scholarly journals 5 kHz thermometry in a swirl-stabilized gas turbine model combustor using chirped probe pulse femtosecond CARS. Part 1: Temporally resolved swirl-flame thermometry

2016 ◽  
Vol 173 ◽  
pp. 441-453 ◽  
Author(s):  
Claresta N. Dennis ◽  
Carson D. Slabaugh ◽  
Isaac G. Boxx ◽  
Wolfgang Meier ◽  
Robert P. Lucht
Keyword(s):  
Gas Turbine ◽  
Probe Pulse ◽  
Swirl Flame ◽  
Turbine Model

scholarly journals 5 kHz thermometry in a swirl-stabilized gas turbine model combustor using chirped probe pulse femtosecond CARS. Part 2. Analysis of swirl flame dynamics

2016 ◽  
Vol 173 ◽  
pp. 454-467 ◽  
Author(s):  
Carson D. Slabaugh ◽  
Claresta N. Dennis ◽  
Isaac Boxx ◽  
Wolfgang Meier ◽  
Robert P. Lucht
Keyword(s):  
Gas Turbine ◽  
Probe Pulse ◽  
Flame Dynamics ◽  
Swirl Flame ◽  
Turbine Model

scholarly journals Chirped probe pulse femtosecond coherent anti-Stokes Raman scattering thermometry at 5 kHz in a Gas Turbine Model Combustor

2015 ◽  
Vol 35 (3) ◽  
pp. 3731-3738 ◽  
Author(s):  
Claresta N. Dennis ◽  
Carson D. Slabaugh ◽  
Isaac G. Boxx ◽  
Wolfgang Meier ◽  
Robert P. Lucht
Keyword(s):  
Raman Scattering ◽  
Gas Turbine ◽  
Probe Pulse ◽  
Anti Stokes ◽  
Turbine Model

The Civic: A Concept in Vortex Induced Combustion for the Solar Gemini 10 kW Gas Turbine

1981 ◽  
Vol 103 (1) ◽  
pp. 34-42 ◽  
Author(s):  
J. R. Shekleton
Keyword(s):  
Gas Turbine ◽  
Diffusion Flames ◽  
Reynolds Numbers ◽  
Flame Stabilization ◽  
Fuel Injector ◽  
Combustion Chambers ◽  
Turbine Generator ◽  
Fuel Injectors ◽  
Swirl Flame ◽  
Combustion Processes

The Radial Engine Division of Solar Turbines International, an Operating Group of International Harvester, under contract to the U.S. Army Mobility Equipment Research & Development Command, developed and qualified a 10 kW gas turbine generator set. The very small size of the gas turbine created problems and, in the combustor, novel solutions were necessary. Differing types of fuel injectors, combustion chambers, and flame stabilizing methods were investigated. The arrangement chosen had a rotating cup fuel injector, in a can combustor, with conventional swirl flame stabilization but was devoid of the usual jet stirred recirculation. The use of centrifugal force to control combustion conferred substantial benefit (Rayleigh Instability Criteria). Three types of combustion processes were identified: stratified and unstratified charge (diffusion flames) and pre-mix. Emphasis is placed on five nondimensional groups (Richardson, Bagnold, Damko¨hler, Mach, and Reynolds numbers) for the better control of these combustion processes.

scholarly journals Influence of Single-Component Fuels on Gas-Turbine Model Combustor Lean Blowout

2018 ◽  
Vol 34 (1) ◽  
pp. 97-107 ◽  
Author(s):  
J. Grohmann ◽  
B. Rauch ◽  
T. Kathrotia ◽  
W. Meier ◽  
M. Aigner
Keyword(s):  
Gas Turbine ◽  
Single Component ◽  
Lean Blowout ◽  
Turbine Model

scholarly journals Dynamics of lean blowout of a swirl-stabilized flame in a gas turbine model combustor

2011 ◽  
Vol 33 (2) ◽  
pp. 2953-2960 ◽  
Author(s):  
M. Stöhr ◽  
I. Boxx ◽  
C. Carter ◽  
W. Meier
Keyword(s):  
Gas Turbine ◽  
Lean Blowout ◽  
Turbine Model
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