTOR BLADE DESIGN, Journal of aircraft, 33(5), 1996, pp. 962-969
Citations number
22
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00218669
Volume
33
Issue
5
Year of publication
1996
Pages
962 - 969
Database
ISI
SICI code
0021-8669(1996)33:5<962:PGAIIM>2.0.ZU;2-E
Abstract
An adaptation of genetic algorithms as an optimization tool for large- scale multidisciplinary design problems is described. The design of a hingeless composite rotor blade is used as a test bed for this class o f problems, where the formulation of the objective and constraint func tions requires the consideration of disciplines of aerodynamics, perfo rmance, dynamics, and structures. A rational decomposition approach ba sed on the use of neural networks is proposed for partitioning the lar ge-scale multidisciplinary design problem into smaller, more tractable subproblems. A design method based on a parallel implementation of ge netic algorithms is shown to be an effective strategy, providing incre ased computational efficiency, and a natural approach to account for t he coupling between temporarily decoupled subproblems.