Optimal design of aeroengine turbine disc based on kriging surrogate models

Computers and Structures

Volumn 89, Issue 1-2, 2011, Pages 27-37

  Huang, Zhangjun ^a,b   Wang, Chengen ^b   Chen, Jian ^a   Tian, Hong ^a  

^a CHANGSHA UNIVERSITY OF SCIENCE AND TECHNOLOGY   (China)

^b KEY LABORATORY OF INTEGRATED AUTOMATION OF PROCESS INDUSTRY   (China)

Author keywords

Design of experiments; Differential evolutionary algorithm; Kriging method; Optimal design; Surrogate model; Turbine disc

Indexed keywords

DIFFERENTIAL EVOLUTIONARY ALGORITHM; KRIGING METHODS; OPTIMAL DESIGN; SURROGATE MODEL; TURBINE DISC;

AIRCRAFT ENGINES; DESIGN OF EXPERIMENTS; EVOLUTIONARY ALGORITHMS; FUEL ADDITIVES; INTERPOLATION; OPTIMAL SYSTEMS; TURBINES;

SHAPE OPTIMIZATION;

EID: 78449245995     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruc.2010.07.010     Document Type: Article

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