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cooling" on near-wall flame propagation and incomplete combustion emissions. The research outcomes will provide fundamental theoretical support for the advancement of high-pressure direct-injection methanol
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-chemical properties similar to conventional kerosene, their combustion behavior can differ significantly, requiring adjustments and optimization of current gas turbines (GT). In this context, numerical
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site, creating NH3/H2 mixtures with improved combustion properties. However, these mixtures emit significant amounts of NOx unless operated at very low fuel/air equivalence ratios (FAER), which
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for diversification and optimization of energy recovery and conversion systems to ensure a stable and secure energy supply. Among potential energy sources, solar radiation, biomass combustion or gasification
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PhD project is centred around advanced CFD modelling of liquid green fuel (methanol and ammonia) combustion under engine-like conditions, i.e., in a constant-volume combustion chamber (CVCC
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laboratory-scale combustion chamber for burning ammonia and hydrogen mixtures, with emphasis on the compatibility of these mixtures. The main objectives include achieving the best possible combustion
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: https://www.brunel.ac.uk/about/our-history/home The Centre for Advanced Powertrain and Fuels (CAPF) at Brunel University London invites applications for a Research Assistant / PhD position as part of
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Centre Euopéen de Recherche et de Formation Avancée en Calcul Scientifique (CERFACS) | Toulouse, Midi Pyrenees | France | 2 months ago
of application of the CFD team are turbulent, unsteady and reacting flows. It has an internationally recognized expertise in combustion and aerospace propulsion. The team has developed software to compute
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, significant technical challenges must be overcome when operating with new fuels or fuel-blends. New and existing engines must be designed to prevent combustion instabilities, flashback, and maintain low NOx
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of the University. (https://www.polito.it/en ) Task description for your Individual Research Project (IRP) Problem Definition: The possibility of assessing environmental sustainability of future launchers from