Optimization of a stator blade using response surface method in a single-stage transonic axial compressor

Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy

Volumn 219, Issue 8, 2005, Pages 595-604

  Jang, C M ^a   Kim, K Y ^b  

^a Korea Institute of Civil Engineering and Building Technology   (South Korea)

^b Inha University   (South Korea)

Author keywords

Adiabatic efficiency; Optimal design; Stacking line; Transonic axial compressor

Indexed keywords

APPROXIMATION THEORY; AXIAL FLOW TURBOMACHINERY; COMPUTATIONAL GEOMETRY; DESIGN; NAVIER STOKES EQUATIONS; NUMERICAL ANALYSIS; NUMERICAL METHODS; OPTIMIZATION; RUNGE KUTTA METHODS; TRANSONIC FLOW; TURBOMACHINE BLADES;

ADIABATIC EFFICIENCY; STACKING LINE; STATOR BLADE; TRANSONIC AXIAL COMPRESSOR;

COMPRESSORS;

BLADE;

EID: 29244482598     PISSN: 09576509     EISSN: None     Source Type: Journal    
DOI: 10.1243/095765005X31298     Document Type: Article

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