Aerospace

Simulating low emission aerospace technology

The aerospace industry has targets to achieve net zero aviation by 2050. Significant steps are being made in reducing emissions and improving fuel economy which are now being supported with new technology such as electric, hydrogen and the use of alternative e-fuels.

Aerospace propulsion manufacturers need to balance the requirements to continue the optimisation of existing engines with lower emissions and increased fuel economy as well as introduce new non-carbon technology.

The design challenge is to consider the available options across full electric, hydrogen, e-fuels and existing technologies in a quick, efficient and cost-effective manner. In the initial stages of development, physical prototype modelling is expensive, requiring virtual simulation tools to answer many of the 'What ifs' before committing to a design path.

Simulation of the propulsion system is at the heart of aerospace design, especially in predicting performance in key areas such as aerodynamics, thermal management and engine behaviour across a range of fuels and duty cycles.

At Realis Simulation we have extensive experience of using software to streamline the propulsion system design process – answering many of the ‘What ifs’ using computer simulation before Original Equipment Manufacturers (OEMs) and Tier 1 suppliers commit to expensive physical prototypes.

Our software models the full propulsion system design from fuel intake, power generation, power transfer and exhaust emissions reduction. It simulates energy losses from friction, oil consumption and thermal heat transfer as well as component durability across various drive cycles using traditional, non-carbon e-fuels, hybrid, electric, hydrogen fuel cells and hydrogen combustion power units.

Our insights

Combustion characteristics and energy distribution of hydrogen engine under high oxygen concentration

Combustion characteristics and energy distribution of hydrogen engine under high oxygen concentration

Technical Paper
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Study of the effects of trapped compression ratio on the heavy fuel operation of a spark ignition unmanned aerial vehicle engine

Study of the effects of trapped compression ratio on the heavy fuel operation of a spark ignition unmanned aerial vehicle engine

Technical Paper
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