A numerical study of secondary flow in axial turbines with application to radial transport of hot streaks

Journal of Turbomachinery

Volumn 122, Issue 4, 2000, Pages 667-673

  Prasad, D ^a   Hendricks, G J ^a  

^a United Technologies   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW TURBINE; MATHEMATICAL ANALYSIS; SECONDARY FLOW;

EID: 0034532924     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1313817     Document Type: Conference Paper

References (24)

1. Dynamic gas temperature measurement system
2. Redistribution of an inlet temperature distortion in an axial flow turbine stage
3. Secondary circulation in fluid flow
4. Navier-stokes analysis of the redistribution of inlet temperature distortions in a turbine
5. Numerical investigation of hot streaks in turbines
6. Unsteady analysis of hot streak migration in a turbine stage
7. Unsteady hot streak migration through a 1 1/2-stage turbine
8. Hot streak clocking effects in a 1 1/2-stage turbine
9. Effect of hot streak indexing in a 1 1/2-stage turbine
10. Hot streaks and phantom cooling in a turbine rotor passage: Part 1-Separate effects
11. Analysis of hot streak effects on turbine rotor heat load
12. Secondary flows
13. Generalized expressions for secondary vorticity using intrinsic coordinates
14. Secondary vorticity in stratified compressible fluids in rotating systems
15. On the multiplicity of steady gas flows having the same streamline pattern
16. A multiple grid scheme for solving the euler equations
17. Cascade viscous flow analysis using Navier-Stokes equations
18. Thin layer approximation and algebraic model for separated turbulent flows
19. Nonreflecting boundary conditions for euler equation calculations
20. Prediction of 3-D unsteady flow and multi-stage turbomachinery using an implicit dual time-step approach
21. Predictions of 3-D multi-stage turbine flow fields using a multiple-grid Euler solver
22. Using a 3-D Euler flow simulation to assess effects of periodic unsteady flow through turbines
23. Intra-stator transport of rotor wakes and its effect on compressor performance