Aircraft wing box optimization considering uncertainty in surrogate models

Structural and Multidisciplinary Optimization

Volumn 42, Issue 5, 2010, Pages 745-753

  Neufeld, Daniel ^a   Behdinan, Kamran ^a   Chung, Joon ^a  

^a RYERSON UNIVERSITY   (Canada)

Author keywords

Aircraft conceptual design; MDO; RBDO

Indexed keywords

AEROSPACE DESIGN; AIRCRAFT CONCEPTUAL DESIGNS; AIRCRAFT WING; APPROXIMATION MODEL; DESIGN GOAL; DESIGN OPTIMIZATION; DESIGN PROCESS; FEASIBLE SOLUTION; HIGH FIDELITY; MDO; PHYSICS-BASED ANALYSIS; RBDO; RELIABILITY-BASED DESIGN OPTIMIZATION; SIMPLIFIED ANALYSIS; SURROGATE MODEL; WING BOX;

AIRCRAFT MODELS; COMPUTATIONAL FLUID DYNAMICS; CONCEPTUAL DESIGN; FUNCTION EVALUATION; MACHINE DESIGN; OPTIMIZATION; UNCERTAINTY ANALYSIS; WINGS;

FINITE ELEMENT METHOD;

EID: 79951766252     PISSN: 1615147X     EISSN: 16151488     Source Type: Journal    
DOI: 10.1007/s00158-010-0532-8     Document Type: Article

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