High fidelity large eddy simulation of reacting supercritical fuel jet-in-cross-flow using GPU acceleration

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Abstract

When liquid fuel is injected into a combustion chamber, the dispersion of the fuel and the ensuing combustion are characterized by the ambient pressure. At elevated pressures, unlike the classical liquid atomization observed at sub-critical pressures, the fuel is dispersed by diffusion-dominated mixing. Numerical simulation of fuel-air mixing and the resulting reactive flow is dependent on accurate modeling of the supercritical flow and is very challenging. In most cases, the combination of the complex thermodynamics and the computational grid resolution requirements render the numerical investigations computationally intractable. However, with the advent of novel heterogeneous computer architectures, it is possible to overcome the computational resource constraints and investigate mixing and combustion of supercritical fuels. In this paper, we study a reacting n-decane Jet-In-Cross-Flow (JICF) of air at high ambient pressure. The flow properties are computed using routines accelerated for Graphics Processing Unit (GPU) computation. The code assisted by GPU computation is nearly 3 times faster due to the reduction in the cost associated with the routines for thermodynamics and subgrid closures. Followed by the dispersion of the supercritical fuel due to the interaction with the turbulent cross flow, the combustion ensues in the leeward side of the jet. The flame is anchored in the aft and spreads downstream following the mixing zone. Due to the heat release, in comparison to the non-reactive case, the downstream turbulence is reduced. The temperature in the mixing zone is correlated to the mixture fraction of the fuel and results in formation of hot spots that convect with the vortices generated by fuel-air mixing.

Original languageEnglish
Title of host publication52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624104060
DOIs
StatePublished - 2016
Event52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016 - Salt Lake City, United States
Duration: Jul 25 2016Jul 27 2016

Publication series

Name52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016

Conference

Conference52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Country/TerritoryUnited States
CitySalt Lake City
Period07/25/1607/27/16

Funding

This research used resources of the Oak Ridge Leadership Computing Facility at the Oak Ridge National Laboratory, which is supported by the Office of Science of the U.S. Department of Energy under contract DE-AC05-00OR22725. Support was also provided by the U.S. Department of Energy, Office of Basic Energy Sciences, Division of Chemical Sciences, Geosciences, and Biosciences. Sandia National Laboratories is a multiprogram laboratory operated by Sandia Corporation, a Lockheed Martin Company, for the United States Department of Energy under contract DE-AC04-94-AL85000.

FundersFunder number
U.S. Department of EnergyDE-AC04-94-AL85000, DE-AC05-00OR22725
Office of Science
Basic Energy Sciences
Sandia National Laboratories
Chemical Sciences, Geosciences, and Biosciences Division

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