Instability mechanism in a swirl flow combustor: precession of vortex core and influence of density gradient

K Manoharan, S Hansford… - … Expo: Power for …, 2015 - asmedigitalcollection.asme.org
Combustion instability is a serious problem limiting the operating envelope of present day
gas turbine systems using a lean premixed combustion strategy. Gas turbine combustors …

Instability Mechanism in a Swirl Flow Combustor: Precession of Vortex Core and Influence of Density Gradient

K Manoharan, S Hansford… - … Expo: Power for …, 2015 - asmedigitalcollection.asme.org
Combustion instability is a serious problem limiting the operating envelope of present day
gas turbine systems using a lean premixed combustion strategy. Gas turbine combustors …

[PDF][PDF] INSTABILITY MECHANISM IN A SWIRL FLOW COMBUSTOR: PRECESSION OF VORTEX CORE AND INFLUENCE OF DENSITY GRADIENT

K Manoharan, S Hansford, J O'Connor, S Hemchandra - scholar.archive.org
Combustion instability is a serious problem limiting the operating envelope of present day
gas turbine systems using a lean premixed combustion strategy. Gas turbine combustors …

INSTABILITY MECHANISM IN A SWIRL FLOW COMBUSTOR: PRECESSION OF VORTEX CORE AND INFLUENCE OF DENSITY GRADIENT

K Manoharan, S Hansford, J O'Connor, S Hemchandra - 2015 - eprints.iisc.ac.in
Combustion instability is a serious problem limiting the operating envelope of present day
gas turbine systems using a lean premixed combustion strategy. Gas turbine combustors …

Instability mechanism in a swirl flow combustor: Precession of vortex core and influence of density gradient

K Manoharan, S Hansford, J O'Connor… - ASME Turbo Expo …, 2015 - pure.psu.edu
Combustion instability is a serious problem limiting the operating envelope of present day
gas turbine systems using a lean premixed combustion strategy. Gas turbine combustors …

INSTABILITY MECHANISM IN A SWIRL FLOW COMBUSTOR: PRECESSION OF VORTEX CORE AND INFLUENCE OF DENSITY GRADIENT

K Manoharan, S Hansford, J O'Connor, S Hemchandra - 2015 - eprints.iisc.ac.in
Combustion instability is a serious problem limiting the operating envelope of present day
gas turbine systems using a lean premixed combustion strategy. Gas turbine combustors …