Results 171 to 180 of about 22,484 (217)
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Short Helical Combustor: Concept Study of an Innovative Gas Turbine Combustor
Volume 4A: Combustion, Fuels and Emissions, 2015An innovative design of a gas turbine annular combustor is investigated analytically and numerically. Its principal feature is the helical arrangement of the burners around the turbine shaft. Hence, a shorter combustor with lower aerodynamical losses and cooling air demand might be realized. A generic model of the combustor is developed and analyzed by
Ariatabar, B., Koch, R., Bauer, H.-J.
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Automatic Combustor Controller Development and Liquid-Fuel Combustor Design Program
1983Abstract : This technical report, prepared for the Aerospace Power Division, Aero Propulsion Laboratory, Wright-Patterson AFB, states design and test results of a combustor controller integrated with an existing 1kW free-piston Stirling engine. This report document also states the design of a liquid-fuel external heat system capable of operating with a
R. A. Farrell +3 more
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Radiative heating in scramjet combustors
31st Thermophysics Conference, 1996Currently, there is considerable interest in scramjet engines for hypersonic aircraft and missiles. This paper presents preliminary calculations of the radiative heating of the walls of scramjet combustion chambers. The analysis assumes isothermal, constant property ow elds that are representative of actual combustor ow elds.
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2012
Explore a unified treatment of the dynamics of combustor systems, including acoustics, fluid mechanics, and combustion in a single rigorous text. This updated new edition features an expansion of data and experimental material, updates the coverage of flow stability, and enhanced treatment of flame dynamics.
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Explore a unified treatment of the dynamics of combustor systems, including acoustics, fluid mechanics, and combustion in a single rigorous text. This updated new edition features an expansion of data and experimental material, updates the coverage of flow stability, and enhanced treatment of flame dynamics.
openaire +1 more source
2012
A highly-reliable combustor is provided that allows flash back of flame into a premixer to be suppressed. The combustor has a mixing chamber forming member 110 that forms a mixing chamber thereinside. The mixing chamber includes a first mixing chamber 200 broadening toward a downstream side.
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A highly-reliable combustor is provided that allows flash back of flame into a premixer to be suppressed. The combustor has a mixing chamber forming member 110 that forms a mixing chamber thereinside. The mixing chamber includes a first mixing chamber 200 broadening toward a downstream side.
openaire +1 more source
Emission analysis of the CH4/NH3/air co-firing fuels in a model combustor
Fuel, 2021Zuohua Huang
exaly

