Performance assessment of a prototype Trapped Vortex Combustor concept for gas turbine application

Proceedings of the ASME Turbo Expo

Volumn 2, Issue , 2001, Pages

  Burrus, D L ^a   Johnson, A W ^a   Roquemore, W M ^b   Shouse, D T ^b  

^a GE AVIATION   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALTERNATIVE FUELS; COAL COMBUSTION; COMBUSTORS; GAS TURBINES; IGNITION; RAMJET ENGINES;

AIR FORCE RESEARCH LABORATORY; AIRCRAFT GAS TURBINE ENGINES; COMBUSTION EFFICIENCIES; GAS TEMPERATURE PROFILE; GAS TURBINE APPLICATIONS; PERFORMANCE ASSESSMENT; TEST RIG CONFIGURATION; TRAPPED VORTEX COMBUSTOR;

ATMOSPHERIC TEMPERATURE;

EID: 84905733210     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2001-GT0087     Document Type: Conference Paper

References (2)

1. Hsu, K. Y., Gross, L. P., and Trump, D. D., "Performance of a Trapped Vortex Combustor", Paper No. 95-0810, AIAA 33rd Aerospace Sciences Meeting and Exhibit, Reno Nevada, January 9-12, 1995.
2. Hsu, K. Y., Gross, L. P., and Roquemore, W. M., "Characteristics of a Trapped Vortex Combustor", Journal of Propulsion and Power, Vol. 14, No. 1, pp. 57-65, January-February 1998