Mixed-variable optimization strategy employing multifidelity simulation and surrogate models

AIAA Journal

Volumn 48, Issue 1, 2010, Pages 215-223

  Singh, Gulshan ^a   Grandhi, Ramana V ^a  

^a WRIGHT STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT STRUCTURAL COMPONENTS; AXISYMMETRIC; COMPRESSIVE RESIDUAL STRESS; DESIGN METHODOLOGY; DESIGN OPTIMIZATION; DESIGN PROBLEMS; DESIGN SPACES; ELASTIC-PLASTIC ANALYSIS; ELASTIC-PLASTIC DEFORMATION; FULL-SCALE MODELS; HIGHLY NONLINEAR; LASER PEENING; MIXED TYPE; MIXED VARIABLES; MODIFIED PARTICLE SWARM OPTIMIZATION; MULTI-FIDELITY SIMULATION; NUMBER OF SHOTS; OPTIMIZATION STRATEGY; OPTIMIZATION VARIABLES; OPTIMUM SOLUTION; PARAMETRIC STUDY; PRESSURE PULSE; SIMULATION-BASED DESIGNS; STRESS CONSTRAINTS; STRUCTURAL COMPONENT; SURFACE ENHANCEMENT; SURFACE FATIGUE LIVES; SURROGATE MODEL;

DESIGN; ELASTOPLASTICITY; LOCATION; RESIDUAL STRESSES; SHOT PEENING; THREE DIMENSIONAL;

PARTICLE SWARM OPTIMIZATION (PSO);

EID: 77049117100     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.43469     Document Type: Article

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