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

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

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

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

^b TECHNICAL UNIVERSITY OF MUNICH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; BOUNDARY LAYERS; ENGINES; MARINE ENGINES; NUMERICAL ANALYSIS; STATORS; SUPERSONIC AIRCRAFT;

AERODYNAMIC EFFECT; AXIAL COMPRESSORS; END-WALL BOUNDARY LAYERS; NAVIER-STOKES SOLVER; RADIAL LOADINGS; STATOR CONFIGURATION; THREE-DIMENSIONAL FLOW; TRANSONIC COMPRESSOR;

NAVIER STOKES EQUATIONS;

EID: 84955473748     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0491     Document Type: Conference Paper

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