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Ignition Delay of 3-Carene:Single Pulse Shock Tube Study


Affiliations
1 Department of Aerospace Engineering, Indian Institute of Science, Bengaluru 560 012, India
2 Department of Applied Physics, Birla Institute of Technology, Mesra 835 215, India
3 Department of Inorganic and Physical Chemistry, Indian Institute of Science, Bengaluru 560 012, India
 

Ignition delay experiments of 3-carene, a biofuel, have been carried out in a single-pulse shock tube for three equivalence ratios, 0.5, 1 and 2. The temperature was varied from 1140 to 1606 K. In the above-mentioned conditions, ignition delay was found to vary from 1.180 ms to 144 μs. The ignition delay values of 3-carene were found to be lower than those of JP-10, a kerosene-based fuel being considered for hypersonic applications.

Keywords

Biofuel Combustion, 3-Carene, Ignition Delay, Shock Tube.
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  • Ignition Delay of 3-Carene:Single Pulse Shock Tube Study

Abstract Views: 304  |  PDF Views: 126

Authors

N. Sharath
Department of Aerospace Engineering, Indian Institute of Science, Bengaluru 560 012, India
K. P. J. Reddy
Department of Aerospace Engineering, Indian Institute of Science, Bengaluru 560 012, India
P. K. Barhai
Department of Applied Physics, Birla Institute of Technology, Mesra 835 215, India
E. Arunan
Department of Inorganic and Physical Chemistry, Indian Institute of Science, Bengaluru 560 012, India

Abstract


Ignition delay experiments of 3-carene, a biofuel, have been carried out in a single-pulse shock tube for three equivalence ratios, 0.5, 1 and 2. The temperature was varied from 1140 to 1606 K. In the above-mentioned conditions, ignition delay was found to vary from 1.180 ms to 144 μs. The ignition delay values of 3-carene were found to be lower than those of JP-10, a kerosene-based fuel being considered for hypersonic applications.

Keywords


Biofuel Combustion, 3-Carene, Ignition Delay, Shock Tube.



DOI: https://doi.org/10.18520/cs%2Fv108%2Fi11%2F2083-2087