Results 91 to 100 of about 21,213 (234)
This work presents a 3D numerical study of a steam-injected combustor for a gas turbine operating on an ammonia-hydrogen fuel blend, aimed at enabling carbon-free hybrid energy systems. The research focuses on the performance and emission characteristics
Serbin Serhiy +4 more
doaj +1 more source
In this paper, we consider the issue of thermo-chemical heat recovery of waste heat from gas turbine engines for the steam conversion of associated gas for offshore vessels. Current trends in the development of offshore infrastructure are identified, and
Cherednichenko Oleksandr +2 more
doaj +1 more source
A high‐pressure shock‐tube facility is developed to investigate high‐temperature chemical‐kinetics for next‐generation combustion systems. The design enables extended test times and integrates multiple optical diagnostics for time‐resolved species detection.
Sulaiman A. Alturaifi +8 more
wiley +1 more source
Computational analysis of the flow field in a laboratory gas turbine combustor
The study of the isothermal non-reactive flow field in a laboratory gas turbine combustor is of significant importance in weak swirl conditions. The numerical simulations are carried out with a commercial software and turbulence RANS models.
Piccoli, Dario
core
Experimental and modelling studies of coal/biomass oxy-fuel combustion in a pilot-scale PF combustor [PDF]
This thesis focuses on enhancing knowledge on co-firing oxy-combustion cycles to boost development of this valuable technology towards the aim of it becoming an integral part of the energy mix.
Jurado Pontes, Nelia
core
Circulating Fluid Bed Combustor
The circulating bed combustor represents an alternative concept of burning coal in fluid bed technology, which offers distinct advantages over both the current conventional fluidized bed combustion system and the pulverized coal boilers equipped with ...
Hsiao, K. H., Fraley, L. D., Do, L. N.
core
Numerical Study on the Solid Fuel Rocket Scramjet Combustor with Cavity
Scramjet based on solid propellant is a good supplement for the power device of future hypersonic vehicles. A new scramjet combustor configuration using solid fuel, namely, the solid fuel rocket scramjet (SFRSCRJ) combustor is proposed.
Chaolong Li +4 more
doaj +1 more source
Fuel Injection and Flame Stabilization in a Liquid-Kerosene-Fueled Supersonic Combustor
Investigations on combustion enhancement and stabilization of liquid kerosene using five different integrated fuel-injection/cavity-based flameholder configurations were conducted in a model combustor of cross sections 51 x 70 mm.
俞刚 +5 more
core +1 more source
The ignition and extinction performances of an engine’s combustion chamber are crucial for its overall performance, reliability, fuel efficiency, and environmental impact.
Wenhui Ling +5 more
doaj +1 more source
The flame stabilization limit on micro-combustor had studied to support the micro power generator system. Micro-combustion became the crucial components in a micro power generation system as heat resource that will be converted into electricity. However,
Saputro Herman +11 more
doaj +1 more source

