Experimental and Numerical Investigation of Non-reacting Flow …
137
5. Hall BF, Chana KS, Povey T (2013) Design of a non-reacting combustor simulator with swirl
and temperature distortion with experimental validation. In: Proceedings of the ASME turbo
expo: turbine technical conference and exposition. Volume 3C: heat transfer. San Antonio,
Texas, USA. June 3–7, 2013. V03CT17A010. ASME
6. Gouda P, Srinivasan K, Sivaramakrishna G, Shashishekar KS (2016) CFD analysis of gas
turbine combustor primary zone using different axial swirler configurations. Int J Mech Prod
Eng 4(6)
7. Karuppannan S, Sondur VM, Sivaramakrishna G, Navindgi RD, Muthuveerappan N (2017)
CFD analyses of combustor-diffuser system of marine gas turbine engine. In: Proceedings of
the ASME gas turbine india conference. Volume 1: compressors, fans and pumps; turbines;
heat transfer; combustion, fuels and emissions. Bangalore, India. V001T04A013. ASME
8. Crocker DS, Nickolaus D, Smith CE (1999) CFD modeling of a gas turbine combustor from
compressor exit to turbine inlet. ASME J Eng Gas Turbines Power 121(1), 89–95
9. Ananda Reddy G, Ganesan V (2004) Non-reacting flow analysis from combustor inlet to outlet
using computational fluid dynamics code. Defence Sci J 54(4), 455–467
10. Dzida M, Kosowski K (2015) Experimental investigations of pressure drop in the combustion
chamber of gas turbine. ASME. Turbo expo: power for land, sea, and air. Volume 3: coal,
biomass and alternative fuels; combustion and fuels; oil and gas applications. V003T06A001
11. Knight MA, Walker RB (1957) The component pressure losses in combustion chambers.
Aeronautical Research Council R and M 2987, UK
12. Zhou D, Wang T (1998) Cold flow computations for the diffuser-combustor section of an
industrial gas turbine. ASME 96-GT-513, Presented at the international gas turbine and aero
engine congress and exhibition, Birmingham, UK
13. Lefebvre AH, Ballal DR (2010) Gas turbine combustion
137
5. Hall BF, Chana KS, Povey T (2013) Design of a non-reacting combustor simulator with swirl
and temperature distortion with experimental validation. In: Proceedings of the ASME turbo
expo: turbine technical conference and exposition. Volume 3C: heat transfer. San Antonio,
Texas, USA. June 3–7, 2013. V03CT17A010. ASME
6. Gouda P, Srinivasan K, Sivaramakrishna G, Shashishekar KS (2016) CFD analysis of gas
turbine combustor primary zone using different axial swirler configurations. Int J Mech Prod
Eng 4(6)
7. Karuppannan S, Sondur VM, Sivaramakrishna G, Navindgi RD, Muthuveerappan N (2017)
CFD analyses of combustor-diffuser system of marine gas turbine engine. In: Proceedings of
the ASME gas turbine india conference. Volume 1: compressors, fans and pumps; turbines;
heat transfer; combustion, fuels and emissions. Bangalore, India. V001T04A013. ASME
8. Crocker DS, Nickolaus D, Smith CE (1999) CFD modeling of a gas turbine combustor from
compressor exit to turbine inlet. ASME J Eng Gas Turbines Power 121(1), 89–95
9. Ananda Reddy G, Ganesan V (2004) Non-reacting flow analysis from combustor inlet to outlet
using computational fluid dynamics code. Defence Sci J 54(4), 455–467
10. Dzida M, Kosowski K (2015) Experimental investigations of pressure drop in the combustion
chamber of gas turbine. ASME. Turbo expo: power for land, sea, and air. Volume 3: coal,
biomass and alternative fuels; combustion and fuels; oil and gas applications. V003T06A001
11. Knight MA, Walker RB (1957) The component pressure losses in combustion chambers.
Aeronautical Research Council R and M 2987, UK
12. Zhou D, Wang T (1998) Cold flow computations for the diffuser-combustor section of an
industrial gas turbine. ASME 96-GT-513, Presented at the international gas turbine and aero
engine congress and exhibition, Birmingham, UK
13. Lefebvre AH, Ballal DR (2010) Gas turbine combustion