High lift and aft-loaded profiles for low-pressure turbines

Journal of Turbomachinery

Volumn 123, Issue 2, 2001, Pages 181-188

  Howell, R J ^a   Ramesh, O N ^a   Hodson, H P ^a   Harvey, N W ^a   Schulte, V ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; REYNOLDS NUMBER; SURFACE PHENOMENA; TURBOMACHINE BLADES; WIRE;

SURFACE -MOUNTED HOT FILMS;

TURBINES;

TURBINE;

EID: 0035299032     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1350409     Document Type: Article

References (15)

1. The technical and economic relevance of understanding boundary layer transition in gas turbine engines
2. Development of blade profiles for low-pressure turbine applications
3. Aerodynamic design of low pressure turbines
4. Unsteady wake-induced boundary layer transition in highly loaded LP turbines
5. Wake passing in LP turbines
6. An inviscid blade-to-blade prediction of a wake-generated unsteady flow
7. Correction for the effect of ambient temperature drift on hot-wire measurements in incompressible flow
8. Determination of mean and dynamic skin friction separation and transition in low-speed flow with a thin-film heated element
9. Boundary layer and loss measurements on the rotor of an axial-flow turbine
10. A semi-empirical theory for surface mounted aerodynamic wall shear stress gages
11. Entropy generation in turbomachinery flows
12. Blade row interaction in a multistage low-pressure turbine