Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex

Journal of Turbomachinery

Volumn 123, Issue 3, 2001, Pages 453-463

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

^a DRESDEN UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW TURBOMACHINERY; FANS; ROTATION; ROTORS; SENSORS; TURBOMACHINE BLADES; VORTEX FLOW;

ROTATING INSTABILITY;

COMPRESSORS;

AXIAL COMPRESSOR; AXIAL FLOW FAN; BLADE; FLUCTUATING FLOW; ROTATING FLOW; VORTEX;

EID: 0035389221     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1370160     Document Type: Article

References (7)

1. Stall inception and the prospects for active control in four high-speed compressors
2. Propagation of multiple short length-scale stall cells in an axial compressor rotor
3. Development of small rotating stall in a single stage axial compressor
4. Stability of flow through multistage axial compressors
5. Non-engine order blade vibration in a high pressure compressor
6. Experimentelle Untersuchung zur Entstehung und Minderung des Blattspitzen-Wirbellärms axialer Strömungsmaschinen
7. The periodical interaction of the tip clearance flow in the blade rows of axial compressors