On the coupling of inverse design and optimization techniques for the multiobjective, multipoint design of turbomachinery blades

Journal of Turbomachinery

Volumn 131, Issue 2, 2009, Pages

  Bonaiuti, Duccio ^a   Zangeneh, Mehrdad ^b  

^a Advanced Design Technology Ltd   (United Kingdom)

^b UNIVERSITY COLLEGE LONDON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC OPTIMIZATION; AERODYNAMIC PARAMETERS; AUTOMATIC OPTIMIZATION; AXIAL COMPRESSORS; BLADE LOADING; BLADE SHAPES; COMPUTATIONAL COSTS; COMPUTATIONAL FLUID DYNAMICS ANALYSIS; DESIGN GUIDELINES; DESIGN METHOD; DESIGN PARAMETERS; DESIGN STRATEGIES; DIRECT CONTROL; INDUSTRIAL PRACTICES; INDUSTRIAL STANDARDS; INVERSE DESIGN METHODS; INVERSE DESIGNS; MECHANICAL DESIGN; MULTI OBJECTIVE; MULTI OBJECTIVE EVOLUTIONARY ALGORITHMS; MULTIPOINT; OFF-DESIGN PERFORMANCE; OPTIMIZATION PROCESS; OPTIMIZATION STRATEGY; PARAMETRIZATIONS; RESPONSE FUNCTIONS; RESPONSE SURFACE METHOD; SIMILAR DESIGN; TIME FRAME; TURBOMACHINES;

AERODYNAMICS; CENTRIFUGAL COMPRESSORS; CENTRIFUGATION; COMPUTATION THEORY; COMPUTATIONAL FLUID DYNAMICS; EVOLUTIONARY ALGORITHMS; MULTIOBJECTIVE OPTIMIZATION; SENSITIVITY ANALYSIS; THREE DIMENSIONAL; TURBINES; TURBOMACHINE BLADES;

MACHINE DESIGN;

EID: 77952832195     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2950065     Document Type: Article

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