Influence of compressor exit conditions on combustor annular diffusers, part 1: Diffuser performance

Journal of Propulsion and Power

Volumn 17, Issue 3, 2001, Pages 678-685

  Barker, A G ^a   Carrotte, J F ^a  

^a LOUGHBOROUGH UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW; COMBUSTORS; COMPRESSORS; DIFFUSERS (FLUID); KINETIC ENERGY; PRESSURE EFFECTS;

COMBUSTOR ANNULAR DIFFUSER; OUTLET GUIDE VANES (OGV);

GAS TURBINES;

EID: 0035331828     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5795     Document Type: Article

References (9)

1. Characteristics of combustor diffusers
2. Experimentally determined optimum geometries for rectilinear diffusers with rectangular, conical or annular cross-section
3. Performance and flow regimes for annular diffusers
4. Influence of compressor exit conditions on diffuser performance
5. Influence of blade wakes on the performance of combustor shortened prediffusers
6. Experimental investigation of the flow in diffusers behind an axial flow compressor
7. The Development of a large annular facility for testing gas turbine combustor diffuser systems
8. Performance of annular combustor-dump diffusers
9. Loss mechanisms in turbomachines