Using sweep and dihedral to control three-dimensional flow in transonic stators of axial compressors

Journal of Turbomachinery

Volumn 123, Issue 1, 2001, Pages 40-48

  Gummer V ^a   Wenger, U ^a   Kau, H P ^a  

^a ROLLS ROYCE DEUTSCHLAND LTD AND CO KG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; BOUNDARY LAYERS; MACHINE DESIGN; NUMERICAL ANALYSIS; STATORS; TURBOMACHINE BLADES;

AERO-ENGINE FANS;

COMPRESSORS;

AXIAL COMPRESSOR; CONTROL SYSTEM; THREE-DIMENSIONAL FLOW;

EID: 0034889109     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1330268     Document Type: Article

References (21)

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4. Sweep and dihedral effects in axial-flow turbomachinery
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7. Theoretische und experimentelle Untersuchungen an konischen Turbinengittern
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10. Comparison of sweep and dihedral effects on compressor cascade performance
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15. A description of eddying motions and flow patterns using critical-point concepts