Assessment Of Dodecane Turbulent-Chemistry Interactions Using Computational Fluid Dynamics

Abstract

Gas turbine fuel surrogates have been used in computational studies of high performance propulsion systems operating under extreme conditions. Detailed mechanisms have been developed for these surrogates that are capable of depicting the performance of jet fuels which have assisted in the analysis and performance-based simulations of combustor designs. However, these detailed mechanisms contain hundreds of species and thousands of elementary reactions making multi-dimensional computational simulations of practical turbine combustor applications unfeasible due to its impact on computational cost and run time. In order to facilitate computational analyses these detailed mechanisms are tuned, allowing for the development of reduced order models or mechanisms that still captures the dominant kinetics of the system.

Publication Date

1-1-2017

Publication Title

53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017

Document Type

Article; Proceedings Paper

Personal Identifier

scopus

DOI Link

https://doi.org/10.2514/6.2017-5081

Socpus ID

85088760949 (Scopus)

Source API URL

https://api.elsevier.com/content/abstract/scopus_id/85088760949

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