The control of shroud leakage flows to reduce aerodynamic losses in a low aspect ratio, shrouded axial flow turbine

Journal of Turbomachinery

Volumn 123, Issue 2, 2001, Pages 334-341

  Wallis, A M ^a   Denton, J D ^a   Demargne, A A J ^a  

^a CA Parsons Works   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ASPECT RATIO; LEAKAGE (FLUID); ROTORS; STREAM FLOW;

ASPECT RATIO TURBINES;

AXIAL FLOW TURBOMACHINERY;

AERODYNAMICS; AXIAL FLOW; GAS TURBINE; LEAKAGE; ROTOR;

EID: 0035299035     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1354143     Document Type: Article

References (7)

1. Some practical effects of tip clearance in turbine blading
2. The practical application of solution-adaption to the numerical simulation of complex turbomachinery problems
3. An experimental study of the tip leakage flow around shrouded turbine blades
4. Loss mechanisms in turbomachines
5. Comparison of design intent and experimental measurements in a low aspect ratio axial flow turbine with three-dimensional blading
6. Parameterized study of high-speed compressor seal cavity flow