In military propulsion applications, the characterization of internal combustion engines operating with jet fuel is vital to understand engine performance, combustion phasing, and emissions when JP-8 is fully substituted for diesel fuel. In this work, high-resolution large eddy simulation (LES) simulations have been performed in-order to provide a comprehensive analysis of the detailed mixture formation process in engine sprays for nozzle configurations of interest to the Army. The first phase examines the behavior of a nonreacting evaporating spray, and demonstrates the accuracy in predicting liquid and vapor transient penetration profiles using a multirealization statistical grid-converged approach. The study was conducted using a suite of single-orifice injectors ranging from 40 to 147 μm at a rail pressure of 1000 bar and chamber conditions at 900 K and 60 bar. The next phase models the nonpremixed combustion behavior of reacting sprays and investigates the submodel ability to predict auto-ignition and lift-off length (LOL) dynamics. The model is constructed using a Kelvin Helmholtz–Rayleigh Taylor (KH–RT) spray atomization framework coupled to an LES approach. The liquid physical properties are defined using a JP-8 mixture containing 80% n-decane and 20% trimethylbenzene (TMB), while the gas phase utilizes the Aachen kinetic mechanism (Hummer, et al., 2007, “Experimental and Kinetic Modeling Study of Combustion of JP-8, Its Surrogates, and Reference Components in Laminar Non Premixed Flows,” Proc. Combust. Inst., 31, pp. 393–400 and Honnet, et al., 2009, “A Surrogate Fuel for Kerosene,” Proc. Combust. Inst., 32, pp. 485–492) and a detailed chemistry combustion approach. The results are in good agreement with the spray combustion measurements from the Army Research Laboratory (ARL), constant pressure flow (CPF) facility, and provide a robust computational framework for further JP-8 studies of spray combustion.
Large Eddy Simulation of High Reynolds Number Nonreacting and Reacting JP-8 Sprays in a Constant Pressure Flow Vessel With a Detailed Chemistry Approach
U.S. Army Research Laboratory,
Vehicle Technology Directorate,
4603 Flare Loop Drive,
Aberdeen Proving Ground, MD 21005
e-mail: luis.g.bravo2.civ@mail.mil
Convergent Science, Inc.,
6400 Enterprise Ln,
Madison, WI 53719
e-mail: sameera.wijeyakulasuriya@convergecfd.com
Convergent Science, Inc.,
6400 Enterprise Ln,
Madison, WI 53719
e-mail: pomraning@convergecfd.com
Convergent Science, Inc.,
6400 Enterprise Ln,
Madison, WI 53719
e-mail: senecal@convergecfd.com
Vehicle Technology Directorate,
4603 Flare Loop Drive,
Aberdeen Proving Ground, MD 21005
e-mail: chol-bum.m.kweon2.civ@mail.mil
U.S. Army Research Laboratory,
Vehicle Technology Directorate,
4603 Flare Loop Drive,
Aberdeen Proving Ground, MD 21005
e-mail: luis.g.bravo2.civ@mail.mil
Convergent Science, Inc.,
6400 Enterprise Ln,
Madison, WI 53719
e-mail: sameera.wijeyakulasuriya@convergecfd.com
Convergent Science, Inc.,
6400 Enterprise Ln,
Madison, WI 53719
e-mail: pomraning@convergecfd.com
Convergent Science, Inc.,
6400 Enterprise Ln,
Madison, WI 53719
e-mail: senecal@convergecfd.com
Vehicle Technology Directorate,
4603 Flare Loop Drive,
Aberdeen Proving Ground, MD 21005
e-mail: chol-bum.m.kweon2.civ@mail.mil
Contributed by the Internal Combustion Engine Division of ASME for publication in the JOURNAL OF ENERGY RESOURCES TECHNOLOGY. Manuscript received February 12, 2016; final manuscript received February 16, 2016; published online March 24, 2016.
Editor: Hameed Metghalchi.This work is in part a work of the U.S. Government. ASME disclaims all interest in the U.S. Government's contributions.
Bravo, L., Wijeyakulasuriya, S., Pomraning, E., Senecal, P. K., and Kweon, C. (March 24, 2016). "Large Eddy Simulation of High Reynolds Number Nonreacting and Reacting JP-8 Sprays in a Constant Pressure Flow Vessel With a Detailed Chemistry Approach." ASME. J. Energy Resour. Technol. May 2016; 138(3): 032207. https://doi.org/10.1115/1.4032901
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