TY - GEN
T1 - High fidelity large eddy simulation of reacting supercritical fuel jet-in-cross-flow using GPU acceleration
AU - Gottiparthi, Kalyana C.
AU - Sankaran, Ramanan
AU - Oefelein, Joseph C.
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=85088062920&partnerID=8YFLogxK
U2 - 10.2514/6.2016-4791
DO - 10.2514/6.2016-4791
M3 - Conference contribution
AN - SCOPUS:85088062920
SN - 9781624104060
T3 - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
BT - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Y2 - 25 July 2016 through 27 July 2016
ER -