There are currently numerous efforts to create renewable fuels that have similar properties to conventional diesel fuels. One major future challenge is evaluating how these new fuels will function in older legacy diesel engines. It is desired to have physically based modeling tools that will predict new fuel performance without extensive full scale engine testing. This study evaluates two modeling tools that are used together to predict ignition delay in a military diesel engine running n-hexadecane as a fuel across the engine's speed-load range. AVL-FIRE® is used to predict the physical delay of the fuel from the start of injection until the formation of a combustible mixture. Then a detailed Lawrence Livermore National Laboratory (LLNL) chemical kinetic mechanism is used to predict the chemical ignition delay. This total model predicted ignition delay is then compared to the experimental engine data. The combined model predicted results show good agreement to that of the experimental data across the engine operating range with the chemical delay being a larger fraction of the total ignition delay. This study shows that predictive tools have the potential to evaluate new fuel combustion performance.
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July 2014
Research-Article
Predicting the Physical and Chemical Ignition Delays in a Military Diesel Engine Running n-Hexadecane Fuel
Jim Cowart
Jim Cowart
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Len Hamilton
Dianne Luning Prak
Jim Cowart
Contributed by the Combustion and Fuels Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received January 15, 2014; final manuscript received January 23, 2014; published online February 20, 2014. Editor: David Wisler.
J. Eng. Gas Turbines Power. Jul 2014, 136(7): 071505 (7 pages)
Published Online: February 20, 2014
Article history
Received:
January 15, 2014
Revision Received:
January 23, 2014
Citation
Hamilton, L., Luning Prak, D., and Cowart, J. (February 20, 2014). "Predicting the Physical and Chemical Ignition Delays in a Military Diesel Engine Running n-Hexadecane Fuel." ASME. J. Eng. Gas Turbines Power. July 2014; 136(7): 071505. https://doi.org/10.1115/1.4026657
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