Viscous throughflow modeling of axial compressor bladerows using a tangential blade force hypothesisr

Journal of Turbomachinery

Volumn 120, Issue 4, 1998, Pages 662-670

  Gallimore, S J ^a  

^a ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW TURBOMACHINERY; BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; MATHEMATICAL MODELS; SHEAR FLOW; TURBOMACHINE BLADES; VISCOUS FLOW;

AXIAL COMPRESSORS; AXISYMMETRIC VISCOUS THROUGHFLOW METHOD;

COMPRESSORS;

AXIAL COMPRESSOR; AXISYMMETRIC FLOW; BLADE AERODYNAMICS;

EID: 0032194746     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841775     Document Type: Article

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