New low emission strategies and combustor designs for civil aeroengine applications

Progress in Computational Fluid Dynamics

Volumn 4, Issue 3-5, 2004, Pages 130-142

  Bauer, Hans Joerg ^a  

^a ROLLS ROYCE DEUTSCHLAND LTD AND CO KG   (Germany)

Author keywords

Aeroengine; Combustion; Gas turbine; Lean direct injection; Lean module; Lean premixed prevapourised combustion; NO formation; NOx; Operability; Pressure ratio; Rich burn quick quench lean burn combustion; Staged combustion

Indexed keywords

AIRCRAFT; COMBUSTION; COMBUSTORS; DIFFUSION; JET ENGINES; NITROGEN OXIDES; OPTIMIZATION;

CONVENTIONAL COMBUSTORS; DEGREE OF MATURITY; HIGH POWER CONDITIONS; LOW EMISSION;

COMPUTATIONAL FLUID DYNAMICS;

AEROSPACE; COMBUSTOR; COMPUTATIONAL FLUID DYNAMICS; EMISSION; INDUSTRIAL APPLICATION;

EID: 2442583626     PISSN: 14684349     EISSN: None     Source Type: Journal    
DOI: 10.1504/pcfd.2004.004081     Document Type: Article

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