An experimental and numerical investigation into the mechanisms of rotating instability

Journal of Turbomachinery

Volumn 124, Issue 3, 2002, Pages 367-374

  März, Joachim ^a   Hah, Chunill ^a   Neise, Wolfgang ^a  

^a ATLAS ELEKTRONIK GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW; COMPRESSORS; NAVIER STOKES EQUATIONS; NUMERICAL METHODS; ROTATION; ROTORS;

AXIAL FLOW COMPRESSORS; DOUBLE PHASE-AVERAGING;

TURBOMACHINERY;

AXIAL COMPRESSOR; CLEARANCE; FLOW ANALYSIS; VORTEX;

EID: 0036649490     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1460915     Document Type: Article

References (15)

1. Experimental study of tip clearance losses and noise in axial turbomachines and their reduction
2. On the azimuthal mode structure of rotating blade flow instabilities in axial turbomachines
3. Non engine order blade vibration in a high speed compressor
4. Experimentelle Untersuchung von Verdichterinstabilitäten am Niedergeschwindigkeitsverdichter Dresden
5. A navier-stokes analysis of three-dimensional turbine flows inside turbine blade rows at design and off-design conditions
6. Calculation of three-dimensional viscous flows in turbomachinery with an implicit relaxation method
7. Calculation of wake-induced unsteady flow in a turbine cascade
8. Unsteady aerodynamic phenomena in a transonic compressor stage
9. Numerical and experimental study for the short wavelength stall inception in a low-speed axial compressor
10. Measurements of tip clearance flow for a high reynolds number axial-flow rotor: Part 1 - Flow visualization
11. Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex
12. Casing boundary layers in multistage axial-flow compressors
13. Stalling pressure rise capability of axial compressor stage