Multiobjective optimization using coupled response surface model and evolutionary algorithm

AIAA Journal

Volumn 43, Issue 6, 2005, Pages 1316-1325

  Lian, Yongsheng ^a,c   Liou, Meng Sing ^b,d  

^a OHIO AEROSPACE INSTITUTE   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

^c UNIVERSITY OF MICHIGAN   (United States)

^d MS 5 11   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT PROPULSION; COMPUTATIONAL FLUID DYNAMICS; FUNCTION EVALUATION; MATHEMATICAL MODELS; OPTIMIZATION; PRESSURE EFFECTS; STRUCTURAL DESIGN; TURBOMACHINE BLADES;

MULTIOBJECTIVE OPTIMIZATION; PRESSURE RATIO; RESPONSE SURFACE MODEL (RSM); SINGLE OBJECTIVE OPTIMIZATION;

EVOLUTIONARY ALGORITHMS;

EID: 20444442818     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.12994     Document Type: Article

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