Aerodynamic loss characteristics of a turbine blade with trailing edge coolant ejection: Part 2- External aerodynamics,total pressure losses, and predictions

Journal of Turbomachinery

Volumn 123, Issue 2, 2001, Pages 249-257

  Uzol, O ^a   Camci, C ^a  

^a PENNSYLVANIA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; REYNOLDS NUMBER; SUBSONIC FLOW; VELOCITY MEASUREMENT;

COOLANT EJECTION;

TURBOMACHINE BLADES;

AERODYNAMICS; ENGINE; FLUID MECHANICS; GAS TURBINE;

EID: 0035299096     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1351817     Document Type: Article

References (12)

1. The aerodynamics of trailing-edge-cooled transonic turbine blades: Part 1- Experimental approach
2. Optimization of trailing edge ejection mixing losses: A theoretical and experimental study
3. Investigation of the flow field downstream of a turbine trailing edge cooled nozzle guide vane
4. Techniques for aerodynamic loss measurement of transonic turbine cascades with trailing-edge region coolant ejection
5. Aerodynamic effect of coolant ejection in the rear part of transonic rotor blades
6. Aerodynamic performance of a transonic turbine guide vane with trailing edge coolant ejection: Part 1- Experimental approach
7. Aerodynamic loss characteristics of a turbine blade with trailing edge coolant ejection: Part 1- Effect of cut-back length, spanwise rib spacing, free-stream reynolds number, and chordwise rib length on discharge coefficients
8. Streakline flow visualization study of a horseshoe vortex in a large-scale, two-dimensional turbine stator cascade
9. Local heat transfer measurements on a large, scale-model turbine blade airfoil using a composite of a heater element and liquid crystals
10. Performance analysis of a turbine stage having cooled nozzle blades with trailing edge ejection
11. Lecture notes on turbulence modeling in industrial flows