Rotating instabilities in An Axial compressor originating from the fluctuating blade Tip Vortex

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Mailach, R ^a   Lehmann, I ^a   Vogeler, K ^a  

^a DRESDEN UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; AXIAL FLOW; AXIAL FLOW TURBOMACHINERY; CENTRIFUGAL COMPRESSORS; LASER DOPPLER VELOCIMETERS; TURBOMACHINE BLADES; VORTEX FLOW; WIND TUNNELS;

EXPERIMENTAL INVESTIGATIONS; HIGH-SPEED AXIAL COMPRESSORS; LASER DOPPLER ANEMOMETRY; ROTATING INSTABILITY; ROTATING STRUCTURES; SPATIAL DEVELOPMENT; UNSTEADY FLOW PHENOMENON; UNSTEADY PRESSURE MEASUREMENTS;

AXIAL-FLOW COMPRESSORS;

EID: 84955256379     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0506     Document Type: Conference Paper

References (19)

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