The use of sweep and dihedral in multistage axial flow compressor blading-Part 1: University research and methods development

Journal of Turbomachinery

Volumn 124, Issue 4, 2002, Pages 521-532

  Gallimore, Simon J ^a   Bolger, John J ^a   Cumpsty, Nicholas A ^a   Taylor, Mark J ^b   Wright, Peter I ^b   Place, James M M ^b  

^a ASME   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

Author keywords

Compressor; Design; Dihedral; Multistage; Sweep

Indexed keywords

AXIAL FLOW; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; MACHINE DESIGN; ROTORS; TURBOMACHINE BLADES;

MULTISTAGE DESIGN;

HIGH PRESSURE TURBOMACHINERY;

AXIAL FLOW COMPRESSOR; BLADE; COMPUTATIONAL FLUID DYNAMICS; DESIGN; RESEARCH AND DEVELOPMENT;

EID: 0036821005     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1507333     Document Type: Article

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