Experimental investigation of turbulent wake-blade interaction in axial compressors

International Journal of Heat and Fluid Flow

Volumn 21, Issue 3, 2000, Pages 285-290

  Sentker, A ^a   Riess, W ^a  

^a LEIBNIZ UNIVERSITY HANNOVER   (Germany)

Author keywords

Low speed axial compressor; Turbulence measurements; Unsteady flow field; Wake transport

Indexed keywords

AXIAL FLOW TURBOMACHINERY; COMPRESSORS; COMPUTER SIMULATION; FLOW MEASUREMENT; FLUID STRUCTURE INTERACTION; INCOMPRESSIBLE FLOW; STATORS; TURBOMACHINE BLADES; UNSTEADY FLOW;

LOW-SPEED AXIAL COMPRESSORS;

WAKES;

AXIAL COMPRESSOR; BLADE AERODYNAMICS; EXPERIMENTAL STUDY; UNSTEADY FLOW; WAKE;

EID: 0034044276     PISSN: 0142727X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-727X(00)00011-4     Document Type: Conference Paper

References (5)

1. Sentker, A., Riess, W., 1996. In: Rodi, W., Bergeles, G. (Eds.),Turbulence Intensity Measurements in a Low Speed Axial Compressor, Engineering Turbulence Modelling and Experiments 3, Elsevier, Amsterdam, pp. 773-783.
2. Sentker, A., Riess, W., 1997. Unsteady flow and turbulence in a low speed axial compressor. In: Eighth International Symposium on Unsteady Aerodynamics and Aeroelasticity of Turbomachines, 15-18 September. Stockholm.
3. Sentker A., Riess W. Measurement of unsteady flow and turbulence in a low speed axial compressor. Experimental Thermal and Fluid Science. 17:1998;124-131.
4. Traulsen, D., 1989. Axialverdichterprüfstand zur Untersuchung von Randzonenströmungen, Fortschrittberichte VDI, Reihe 7, Nr. 161.
5. Zaccaria M.A., Lakshminarayana B. Unsteady flow field due to nozzle wake interaction with the rotor in an axial flow turbine: part I rotor passage flow field. Journal of Turbomachinery. 119:1997;201-213.