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Combustion Modeling

Completed TRL 2 (started at 1, targeting 4)

Description

The Combustion Modeling Technical Challenge develops new computational models that more accurately predict detailed chemical reactions associated with jet fuel combustion. These new models will lead to the design of more fuel-efficient jet engines and allow the relative merits of different alternative fuels to be assessed. Near-term goals include the accurate prediction of lean flame blowout and soot emissions as a function of changes in fuel composition.

Benefits

Improved models of chemically reacting flows found in jet engines including advances in chemistry, spray, and turbulent combustion models will enable engine designs offering improved fuel efficiency and reduced NOx emissions. Advances in model accuracy and understanding of combustion processes will accelerate certification and use of promising alternative fuels, in collaboration with the National Jet Fuels Combustion Program (NJFCP).

Details

Technology areaPropulsion Systems > Aero Propulsion > Alternative Low-Carbon Jet Fuel
ProgramTransformative Aeronautics Concepts Program (TACP)
Lead organizationGlenn Research Center, Cleveland, OH
Start date2016-10-01
End date2021-09-30

Project contacts

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How to get involved

This is early/mid-stage (TRL 2) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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